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Author SHA1 Message Date
lyf 267a659242 feat(ui): 新增裁判系统自定义UI(0x0301)并打通键鼠→底盘链路 
键鼠控制(此前 WASD 无反应):
- 云台 robot_cmd_task:0x0304 与 USART3 帧内键鼠合并为共享视图 keyboard_merged(0x0304 优先);
  键鼠模式由帧内键鼠动作进入,动云台左摇杆退出
- c_comm_task/c_comm:键鼠在控时底盘摇杆由 WASD+鼠标合成,改读共享视图(此前只认 0x0304)
- dr16/调试输出:新增帧内键鼠原始字节诊断(key_lo/key_hi/mouse_*/s1/frames)

自定义UI(底盘板经裁判系统 USART6 绘制到选手端):
- 新增 底盘/modules/comms/referee_ui.c|h:15 字节图形组包(带编译期断言),
  v5 卡片式 HUD = 俯仰梯(pitch) + 罗盘刻度带(底盘朝向) + 预估底盘功率 + 超级电容
  + 摩擦轮 L/R 转速 + 小陀螺状态,yaw 在刻度带右侧;5Hz 刷新,约 50 图元/8 包
- referee.c 新增 referee_send_frame()(cmd 0x0301 机器人交互数据,CRC8+CRC16,USART6 TX DMA)
- 新增 CToC 0x1B9:云台把 pitch 与摩擦轮转速带给底盘(底盘本地没有这两个量)
- 版式避开官方保留区:顶部比分条/左下小地图/右下战车模块/中部两块官方保留

验证:云台 Code=99540 RO=1764 RW=420 ZI=62572;底盘 Code=99452 RO=1928 RW=416 ZI=62584;均 0 错误 0 警告。
未做实机验证(当前无板/无图传);UI 协议常量(UI_RECEIVER_ID/UI_SEND_HZ)与版式坐标集中在 referee_ui.h 宏区,便于按协议 PDF 一处校正。
 2026-10-16 04:24:32 +08:00
lyf 370d4519b5 电流环控制，并实现简单的补偿控制，还差参数具体化。 2026-10-16 00:54:52 +08:00
lyf 67eea77789 yaw正方向修正 2026-10-10 21:17:58 +08:00
lyf 79a545b379 修复上电云台正方向问题，以及初步调好了底盘跟随PID，以及小陀螺模式下的运动偏移问题。 2026-09-12 19:05:26 +08:00
43 changed files with 1588 additions and 270 deletions
Expand all files Collapse all files
.gitignore
+14
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@@ -28,6 +28,20 @@
*.uvguix
DebugConfig/
# ---- J-Link 调试器自动生成(与具体探针/机器绑定, 非源码) ----
# JLinkSettings.ini: 点"下载/调试"时 Keil 写下的连接参数(器件/接口/速率)
# JLinkLog.txt: J-Link 驱动日志
# 两者都会随换机器、换探针、换烧录方式而变, 不应入库; 缺失时 Keil 会自动重建
JLinkSettings.ini
JLinkLog.txt
JLinkLog.txt.*
*.jlink
# ---- Keil UV4 编译/烧录日志(uv4 -b/-f -o 生成) ----
build_log.txt
*_build.txt
*_flash.txt
# ---- 编辑器 / 系统 ----
*.bak
*.ddk
.vscode/settings.json
Vendored
+3
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@@ -0,0 +1,3 @@
{
"python.analysis.stubPath": "C:\\Users\\16936\\.kendryte\\k230_canmv_pylance\\4702c5814722ec2f\\typings"
}
README.md
+6 -1
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@@ -175,7 +175,7 @@ FreeRTOS 节拍 1 kHz。任务来自 `Core/Src/freertos.c`:
| 板 | CAN1 | CAN2 |
| --- | --- | --- |
| 云台板 | Pitch GM6020 `0x206`、摩擦轮 M3508 `0x201/0x202` | Yaw GM6020 `0x205`、底盘回传 `0x019` |
| 云台板 | Pitch GM6020 `0x206`(0x1FE)、摩擦轮 M3508 `0x201/0x202`(0x200) | Yaw GM6020 `0x205`(0x1FE)、拨弹 M2006 `0x201`(0x200)、底盘回传 `0x019` |
| 底盘板 | 四轮 M3508 `0x201~0x204` | 云台数据 `0x149/0x189/0x1A9` |
### 6.2 串口分配
@@ -344,6 +344,9 @@ gx=0.0012 gy=-0.0031 gz=0.0165 zo=0.0009 ck=1 ca=803 cg=1002 se=0 st=1
> 每一条都是实际踩过的坑。更详细的排障过程见 [doc/已知问题与排障.md](./doc/已知问题与排障.md)。
### 11.0 已知底盘1号电机，云台pitch电机会掉线，记得检修
### 11.1 增删源文件必须同步改 `.uvprojx`(和 `.uvoptx`)
新增/删除 `.c` 后必须同时在 Keil 工程里增删条目,并检查:
@@ -431,3 +434,5 @@ BMI088 的 DRDY 是**电平型**信号:某次失败或被挡掉的读取没把
## 参考
- 踩坑记录与排障手册:[`doc/已知问题与排障.md`](./doc/已知问题与排障.md)
云台/Application/Task/Inc/robot_cmd_task.h
+9
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@@ -24,4 +24,13 @@ typedef struct
extern keyboard_data_t keyboard_data;
/* ---- 键鼠来源合并视图(2026-10-16) ----
* 客户端键鼠既可能从裁判系统 0x0304 进来,也可能从 USART3 那 18 字节帧进来
* (官方 18 字节控制帧里就带鼠标与按键,由 dr16 解析成 dr16.mouse_rl / dr16.key_w 等)。
* robot_cmd_task 每周期把两路合并到下面这个视图:
* 云台/发射控制 与 c_comm_task 的底盘摇杆合成 都读它,
* 避免两处各判一次出现"云台跟鼠标、底盘却还在收遥控器原始摇杆"。 */
extern keyboard_data_t keyboard_merged; /* 合并后的键鼠数据(0x0304 优先) */
extern uint8_t keyboard_merged_online; /* 1=键鼠在控(0x0304 在线 或 帧内键鼠有动作) */
#endif
云台/Application/Task/Src/c_comm_task.c
+25 -15
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@@ -33,28 +33,38 @@ void c_comm_task(void const * argument)
for (;;)
{
#if defined(ROBOT_TYPE_GIMBAL)
uint8_t kb_online = (keyboard_data.last_tick != 0 &&
HAL_GetTick() - keyboard_data.last_tick < DEVICE_OFFLINE_TIME_MS * 10);
/* 键鼠来源已由 robot_cmd_task 合并(0x0304 优先,否则 USART3 帧内键鼠)。
* 直接用共享视图,保证"云台怎么控、底盘就怎么收"——否则 WASD 合成的
* 底盘摇杆会因为这里只认 0x0304 而被整段跳过(客户端键鼠走帧内时平移失效)。 */
uint8_t kb_online = keyboard_merged_online;
uint8_t kb[12];
kb[0] = (uint8_t)(keyboard_data.mouse_rl & 0xFF);
kb[1] = (uint8_t)((uint16_t)keyboard_data.mouse_rl >> 8);
kb[2] = (uint8_t)(keyboard_data.mouse_du & 0xFF);
kb[3] = (uint8_t)((uint16_t)keyboard_data.mouse_du >> 8);
kb[4] = (uint8_t)(keyboard_data.mouse_wheel & 0xFF);
kb[5] = (uint8_t)((uint16_t)keyboard_data.mouse_wheel >> 8);
kb[6] = keyboard_data.mouse_key_l;
kb[7] = keyboard_data.mouse_key_r;
kb[8] = (uint8_t)(keyboard_data.key_w | (keyboard_data.key_s << 1) |
(keyboard_data.key_a << 2) | (keyboard_data.key_d << 3) |
(keyboard_data.key_shift << 4) | (keyboard_data.key_ctrl << 5) |
(keyboard_data.key_q << 6) | (keyboard_data.key_e << 7));
kb[9] = (uint8_t)(keyboard_data.key_alpha1 | (keyboard_data.key_alpha2 << 1));
kb[0] = (uint8_t)(keyboard_merged.mouse_rl & 0xFF);
kb[1] = (uint8_t)((uint16_t)keyboard_merged.mouse_rl >> 8);
kb[2] = (uint8_t)(keyboard_merged.mouse_du & 0xFF);
kb[3] = (uint8_t)((uint16_t)keyboard_merged.mouse_du >> 8);
kb[4] = (uint8_t)(keyboard_merged.mouse_wheel & 0xFF);
kb[5] = (uint8_t)((uint16_t)keyboard_merged.mouse_wheel >> 8);
kb[6] = keyboard_merged.mouse_key_l;
kb[7] = keyboard_merged.mouse_key_r;
kb[8] = (uint8_t)(keyboard_merged.key_w | (keyboard_merged.key_s << 1) |
(keyboard_merged.key_a << 2) | (keyboard_merged.key_d << 3) |
(keyboard_merged.key_shift << 4) | (keyboard_merged.key_ctrl << 5) |
(keyboard_merged.key_q << 6) | (keyboard_merged.key_e << 7));
kb[9] = (uint8_t)(keyboard_merged.key_alpha1 | (keyboard_merged.key_alpha2 << 1));
kb[10] = 0;
kb[11] = 0;
c_comm_master_send(kb_online, kb, gimbal_motor_offline(),
cmd_robot.spin_flag); // 故障位+小陀螺使能位
/* 0x1B9 自定义UI 专用量:底盘本地没有 pitch 与摩擦轮转速,
* 由云台随板间通讯带给它(见 底盘/modules/comms/referee_ui.c)。
* pitch 取云台 pitch 环反馈 -att_deg_roll;摩擦轮转速取电机反馈 rpm。 */
c_comm_master_send_ui(-att_deg_roll,
(float)motor_friction_l.fdb.rotor_speed,
(float)motor_friction_r.fdb.rotor_speed,
cmd_robot.spin_flag);
/* 0x1A9 姿态帧:跟随符号自动综合的数据源
* flags:bit0=att_ready bit1=tick增向CCW bit2=bit1有效 */
{
云台/Application/Task/Src/debug_task.c
+133 -9
View File
@@ -1,5 +1,5 @@
/* =============================================================================
* debug_task.c - USB 虚拟串口(CDC)姿态输出(欧拉角 + 姿态链路诊断)
* debug_task.c - USB 虚拟串口(CDC)姿态输出(欧拉角 + 姿态链路诊断 + 控制量)
* 每 DEBUG_OUT_PERIOD_MS 输出一行。单位: 角度 ° / 加速度 m/s² / 角速度 rad/s
*
* ---- 欧拉角(QuaternionEKF 解算结果,见 modules/ins) ----
@@ -25,7 +25,30 @@
* se bmi088_spi_errors:SPI/DMA 出错次数;st=bmi088_spi_state()
* (1=READY,非 1 说明 SPI 被卡住,数据路会因此停摆)
*
* 开关: DEBUG_ATT_HEALTH=0 只输出三个欧拉角;DEBUG_ATT_DIAG=0 去掉诊断位。
* ---- 控制量(DEBUG_CMD_OUT=1 时追加;用于排查 控制源→cmd_robot→执行机构) ----
* online 1=**遥控器(DR16)在线** —— 本板这一位只反映 DR16,键鼠不置位!
* 没有遥控器时整段控制分支都不执行(见 robot_cmd_task.c 的 online 门控),
* 所以"键鼠测试"也必须有遥控器在线,否则这里恒为 0。
* src 0=遥控器 1=键鼠(判据:0x0304 在 1s 内到过 keyboard_data.last_tick)
* spin 小陀螺使能(云台侧检测,随 0x189 下发给底盘)
* yaw_d/pitch_d 本周期云台角度增量(°/2ms 任务周期,×500 即 °/s)
* fric/fire/eject 发射机构开关 reset 云台角度复位请求
* s2/ctrl 遥控器 S2 档位与 Ctrl 按下沿 —— 底盘就是靠这两个量推出
* chassis_mode,所以本板不输出模式本身(本板该字段恒为 OFF)
* wheel 遥控拨轮原始值(1000~1050 为中立)
* --- 以下为 DR16 帧内容诊断(判断"键鼠数据到底有没有到机器人") ---
* s1 左侧拨杆(1上 2下 3中)。注意官方 RoboRTS 的 dbus.c 与本工程一致:
* sw2=bit44-45→s2, sw1=bit46-47→s1;若与实物相反,用本列与 s2 对照即可判定
* mouse_rl/mouse_du/mouse_wheel 帧里 data[6..11] 解析出的鼠标三轴
* mouse_l/mouse_r 帧里 data[12]/data[13](鼠标左右键)
* key_lo/key_hi 帧里 data[14]/data[15] **原始字节**(不做位拆分)
* ★ 按下 W 时 key_lo 应变 0x01;若恒为 0,说明帧里根本没有键鼠数据
* frames dr16_frame_count;持续增长说明 USART3 一直在收帧
* 无健康位(DEBUG_ATT_HEALTH=0)时输出为纯数字 CSV,列序即上面顺序,
* 可被 Lissio FireWater 直接解析成通道绘图。
*
* 开关: DEBUG_ATT_HEALTH=0 只输出三个欧拉角;DEBUG_ATT_DIAG=0 去掉诊断位;
* DEBUG_CMD_OUT=1 追加控制量字段。
* ========================================================================== */
#include "debug_task.h"
#include "cmsis_os.h"
@@ -35,24 +58,70 @@
#include "attitude.h"
#include "ins.h"
#include "bmi088.h"
#include "gimbal.h"
#include "dr16.h"
#include "robot_typedef.h"
#include <stdio.h>
#include <math.h>
#include <string.h>
/* ===== 2026-10-15 台架调参临时遥测(已停用,保留备查) =====
* 启用时把 #if 0 改 #if 1:本任务改为输出 5 列 CSV
* setpoint_deg, actual_deg, out_current, ecd_deg, gyro_x_dps
* (逗号分隔+换行,可被 Lissio FireWater 自动识别为 5 通道),采样率提到 200Hz,
* 用于定量观测阶跃响应与判断"轴是否真的在转动"。 */
#if 0
#include "robot_param.h"
#define DEBUG_PITCH_TUNE 1
#if DEBUG_PITCH_TUNE
#define DEBUG_OUT_PERIOD_MS 5 /* 200Hz:2ms 控制环的阶跃响应需 ≥100Hz 采样才量得准 */
#endif
#endif
/* 1-输出健康位(cvg/rdy/imu/an/gn); 0-只输出三个欧拉角 */
#define DEBUG_ATT_HEALTH 1
#define DEBUG_ATT_HEALTH 0
/* 1-再附加原始陀螺/零偏/采样计数(排障用); 0-只留上面的通用健康位 */
#define DEBUG_ATT_DIAG 1
#define DEBUG_ATT_DIAG 0
/* 1-仅输出 Pitch 调参行(便于用 VOFA+/串口示波器绘图); 0-同时输出姿态行与 Pitch 调参行 */
#define DEBUG_PITCH_ONLY 0
/* 1-追加控制量字段(见文件头); 0-保持原姿态输出不变 */
#define DEBUG_CMD_OUT 1
/* 输出周期(ms)。姿态观测建议 100ms(10Hz) */
#define DEBUG_OUT_PERIOD_MS 100
void debug_task(void const * argument)
{
char line[192];
char line[384];
char tail[112];
char pitch_line[128];
for (;;)
{
#if 0
/* ===== 2026-10-15 台架 Pitch 调参遥测(已停用,保留备查) =====
* 5 列 CSV → Lissio FireWater 直接成 5 通道:
* setpoint(位置环设定值含台架偏置), actual(-att_deg_roll),
* out(最终电流), ecd_deg(编码器机械角), gyro_x_dps(陀螺 x 轴角速度) */
const float tune_ecd_deg = ((float)motor_pitch_gimbal.fdb.raw_angle -
(float)PITCH_GM6020_ENCODER_ZERO) * (360.0f / 8192.0f);
const float tune_gyro_dps = bmi088_gyro[0] * 57.29578f;
int len = snprintf(line, sizeof(line), "%.3f,%.3f,%.1f,%.3f,%.2f\n",
gimbal_pitch_setpoint_deg(),
-att_deg_roll,
pitch_current,
tune_ecd_deg,
tune_gyro_dps);
#endif
#if DEBUG_PITCH_ONLY
/* 仅输出 Pitch 调参数据(编码值、roll、PID最后输出值、遥控pitch杆量) */
int len = snprintf(line, sizeof(line),
"p_ecd=%u roll=%.2f p_out=%.1f rc_pitch=%u\r\n",
(unsigned)motor_pitch_gimbal.fdb.raw_angle,
att_deg_roll,
pitch_current,
(unsigned)dr16.rc_l_UD);
#else
const float an = sqrtf(bmi088_accel[0] * bmi088_accel[0] +
bmi088_accel[1] * bmi088_accel[1] +
bmi088_accel[2] * bmi088_accel[2]);
@@ -71,14 +140,69 @@ void debug_task(void const * argument)
#endif
#if DEBUG_ATT_HEALTH
#if DEBUG_CMD_OUT
/* 健康位分支是文本格式,控制量就按 key=value 追加,便于人读 */
char ctl[160];
snprintf(ctl, sizeof(ctl),
" online=%u src=%u spin=%u yaw_d=%.4f pitch_d=%.4f fric=%u fire=%u"
" eject=%u reset=%u s2=%u ctrl=%u wheel=%d",
(unsigned)cmd_robot.online, (unsigned)cmd_robot.source,
(unsigned)cmd_robot.spin_flag,
cmd_robot.gimbal_yaw_delta, cmd_robot.gimbal_pitch_delta,
(unsigned)cmd_robot.friction_on, (unsigned)cmd_robot.fire,
(unsigned)cmd_robot.eject, (unsigned)cmd_robot.gimbal_reset,
(unsigned)dr16.s2, (unsigned)dr16.key_push_ctrl,
(int)cmd_robot.thumb_wheel);
#else
const char * ctl = "";
#endif
int len = snprintf(line, sizeof(line),
"yaw=%.2f pitch=%.2f roll=%.2f cvg=%u rdy=%u imu=%u an=%.2f gn=%.3f%s\r\n",
"ecd=%u yaw=%.2f pitch=%.2f roll=%.2f cvg=%u rdy=%u imu=%u an=%.2f gn=%.3f%s%s\r\n",
(unsigned)motor_yaw_gimbal.fdb.raw_angle,
att_deg_yaw, att_deg_pitch, att_deg_roll,
(unsigned)INS.ConvergeFlag, (unsigned)att_ready,
(unsigned)bmi088_online, an, gn, tail);
(unsigned)bmi088_online, an, gn, tail, ctl);
#else
int len = snprintf(line, sizeof(line), "yaw=%.2f pitch=%.2f roll=%.2f\r\n",
att_deg_yaw, att_deg_pitch, att_deg_roll);
#if DEBUG_CMD_OUT
/* 纯数字 CSV。前 3 列保持原样(pitch_ecd, pitch_current, yaw_ecd),其余:
* online,src,spin, yaw_d,pitch_d, fric,fire,eject,reset, s2,ctrl,wheel,
* s1, mouse_rl,mouse_du,mouse_wheel,mouse_l,mouse_r, key_lo,key_hi,
* dr16_frame_count
* 末尾这 9 列是 DR16 帧内容诊断:key_lo/key_hi 就是帧里的 data[14]/data[15]。
* 按住 W 时若它们仍为 0,说明帧里本就没有键鼠数据(不是解析问题)。 */
int len = snprintf(line, sizeof(line),
"%u,%.1f,%u,%u,%u,%u,%.4f,%.4f,%u,%u,%u,%u,%u,%u,%d,%u,%d,%d,%d,%u,%u,%u,%u,%lu\r\n",
(unsigned)motor_pitch_gimbal.fdb.raw_angle,
pitch_current,
(unsigned)motor_yaw_gimbal.fdb.raw_angle,
(unsigned)cmd_robot.online,
(unsigned)cmd_robot.source,
(unsigned)cmd_robot.spin_flag,
cmd_robot.gimbal_yaw_delta,
cmd_robot.gimbal_pitch_delta,
(unsigned)cmd_robot.friction_on,
(unsigned)cmd_robot.fire,
(unsigned)cmd_robot.eject,
(unsigned)cmd_robot.gimbal_reset,
(unsigned)dr16.s2,
(unsigned)dr16.key_push_ctrl,
(int)cmd_robot.thumb_wheel,
(unsigned)dr16.s1,
(int)dr16.mouse_rl,
(int)dr16.mouse_du,
(int)dr16.mouse_wheel,
(unsigned)dr16.mouse_key_l,
(unsigned)dr16.mouse_key_r,
(unsigned)dr16.key_code_lo,
(unsigned)dr16.key_code_hi,
(unsigned long)dr16_frame_count);
#else
int len = snprintf(line, sizeof(line), "%u,%.1f,%u\r\n",
(unsigned)motor_pitch_gimbal.fdb.raw_angle,
pitch_current,(unsigned)motor_yaw_gimbal.fdb.raw_angle);
#endif
#endif
#endif
if (len > 0)
云台/Application/Task/Src/gimbal_task.c
+32 -4
View File
@@ -1,14 +1,14 @@
/* =============================================================================
* gimbal_task.c - 云台控制任务(2ms)
* gimbal_task.c - 云台控制任务(2ms/500Hz)
* 状态机:
* YAW_WAIT 等待"姿态就绪+云台电机在线"(遥控可后到)
* YAW_RUN 正常串级控制(符号用参数回退值,直至手势自检完成)
* YAW_DETECT 装配符号自检——**仅由操作手手势显式触发,绝不自动执行**:
* 遥控在线时"左摇杆推到最左 + 右摇杆推到最右"保持 0.5s。
* 检测期间云台会轻转几度(约 20% 电压脉冲 60ms),操作手应
* 检测期间云台会轻转几度(约 20% 电流脉冲 60ms),操作手应
* 确认云台周围无人后再做手势。失败重试 3 次后回退参数符号。
* 任意门控失效(遥控离线/电机掉线/姿态不可用/底盘故障)立即清零输出
* 拨弹电流由 shoot_task 写入共享变量,本任务与 Pitch 共帧发送(0x1FF CAN1)
* Yaw/Pitch GM6020 采用 0x1FE 电流帧控制;拨弹 M2006 由 shoot_task 独立发 0x200
* ========================================================================== */
#include "app_tasks.h"
#include "cmsis_os.h"
@@ -26,7 +26,7 @@
#define CALIB_GESTURE_L_RL 400 // < 400 即最左
#define CALIB_GESTURE_R_RL 1600 // > 1600 即最右
#define CALIB_GESTURE_MS 500 // 保持时长
#define CALIB_GESTURE_TICKS (CALIB_GESTURE_MS / 2) // 2ms 任务
#define CALIB_GESTURE_TICKS (CALIB_GESTURE_MS / 2) // 2ms 任务(500Hz)
typedef enum
{
@@ -64,6 +64,34 @@ void gimbal_task(void const * argument)
if (gesture)
gesture_cnt = 0;
#if 0
/* ===== 2026-10-15 台架 Pitch 阶跃发生器(已停用,保留备查) =====
* **有界**测试,不是持续抖动:只跑 GIMBAL_BENCH_PITCH_HALF_COUNT 个半周期,
* 跑完自动归零并锁存,之后云台恢复静止(重新上电/改开关才会再跑一次)。
* 配合 gimbal.c 的台架偏置使用;2ms 任务,半周期 tick 数 = HALF_MS / 2 */
{
static uint32_t bench_phase = 0;
static uint8_t bench_done = 0;
const uint32_t half_ticks = (uint32_t)GIMBAL_BENCH_PITCH_HALF_MS / 2u;
if (!bench_done && half_ticks > 0u)
{
const uint32_t total_ticks = half_ticks * (uint32_t)GIMBAL_BENCH_PITCH_HALF_COUNT;
if (bench_phase >= total_ticks)
{
bench_done = 1;
gimbal_bench_pitch_offset = 0.0f; /* 跑完立即停,不再抖动 */
}
else
{
gimbal_bench_pitch_offset = ((bench_phase / half_ticks) % 2u)
? GIMBAL_BENCH_PITCH_STEP_DEG
: 0.0f;
bench_phase++;
}
}
}
#endif
switch (state)
{
case YAW_WAIT:
云台/Application/Task/Src/monitor_task.c
+2 -2
View File
@@ -85,8 +85,8 @@ static int8_t linkcheck_first_offline(void)
{
uint32_t now = HAL_GetTick();
#if defined(ROBOT_TYPE_GIMBAL)
/* 设备序号:0 摩擦轮L(0x201) 1 摩擦轮R(0x202) 2 Pitch(0x206)
* 3 Yaw(0x205) 4 拨弹(0x207,安装时) 5 底盘回传(0x019) */
/* 设备序号:0 摩擦轮L(CAN1 0x201) 1 摩擦轮R(CAN1 0x202) 2 Pitch(CAN1 0x206)
* 3 Yaw(CAN2 0x205) 4 拨弹(CAN2 0x201,安装时) 5 底盘回传(0x019) */
if (LINK_OFFLINE(motor_friction_l.fdb.last_online_tick))
return 0;
if (LINK_OFFLINE(motor_friction_r.fdb.last_online_tick))
云台/Application/Task/Src/robot_cmd_task.c
+102 -19
View File
@@ -1,6 +1,6 @@
/* =============================================================================
* robot_cmd_task.c - 控制源汇总(2ms),发布 cmd_robot_t(robot_typedef.h)
* 云台板: DR16 遥控器 + 图传键鼠(0x0304,referee 键盘钩子填充 keyboard_data)
* 云台板: DR16 遥控器 + 键鼠(0x0304 优先;USART3 的 18 字节帧里同样带键鼠,两路已合并,见 KB_FROM_DBUS_FRAME)
* 键鼠/遥控互斥(与 legacy 一致);摇杆->云台增量与限位门控;
* Q 摩擦轮/左键发射/E 退弹/拨轮;首帧触发 gimbal_reset
* 底盘板: 从 ctoc_remote(0x149/0x189 解析结果)生成:
@@ -31,6 +31,9 @@ volatile cmd_robot_t cmd_robot;
#if defined(ROBOT_TYPE_GIMBAL)
keyboard_data_t keyboard_data;
/* 键鼠来源合并视图(声明见 robot_cmd_task.h):云台控制与 c_comm_task 底盘摇杆合成共用 */
keyboard_data_t keyboard_merged;
uint8_t keyboard_merged_online = 0;
static uint8_t keyboard_online = 0;
void dr16_frame_callback(const uint8_t * frame, uint16_t len)
@@ -74,6 +77,15 @@ static void referee_keyboard_hook(const uint8_t data[12])
keyboard_data.last_tick = HAL_GetTick();
}
/* ---- 键鼠输入来源(2026-10-16 修) ----
* 背景:客户端键鼠是从 USART3 那 18 字节帧进来的(data[6..15]),dr16_parse 早就
* 解析进 dr16.mouse_rl / dr16.key_w 等字段,但控制逻辑只读 0x0304 填的
* keyboard_data,于是"键鼠控制完全没用"。此开关让两路合并。
* 1 = 除 0x0304 外同时接受帧内键鼠:见到键鼠动作即进入键鼠模式并保持,
* 直到操作手去动云台左摇杆才交还遥控器(右摇杆在底盘,键鼠模式下仍要能用)。
* 0 = 旧行为:只有 0x0304 在线才走键鼠。 */
#define KB_FROM_DBUS_FRAME 1
void robot_cmd_task(void const * argument)
{
referee_set_keyboard_hook(referee_keyboard_hook);
@@ -81,13 +93,80 @@ void robot_cmd_task(void const * argument)
while (!app_ready)
osDelay(2);
/* 键鼠模式状态:帧内键鼠动作置 1,左摇杆动作清 0 */
static uint8_t kb_mode = 0;
for (;;)
{
keyboard_online = (keyboard_data.last_tick != 0 &&
HAL_GetTick() - keyboard_data.last_tick < DEVICE_OFFLINE_TIME_MS * 10);
#if KB_FROM_DBUS_FRAME
{
uint8_t kb_act = 0, rc_act = 0;
/* 键鼠动作:鼠标移动 / 滚轮 / 左右键 / 任意按键(data[14]或data[15]非 0) */
if (dr16.mouse_rl > 1 || dr16.mouse_rl < -1) kb_act = 1;
if (dr16.mouse_du > 1 || dr16.mouse_du < -1) kb_act = 1;
if (dr16.mouse_wheel != 0) kb_act = 1;
if (dr16.mouse_key_l || dr16.mouse_key_r) kb_act = 1;
if (dr16.key_code_lo || dr16.key_code_hi) kb_act = 1;
/* 遥控器动作:只认云台左摇杆 */
if (dr16.rc_l_UD > 1050 || dr16.rc_l_UD < 1000) rc_act = 1;
if (dr16.rc_l_RL > 1050 || dr16.rc_l_RL < 1000) rc_act = 1;
if (kb_act) kb_mode = 1;
if (rc_act) kb_mode = 0;
}
#endif
/* 是否键鼠在控:0x0304 在线时始终算键鼠(保持原有优先级) */
uint8_t kb_active = (keyboard_online || kb_mode) ? 1 : 0;
/* ---- 合并成共享视图 keyboard_merged ----
* 0x0304 在线 → 整份用 keyboard_data;否则用 USART3 帧里那一套。
* 云台控制、发射机构、以及 c_comm_task 里 WASD→底盘摇杆的合成都读这个
* 视图,避免两处各判一次导致"云台跟鼠标了、底盘却还在收遥控器原始摇杆"。 */
if (keyboard_online)
{
keyboard_merged = keyboard_data;
}
else
{
keyboard_merged.mouse_rl = dr16.mouse_rl;
keyboard_merged.mouse_du = dr16.mouse_du;
keyboard_merged.mouse_wheel = dr16.mouse_wheel;
keyboard_merged.mouse_key_l = dr16.mouse_key_l;
keyboard_merged.mouse_key_r = dr16.mouse_key_r;
keyboard_merged.key_w = dr16.key_w;
keyboard_merged.key_s = dr16.key_s;
keyboard_merged.key_a = dr16.key_a;
keyboard_merged.key_d = dr16.key_d;
keyboard_merged.key_shift = dr16.key_shift;
keyboard_merged.key_ctrl = dr16.key_ctrl;
keyboard_merged.key_q = dr16.key_q;
keyboard_merged.key_e = dr16.key_e;
/* alpha 键:dr16 侧那两位恒为 0(见 dr16.c 的 >>9/>>10),照搬保持语义 */
keyboard_merged.key_alpha1 = dr16.key_alpha1;
keyboard_merged.key_alpha2 = dr16.key_alpha2;
keyboard_merged.key_push_q = dr16.key_push_q;
keyboard_merged.key_push_e = dr16.key_push_e;
keyboard_merged.key_push_shift = dr16.key_push_shift;
keyboard_merged.key_push_ctrl = dr16.key_push_ctrl;
keyboard_merged.last_tick = dr16_last_tick;
}
keyboard_merged_online = kb_active;
/* 控制逻辑用的简写(取自共享视图) */
int16_t kb_mouse_rl = keyboard_merged.mouse_rl;
int16_t kb_mouse_du = keyboard_merged.mouse_du;
uint8_t kb_mouse_l = keyboard_merged.mouse_key_l;
uint8_t kb_push_q = keyboard_merged.key_push_q;
uint8_t kb_push_e = keyboard_merged.key_push_e;
cmd_robot.online = (dr16_status == 1 && !dr16_offline());
cmd_robot.source = keyboard_online ? 1 : 0;
cmd_robot.source = kb_active ? 1 : 0;
if (cmd_robot.online)
{
@@ -95,10 +174,10 @@ void robot_cmd_task(void const * argument)
float yaw_delta = 0, pitch_delta = 0;
uint16_t pos = motor_pitch_gimbal.fdb.raw_angle;
if (!keyboard_online)
if (!kb_active)
{
/* 遥控器:左摇杆,输出与摇杆偏量成比例(legacy 为过死区即全速,
* 体感过灵敏),限位门控与方向保持 legacy */
/* 遥控器:左摇杆向上(>1050)为抬头(pitch_delta减小,pos向2260减小),门控须 pos > UPPER_LIMIT(2260);
* 左摇杆向下(<1000)为低头(pitch_delta增大,pos向3950增大),门控须 pos < LOWER_LIMIT(3950) */
if (dr16.rc_l_UD > 1050 && pos > PITCH_GM6020_POSITION_UPPER_LIMIT)
pitch_delta -= GIMBAL_PITCH_LEVER_RATE / 8192.0f * 360.0f *
((float)dr16.rc_l_UD - 1024.0f) / 660.0f;
@@ -113,24 +192,27 @@ void robot_cmd_task(void const * argument)
}
else
{
/* 键鼠:同改为比例输出 */
if (keyboard_data.mouse_du < -8 && pos > PITCH_GM6020_POSITION_UPPER_LIMIT)
/* 键鼠:鼠标前推(>8)为抬头(pitch_delta减小),门控须 pos > UPPER_LIMIT;鼠标后拉(<-8)为低头(pitch_delta增大),门控须 pos < LOWER_LIMIT */
if (kb_mouse_du > 8 && pos > PITCH_GM6020_POSITION_UPPER_LIMIT)
pitch_delta -= GIMBAL_PITCH_LEVER_RATE / 8192.0f * 360.0f *
(-(float)keyboard_data.mouse_du * PC_MOUSE_DU_SENSITIVITY) / 660.0f;
else if (keyboard_data.mouse_du > 8 && pos < PITCH_GM6020_POSITION_LOWER_LIMIT)
((float)kb_mouse_du * PC_MOUSE_DU_SENSITIVITY) / 660.0f;
else if (kb_mouse_du < -8 && pos < PITCH_GM6020_POSITION_LOWER_LIMIT)
pitch_delta += GIMBAL_PITCH_LEVER_RATE / 8192.0f * 360.0f *
((float)keyboard_data.mouse_du * PC_MOUSE_DU_SENSITIVITY) / 660.0f;
(-(float)kb_mouse_du * PC_MOUSE_DU_SENSITIVITY) / 660.0f;
if (keyboard_data.mouse_rl != 0)
if (kb_mouse_rl != 0)
yaw_delta -= GIMBAL_LEVER_SPEED_MAP_RATE * GIMBAL_YAW_PITCH_SPEED_RATE *
GIMBAL_YAW_PITCH_SPEED_RATE * 0.0439453125f *
((float)keyboard_data.mouse_rl * PC_MOUSE_RL_SENSITIVITY / 660.0f * 2.0f);
((float)kb_mouse_rl * PC_MOUSE_RL_SENSITIVITY / 660.0f * 2.0f);
}
cmd_robot.gimbal_yaw_delta = yaw_delta;
cmd_robot.gimbal_pitch_delta = pitch_delta;
/* ---- 发射机构 ---- */
if (!keyboard_online)
/* ---- 发射机构 ----
* 键鼠模式用 Q / 鼠标左键 / E(两路来源已合并进 kb_*,0x0304 优先);
* 遥控模式用 S1 与拨轮。kb_push_* 是"按下翻转"的常驻状态,
* 且键鼠模式只在动左摇杆时才退出,所以摩擦轮/E 的状态不会自己掉。 */
if (!kb_active)
{
cmd_robot.friction_on = (dr16.s1 == 1);
cmd_robot.fire = (dr16.thumb_wheel < 1000);
@@ -138,9 +220,9 @@ void robot_cmd_task(void const * argument)
}
else
{
cmd_robot.friction_on = keyboard_data.key_push_q;
cmd_robot.fire = keyboard_data.mouse_key_l;
cmd_robot.eject = keyboard_data.key_push_e;
cmd_robot.friction_on = kb_push_q;
cmd_robot.fire = kb_mouse_l;
cmd_robot.eject = kb_push_e;
}
cmd_robot.thumb_wheel = dr16.thumb_wheel;
}
@@ -153,12 +235,13 @@ void robot_cmd_task(void const * argument)
cmd_robot.eject = 0;
}
/* 小陀螺使能:Ctrl 沿翻转(仅在遥控源检测,键鼠 TODO);
/* 小陀螺使能:Ctrl 沿翻转。键鼠模式下取键鼠那一路的 Ctrl(0x0304 的
* keyboard_data 或帧内 dr16.key_push_ctrl),遥控模式用遥控器 Ctrl。
* 云台侧是数据源头,底盘只收状态位——重连瞬间保持态跳变不会在
* 底盘误触发沿(修复"重连误开小陀螺疯转") */
{
static uint8_t spin_flag = 0, last_ctrl = 0;
uint8_t ctrl_now = (!keyboard_online) ? dr16.key_push_ctrl : 0;
uint8_t ctrl_now = keyboard_online ? keyboard_data.key_push_ctrl : dr16.key_push_ctrl;
if (last_ctrl == 0 && ctrl_now == 1)
spin_flag = !spin_flag;
last_ctrl = ctrl_now;
云台/Application/Task/Src/shoot_task.c
+2 -2
View File
@@ -1,7 +1,7 @@
/* =============================================================================
* shoot_task.c - 发射机构任务(2ms)
* shoot_control() 计算摩擦轮/拨弹电流 -> shoot_send_cmd() 发 0x200;
* 拨弹电流由云台任务与 Pitch 共帧发送;发射机构上电状态来自底盘 0x019
* shoot_control() 计算摩擦轮/拨弹电流 -> shoot_send_cmd() 发 0x200(CAN1 摩擦轮 / CAN2 拨弹);
* 发射机构上电状态来自底盘 0x019
* ========================================================================== */
#include "app_tasks.h"
#include "cmsis_os.h"
云台/Application/robot_param.h
+84 -23
View File
@@ -9,9 +9,11 @@
#define ROBOT_PARAM_H
/* ============================ 云台 ============================ */
#define PITCH_GM6020_POSITION_LOWER_LIMIT 3990 // Pitch 轴编码器值下限(云台抬起方向)
#define PITCH_GM6020_POSITION_UPPER_LIMIT 2220 // Pitch 轴编码器值上限(云台压低方向)
#define PITCH_GM6020_ENCODER_ZERO 3245 // Pitch 轴编码器零位
#define PITCH_GM6020_POSITION_UPPER_LIMIT 2260 // Pitch 轴抬起极限(最高位,编码器较小值;实测2203撞死限位,留余量设2260)
#define PITCH_GM6020_POSITION_LOWER_LIMIT 3950 // Pitch 轴压低极限(最低位,编码器较大值;实测4234撞死限位,留余量设3950)
#define PITCH_GM6020_ENCODER_ZERO 3200 // Pitch 轴编码器水平零位
#define YAW_GM6020_ENCODER_ZERO 7730 // Yaw 轴编码器零位(机械正前方,0~8191)
#define CHASSIS_SPIN_FEEDFORWARD_K 0.008f // 小陀螺解算时延前馈补偿系数(s)
#define GIMBAL_FRICTION_WHEEL_SPEED 5500.0f // 摩擦轮转速(RPM)
#define GIMBAL_RAMMER_SPEED -5400.0f// 拨弹盘转速(RPM,负向发射)
@@ -29,35 +31,58 @@
* 这是反复"疯转"的根源,已废弃;
* - 现在两环共用陀螺,整条链只有一个装配符号,由上电自检自动测定
* (GIMBAL_YAW_DETECT 见下),无需人工猜;
* - 单位:角度环 误差° -> 目标角速度°/s;速度环 误差°/s -> 电压。
* - 单位:角度环 误差° -> 目标角速度°/s;速度环 误差°/s -> 电流。
* 调参顺序:先速度环(点动不振荡),再位置环(刚性)——见移植 README §8.1 */
#define GIMBAL_YAW_ANGLE_KP 15.0f // ° -> °/s:10° 误差给 150°/s
#define GIMBAL_YAW_ANGLE_KP 20.0f // ° -> °/s:10° 误差给 150°/s
#define GIMBAL_YAW_ANGLE_KI 0.0f
#define GIMBAL_YAW_ANGLE_KD 0.0f // 速度环本身即微分,不再叠加
#define GIMBAL_YAW_ANGLE_EK_DEADBAND 0.05f // 误差死区(°),QEKF 噪声小可用窄死区
#define GIMBAL_YAW_ANGLE_OUT_LIMIT 360.0f // 目标角速度上限(°/s)
#define GIMBAL_YAW_SPEED_KP 60.0f // °/s -> 电压:100°/s 误差给 6000(约 24% 满电压)
#define GIMBAL_YAW_SPEED_KP 85.0f // °/s -> 电流:100°/s 误差给 6000(约 36% 满电流)
#define GIMBAL_YAW_SPEED_KI 0.0f // 稳定后可回填 0.5~2 消速度稳态差
#define GIMBAL_YAW_SPEED_KD 0.0f // 陀螺速率反馈噪声小,先不用 D
#define GIMBAL_YAW_SPEED_OUT_LIMIT 25000.0f// GM6020 电压限幅
#define GIMBAL_YAW_SPEED_OUT_LIMIT 16384.0f// GM6020 电流限幅(±16384 对应 ±3A)
#define GIMBAL_YAW_SPIN_FEEDFORWARD_K 24.0f // 小陀螺底盘自旋解耦前馈系数(RPM->电流)
/* Yaw 装配符号自动检测:上电自检时给 Yaw 电机一个正向小电压脉冲,
/* Yaw 装配符号自动检测:上电自检时给 Yaw 电机一个正向小电流脉冲,
* 看陀螺 z 轴往哪边转——脉冲引起同向转动则符号 +1,反向则 -1。
* 检测时云台会轻转几度,勿扶云台;失败(被按住/电机离线)时用 FALLBACK */
#define GIMBAL_YAW_SIGN_AUTO 1 // 1=上电自动检测 0=直接用 FALLBACK
#define GIMBAL_YAW_SIGN_FALLBACK (1.0f)
#define GIMBAL_YAW_DETECT_VOLTAGE 5000 // 检测脉冲电压(约 20% 满电压)
#define GIMBAL_YAW_DETECT_CURRENT 3500 // 检测脉冲电流(约 21% 满电流 16384)
#define GIMBAL_YAW_DETECT_RATE_MIN 20.0f // 判定转动的陀螺速率阈值(°/s)
/* ---- Pitch(位置环陀螺 Roll,速度环转子转速——Pitch 无符号史问题,维持原案) ---- */
#define GIMBAL_PITCH_ANGLE_EK_DEADBAND 0.3f // 位置环误差死区(°)
#define GIMBAL_PITCH_ANGLE_EK_DEADBAND 0.05f // 误差死区(°),收窄死区消除边缘阶跃
#define GIMBAL_PITCH_ANGLE_KP 15.0f
#define GIMBAL_PITCH_ANGLE_KI 0.0f
#define GIMBAL_PITCH_ANGLE_KD 100.0f
#define GIMBAL_PITCH_SPEED_KP 150.0f
#define GIMBAL_PITCH_SPEED_KI 0.001f
#define GIMBAL_PITCH_SPEED_KD 5.0f
#define GIMBAL_PITCH_ANGLE_KD 0.0f // 原100.0f是万级电流振颤主因!清零以消除剧烈振荡
#define GIMBAL_PITCH_SPEED_KP 40.0f // 速度/电流环Kp
#define GIMBAL_PITCH_SPEED_KI 0.0f
#define GIMBAL_PITCH_SPEED_KD 0.0f
/* Pitch 重力拟合前馈参数: I_g = K_COS * cos(a) + K_SIN * sin(a) + K_CONST
* 其中 a = (raw_angle - ZERO_ECD) * 360 / 8192 (°) */
#define GIMBAL_PITCH_GRAVITY_ZERO_ECD 3200.0f // 重力补偿拟合基准编码值
#define GIMBAL_PITCH_GRAVITY_K_COS 2856.1f// cos 项系数
#define GIMBAL_PITCH_GRAVITY_K_SIN 4340.3f// sin 项系数
#define GIMBAL_PITCH_GRAVITY_K_CONST 2826.5f // 常数偏置项
/* ---- 2026-10-15 台架前馈实测记录(未采用,保留备查) ----
* 用上位机 203Hz 遥测在编码器 -16.91°/+4.88°/+9.30° 三处长时间静止(编码器
* 零漂移+目标恒定)实测真实保持电流 3597/4498/4613 counts;当时上面这组参数
* 分别高估 699/1543/1733 counts,折合 1.17~2.89° 稳态静差
* (位置环 Kp15×Kp40 = 600 counts/°:静差 = 前馈高估量 / 600)。
* 按"保留原相位与形状(K_COS:K_SIN 不变)、幅值×0.503 并微调常数项"重标定为:
* GIMBAL_PITCH_GRAVITY_K_COS 1435.4f
* GIMBAL_PITCH_GRAVITY_K_SIN 2181.3f
* GIMBAL_PITCH_GRAVITY_K_CONST 2861.6f
* 该组在当次数据上残差 RMS 16 counts(0.03°),看似很准;**但换到另一机械状态后
* 同一编码器角度实测保持电流又差约 1650 counts**,说明被标定对象本身在变
* (见上方"机械滞回 2130 counts"记录),故不采用,前馈保持原值不动。
* 另一并记录:PID 动态特性实测良好(上升时间 0.095~0.14s、超调 0.3~5.2%、
* 16s 稳态段纹波 p-p 0.046°、无振荡),故 GIMBAL_PITCH_*_KP/KI/KD 也未改动。 */
#define GIMBAL_FRICTION_WHEEL_KP 16.0f
#define GIMBAL_FRICTION_WHEEL_KI 0.0f
@@ -91,10 +116,10 @@
* err = wrap180(云台yaw - 底盘yaw)
* 不再依赖底盘侧 GM6020(0x205) 反馈,皮带虚位不在环内,无基准锁定时序坑。
* 两板 INS 各自上电零点任意,但差值只随相对转动变化,天然正确 */
#define CHASSIS_FOLLOW_KP 0.4f // w 量纲/°:10° 偏差给 w=4
#define CHASSIS_FOLLOW_KP 0.4678f // w 量纲/°:10° 偏差给 w=4
#define CHASSIS_FOLLOW_KI 0.0f // 调试期 0,同旧教训(积分残留)
#define CHASSIS_FOLLOW_KD 0.0f
#define CHASSIS_FOLLOW_OUT_LIMIT 4.0f // 输出限幅(介于慢/快陀螺之间)
#define CHASSIS_FOLLOW_KD 24.452f
#define CHASSIS_FOLLOW_OUT_LIMIT 5.5f // 输出限幅(介于慢/快陀螺之间)
#define CHASSIS_FOLLOW_DEADBAND 1.0f // 误差死区(°)
/* 跟随符号全自动综合:云台自检(0x1A9 flags)下发编码器 tick 增向,
@@ -114,10 +139,11 @@
#define CTOC_SLAVE_ID1 0x149 // 云台->底盘:摇杆数据
#define CTOC_SLAVE_ID2 0x189 // 云台->底盘:控制状态+故障/陀螺使能位
#define CTOC_SLAVE_ID3 0x1A9 // 云台->底盘:云台世界系 yaw(float)+att_ready
#define CTOC_SLAVE_ID4 0x1B9 // 云台->底盘:自定义UI 专用(pitch + 摩擦轮 L/R 转速)
/* ============================ CAN ID ============================ */
/* 云台板:CAN1 = Pitch GM6020(0x206)+摩擦轮 M3508(0x201/0x202)
* CAN2 = Yaw GM6020(0x205)+底盘回传(0x019)
/* 云台板:CAN1 = Pitch GM6020(0x206,0x1FE)+摩擦轮 M3508(0x201/0x202,0x200)
* CAN2 = Yaw GM6020(0x205,0x1FE)+拨弹 M2006(0x201,0x200)+底盘回传(0x019)
* 底盘板:CAN1 = 四轮 M3508(0x201~0x204)
* CAN2 = 云台数据(0x149/0x189/0x1A9) */
@@ -125,10 +151,45 @@
#define DEBUG_SHOOT_WITHOUT_REFEREE 1 // 1=无裁判系统时也允许开摩擦轮(台架调试用),比赛请改 0
#define GIMBAL_RAMMER_INSTALLED 0 // 1=拨弹 M2006 已安装;0=暂缺,不参与掉线判定
/* 1=调试模式:把 CAN 掉线警告音替换成循环播放的旋律(台架调试时避免连续滴滴声
* 干扰)。红灯常亮与其它灯语完全不变,仍能看出是哪台设备掉线;比赛请改 0。
* 旋律音符表见 modules/BUZZER/buzzer.c 的 buzzer_melody[] */
#define DEBUG_BUZZER_MELODY 1
/* ================= 2026-10-15 Pitch 台架 PID 调参改动(已停用,保留备查) =================
* 以下开关是一次台架 Pitch 调参试验所加,已用 #if 0 停用:不参与编译、不影响现有行为。
* 需要复现时把外层 #if 0 改成 #if 1,并同步启用 gimbal.c / gimbal_task.c / gimbal.h
* / debug_task.c 里同名的停用块。
* 启用前务必先确认机械无卡滞:当时实测**同一编码器角度下保持电流可差 2130 counts
* (≈3.55° 当量)**,属机械滞回(线缆拖拽/接触/摩擦),不是控制问题;机械不一致时
* 任何固定前馈都标不准,调参也无意义。 */
#if 0
/* ---- Pitch 台架 PID 调参(仅台架;调完/比赛必须置 0) ----
* 1=在 Pitch 位置环设定值上叠加一个方波阶跃,用于定量观测阶跃响应。
* 安全约束(务必遵守):
* - **有界**:只跑 GIMBAL_BENCH_PITCH_HALF_COUNT 个半周期就自动归零停住,
* 不做长时间连续抖动;
* - **限位内**:轴距上下软限位不足 GIMBAL_BENCH_PITCH_SAFE_MARGIN_DEG 时
* 不施加阶跃,绝不把轴推向限位;
* - 该偏置是纯附加量,不累加进 pitch_target_deg,关掉即完全恢复原行为。 */
#define GIMBAL_BENCH_PITCH_TUNE 0
#define GIMBAL_BENCH_PITCH_STEP_DEG 3.0f // 阶跃幅值(°)
#define GIMBAL_BENCH_PITCH_HALF_MS 800 // 半周期(ms),(跑完自动停,非持续抖动)
#define GIMBAL_BENCH_PITCH_HALF_COUNT 4 // 总半周期数:4×0.8s=3.2s 后自动静止
#define GIMBAL_BENCH_PITCH_SAFE_MARGIN_DEG 5.0f // 距上下限位至少留这么多才允许阶跃
/* Pitch 软限位外的电流限制(方向 + 堵转双层保护):
* - 压向限位的方向一律清零(绝不顶限位);
* - 离开限位的方向允许 GIMBAL_PITCH_LIMIT_CURRENT_RECOVER,让轴能自行归位
* (烧录/上电会短暂失力矩,轴会掉到限位,必须能自己爬起来);
* - 但限位外若连续 GIMBAL_PITCH_LIMIT_STALL_MS 编码器一动不动,判为堵转/
* 撞死,允许电流降到 GIMBAL_PITCH_LIMIT_CURRENT,避免长时间过载发热。
* 轴回到软限位内后闭环自动恢复正常输出。 */
#define GIMBAL_PITCH_LIMIT_CURRENT_RECOVER 12000.0f // 限位外抬升方向允许电流(≈2.2A,额定3A的73%)
#define GIMBAL_PITCH_LIMIT_CURRENT 1500.0f // 限位外判定堵转后的涓流上限(≈0.27A)
#define GIMBAL_PITCH_LIMIT_STALL_MS 300 // 限位外不动多久判定堵转(高位电流只持续这么久)
#endif
/* ================= 以上为停用块,以下为原有代码 ================= */
/* 1=把 CAN 掉线警告音替换成循环播放的旋律《你》(RM动画片尾曲),报警时播放;
* 旋律音符表见 modules/dev/buzzer.c 的 buzzer_melody[] */
#define DEBUG_BUZZER_MELODY 0
#define BUZZER_MELODY_SPEED_DIV 1 // 旋律降速分频(默认1:每步100ms精准匹配原版带吐音断音节拍)
/* ============================ 掉线检测 ============================ */
#define DEVICE_OFFLINE_TIME_MS 100 // CAN 设备/裁判系统掉线判定时间
云台/MDK-ARM/Simba-ELCT-FrameWork.uvoptx
+8 -3
View File
@@ -114,9 +114,14 @@
<tDlgDll></tDlgDll>
<tDlgPa></tDlgPa>
<tIfile></tIfile>
<pMon>BIN\CMSIS_AGDI.dll</pMon>
<pMon>Segger\JL2CM3.dll</pMon>
</DebugOpt>
<TargetDriverDllRegistry>
<SetRegEntry>
<Number>0</Number>
<Key>JL2CM3</Key>
<Name>-U20090928 -O78 -S2 -ZTIFSpeedSel5000 -A0 -C0 -JU1 -JI127.0.0.1 -JP0 -RST0 -N00("ARM CoreSight SW-DP") -D00(2BA01477) -L00(0) -TO18 -TC10000000 -TP21 -TDS8007 -TDT0 -TDC1F -TIEFFFFFFFF -TIP8 -TB1 -TFE0 -FO7 -FD20000000 -FC1000 -FN1 -FF0STM32F4xx_1024.FLM -FS08000000 -FL0100000 -FP0($$Device:STM32F407IGHx$CMSIS\Flash\STM32F4xx_1024.FLM)</Name>
</SetRegEntry>
<SetRegEntry>
<Number>0</Number>
<Key>ARMRTXEVENTFLAGS</Key>
@@ -140,7 +145,7 @@
<SetRegEntry>
<Number>0</Number>
<Key>CMSIS_AGDI</Key>
<Name>-X"" -O206 -S8 -C0 -P00000000 -N00("ARM CoreSight SW-DP") -D00(2BA01477) -L00(0) -TO65554 -TC10000000 -TT10000000 -TP20 -TDS8007 -TDT0 -TDC1F -TIEFFFFFFFF -TIP8 -FO15 -FD20000000 -FC1000 -FN1 -FF0STM32F4xx_1024.FLM -FS08000000 -FL0100000 -FP0($$Device:STM32F407IGHx$CMSIS\Flash\STM32F4xx_1024.FLM)</Name>
<Name>-X"Any" -UAny -O206 -S8 -C0 -P00000000 -N00("") -D00(00000000) -L00(0) -TO65554 -TC10000000 -TT10000000 -TP20 -TDS8007 -TDT0 -TDC1F -TIEFFFFFFFF -TIP8 -FO15 -FD20000000 -FC1000 -FN1 -FF0STM32F4xx_1024.FLM -FS08000000 -FL0100000 -FP0($$Device:STM32F407IGHx$CMSIS\Flash\STM32F4xx_1024.FLM)</Name>
</SetRegEntry>
<SetRegEntry>
<Number>0</Number>
@@ -1040,7 +1045,7 @@
<Group>
<GroupName>Application/Task</GroupName>
<tvExp>1</tvExp>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
<cbSel>0</cbSel>
<RteFlg>0</RteFlg>
云台/README.md
+5 -5
View File
@@ -8,8 +8,8 @@
## 这块板负责什么
- **云台控制**:Yaw(GM6020 `0x205`,CAN2)/ Pitch(GM6020 `0x206`,CAN1)双环
- **发射机构**:摩擦轮 M3508 `0x201`/`0x202` + 拨弹 M2006 `0x207`(装与不装由 `GIMBAL_RAMMER_INSTALLED` 决定)
- **云台控制**:Yaw(GM6020 `0x205`,CAN2 `0x1FE`电流控制)/ Pitch(GM6020 `0x206`,CAN1 `0x1FE`电流控制)双环
- **发射机构**:摩擦轮 M3508 `0x201`/`0x202`(CAN1 `0x200`) + 拨弹 M2006 `0x201`(CAN2 `0x200`)(装与不装由 `GIMBAL_RAMMER_INSTALLED` 决定)
- **图传链路 / 裁判系统**:USART6(3pin 口)
- **DR16 遥控器**:USART3
- **板间通讯主控**:云台把世界系 yaw(`0x1A9`)与摇杆/控制状态(`0x149`/`0x189`)发给底盘
@@ -38,7 +38,7 @@ USE_HAL_DRIVER, STM32F407xx, ARM_MATH_CM4, ROBOT_TYPE_GIMBAL
1. `led_init` 点亮蓝灯 → 各外设初始化
2. IMU 初始化 + **z 轴零偏静止标定(约 0.5~1.5 s,这段时间别碰车)**
3. **Yaw 装配符号自检**:给 Yaw 电机一个正向小电压脉冲,看陀螺 z 轴往哪边转,自动定符号;**云台会轻转几度,不要扶住云台**。失败(被按住 / 电机离线)时回退到 `GIMBAL_YAW_SIGN_FALLBACK`
3. **Yaw 装配符号自检**:给 Yaw 电机一个正向小电流脉冲,看陀螺 z 轴往哪边转,自动定符号;**云台会轻转几度,不要扶住云台**。失败(被按住 / 电机离线)时回退到 `GIMBAL_YAW_SIGN_FALLBACK`
4. 自检结果经 `0x1A9` 的 flags 下发给底盘,与底盘自测的车身转向相乘完成跟随符号综合
## 蜂鸣器序号(本板)
@@ -46,8 +46,8 @@ USE_HAL_DRIVER, STM32F407xx, ARM_MATH_CM4, ROBOT_TYPE_GIMBAL
CAN 掉线报警按设备序号响 `n` 下:
```
0 = 摩擦轮L(0x201) 1 = 摩擦轮R(0x202) 2 = Pitch(0x206)
3 = Yaw(0x205) 4 = 拨弹(0x207) 5 = 底盘回传(0x019)
0 = 摩擦轮L(CAN1 0x201) 1 = 摩擦轮R(CAN1 0x202) 2 = Pitch(CAN1 0x206)
3 = Yaw(CAN2 0x205) 4 = 拨弹(CAN2 0x201) 5 = 底盘回传(0x019)
```
**响三下 = Pitch 电机掉线。** 台架调试嫌吵时把 `robot_param.h` 的 `DEBUG_BUZZER_MELODY` 置 1(只换声音不换灯语)。
云台/modules/comms/c_comm.c
+20
View File
@@ -136,6 +136,26 @@ void c_comm_master_send(uint8_t keyboard_online, const uint8_t kb[12], uint8_t m
c_comm_send_frame(&hcan2, CTOC_SLAVE_ID2, data);
}
/* 0x1B9 云台->底盘:自定义UI 专用量(底盘本地没有,见 referee_ui)
* [0..1] pitch(0.01°) [2..3] 左摩擦轮(rpm/100) [4..5] 右摩擦轮(rpm/100)
* [6] bit0=小陀螺使能 */
void c_comm_master_send_ui(float pitch_deg, float fric_l_rpm, float fric_r_rpm, uint8_t spin_on)
{
uint8_t data[8] = {0};
int16_t p = (int16_t)(pitch_deg * 100.0f);
int16_t fl = (int16_t)(fric_l_rpm / 100.0f);
int16_t fr = (int16_t)(fric_r_rpm / 100.0f);
data[0] = (uint8_t)(p & 0xFF);
data[1] = (uint8_t)((uint16_t)p >> 8);
data[2] = (uint8_t)(fl & 0xFF);
data[3] = (uint8_t)((uint16_t)fl >> 8);
data[4] = (uint8_t)(fr & 0xFF);
data[5] = (uint8_t)((uint16_t)fr >> 8);
data[6] = spin_on ? 0x01 : 0;
c_comm_send_frame(&hcan2, CTOC_SLAVE_ID4, data);
}
#elif defined(ROBOT_TYPE_CHASSIS)
/* ============================ 底盘板(从机) ============================ */
云台/modules/comms/c_comm.h
+5
View File
@@ -63,6 +63,11 @@ extern volatile int8_t ctoc_encoder_ccw;
/* 底盘板:0x1A9 帧是否新鲜(掉线检测) */
extern uint8_t ctoc_att_fresh(void);
/* ---- 0x1B9 云台->底盘:自定义UI 专用数据 ---------------------------------
* 底盘本地没有、但裁判系统自定义UI 需要的量(见 底盘/modules/comms/referee_ui):
* pitch 角度与左右摩擦轮转速。接收侧解析见底盘 c_comm.c(c_comm_rx_0x1b9)。 */
extern void c_comm_master_send_ui(float pitch_deg, float fric_l_rpm, float fric_r_rpm, uint8_t spin_on);
/* 注册 CAN 接收回调(can_start() 之后调用) */
extern void c_comm_init(void);
云台/modules/comms/dr16.c
+6
View File
@@ -48,6 +48,12 @@ void dr16_parse(const uint8_t * data)
dr16.key_alpha1 = (data[14] >> 9) & 0x01;
dr16.key_alpha2 = (data[14] >> 10) & 0x01;
/* 原始按键字节。注意 data[14] 是 uint8_t:上面两条 >>9/>>10 恒为 0
* (整型提升后 byte 值 <256,右移 9 位必然为 0),即 alpha 键从未被真正解析。
* 官方 16 位 key_code 的高字节在 data[15],这里先原样存下来供诊断/后续解析。 */
dr16.key_code_lo = data[14];
dr16.key_code_hi = data[15];
dr16.thumb_wheel = (int16_t)(((uint16_t)data[17] << 8) | data[16]); // B[120:135]
/* 按键边沿检测(legacy 语义:Q/E/Shift/Ctrl 按下翻转,鼠标右键按下瞬间置 1) */
云台/modules/comms/dr16.h
+7
View File
@@ -37,6 +37,13 @@ typedef struct
uint8_t key_alpha1; // 图传扩展键
uint8_t key_alpha2;
/* 原始按键字节(诊断用,不做位拆分) —— 用来判断"帧里到底有没有键鼠数据":
* 官方 dbus.h 的 key_code 是 16 位:bit0..7 = W/S/A/D/Shift/Ctrl/Q/E(=data[14]),
* bit8..15 = R/F/G/Z/X/C/V/B(=data[15])。本工程此前只读了 data[14]。
* 拨键盘时这两个字节若非 0 说明数据确实到了;全 0 说明帧里就是空的。 */
uint8_t key_code_lo; // data[14]
uint8_t key_code_hi; // data[15]
int16_t thumb_wheel; // 遥控器拨轮
/* 按键边沿检测(legacy 语义) */
云台/modules/control/gimbal.c
+174 -46
View File
@@ -2,11 +2,11 @@
* gimbal.c - 云台双轴控制(串级 PID)
* Yaw(2026-09 重写):双陀螺环,见 gimbal.h 与 robot_param.h 说明
* 位置环:err(°) = 目标角 - SIGN*att_deg_yaw -> 目标角速度(°/s,限幅)
* 速度环:err(°/s) = 目标角速度 - SIGN*gyro_z -> 电压(限幅)
* 稳定性条件:SIGN*G>0,G 为"电压->陀螺 z 角速度"的装配增益,
* 速度环:err(°/s) = 目标角速度 - SIGN*gyro_z -> 电流(限幅)
* 稳定性条件:SIGN*G>0,G 为"电流->陀螺 z 角速度"的装配增益,
* 由 gimbal_detect_yaw_sign() 上电实测,彻底消除双传感器符号打架
* Pitch:位置环用 QEKF Roll(安装方向),速度环转子转速(legacy 案,无符号史问题)
* 发送:CAN2 0x1FF 槽1=Yaw 电压;CAN1 0x1FF 槽2=Pitch 电压,槽3=拨弹电流
* 发送:CAN2 0x1FE 槽1=Yaw 电流;CAN1 0x1FE 槽2=Pitch 电流
* ========================================================================== */
#include "gimbal.h"
#include "shoot.h"
@@ -16,11 +16,18 @@
#include "can.h"
#include "robot_param.h"
#include "filter.h"
#include "robot_typedef.h"
#include "dr16.h"
#include <math.h>
#ifndef RAD_TO_ANGLE
#define RAD_TO_ANGLE 57.295779513082320876798154814105f
#endif
#ifndef ANGLE_TO_RAD
#define ANGLE_TO_RAD 0.01745329251994329576923690768489f
#endif
dji_motor_t motor_yaw_gimbal;
dji_motor_t motor_pitch_gimbal;
dji_motor_t motor_friction_l;
@@ -32,25 +39,32 @@ static PID_PositionTypeDef pitch_angle_pid, pitch_speed_pid;
static float yaw_target_deg; // 世界系目标角(°)
static float pitch_target_deg; // 目标角(°)
static float yaw_voltage;
static float pitch_voltage;
static float yaw_current;
float pitch_pid = 0.0f;
float pitch_g = 0.0f;
float pitch_current = 0.0f;
/* ===== 2026-10-15 台架调参临时量(已停用,保留备查) ===== */
#if 0
/* 台架调参用 Pitch 目标角附加偏置(°)。由 gimbal_task 的方波发生器写入,
* 只叠加到位置环设定值上,不累加进 pitch_target_deg,默认 0 无副作用 */
float gimbal_bench_pitch_offset = 0.0f;
/* 实际施加的偏置(经限位安全门控后),仅用于遥测显示真实设定值 */
static float pitch_applied_offset = 0.0f;
#endif
/* 装配符号:0=未检测,±1=已测定;未检测前 gimbal_control 不应被调用 */
static float yaw_sign_f = 0.0f;
static uint8_t yaw_sign_valid = 0;
/* 拨弹电流由 shoot 模块写入,云台与拨弹共帧(0x1FF CAN1)发送 */
static int16_t rammer_current_shared = 0;
void shoot_share_rammer_current(int16_t current);
void gimbal_motor_init(void)
{
dji_motor_init(&motor_yaw_gimbal, &hcan2, 0x205, DJI_MOTOR_6020);
dji_motor_init(&motor_pitch_gimbal, &hcan1, 0x206, DJI_MOTOR_6020);
dji_motor_init(&motor_friction_l, &hcan1, 0x201, DJI_MOTOR_3508);
dji_motor_init(&motor_friction_r, &hcan1, 0x202, DJI_MOTOR_3508);
dji_motor_init(&motor_rammer, &hcan1, 0x207, DJI_MOTOR_2006);
dji_motor_init(&motor_rammer, &hcan2, 0x201, DJI_MOTOR_2006);
/* Yaw 位置环:° -> °/s */
PID_PositionStructureInit(&yaw_angle_pid, 0);
@@ -58,7 +72,7 @@ void gimbal_motor_init(void)
PID_PositionSetEkRange(&yaw_angle_pid, -GIMBAL_YAW_ANGLE_EK_DEADBAND, GIMBAL_YAW_ANGLE_EK_DEADBAND);
PID_PositionSetOUTRange(&yaw_angle_pid, -GIMBAL_YAW_ANGLE_OUT_LIMIT, GIMBAL_YAW_ANGLE_OUT_LIMIT);
/* Yaw 速度环:°/s -> 电压 */
/* Yaw 速度环:°/s -> 电流 */
PID_PositionStructureInit(&yaw_speed_pid, 0);
PID_PositionSetParameter(&yaw_speed_pid, GIMBAL_YAW_SPEED_KP, GIMBAL_YAW_SPEED_KI, GIMBAL_YAW_SPEED_KD);
PID_PositionSetOUTRange(&yaw_speed_pid, -GIMBAL_YAW_SPEED_OUT_LIMIT, GIMBAL_YAW_SPEED_OUT_LIMIT);
@@ -71,8 +85,8 @@ void gimbal_motor_init(void)
PID_PositionStructureInit(&pitch_speed_pid, 300);
PID_PositionSetParameter(&pitch_speed_pid, GIMBAL_PITCH_SPEED_KP, GIMBAL_PITCH_SPEED_KI, GIMBAL_PITCH_SPEED_KD);
PID_PositionSetEkRange(&pitch_speed_pid, -5, 5);
PID_PositionSetOUTRange(&pitch_speed_pid, -30000, 30000);
PID_PositionSetEkRange(&pitch_speed_pid, 0, 0);
PID_PositionSetOUTRange(&pitch_speed_pid, -16384, 16384);
}
uint8_t gimbal_detect_yaw_sign(void)
@@ -81,24 +95,24 @@ uint8_t gimbal_detect_yaw_sign(void)
return 0;
/* 静默期:输出清零等待机械/陀螺稳定 */
dji_motor_send_current_high(&hcan2, 0, 0, 0, 0);
dji_motor_send_gm6020_current_low(&hcan2, 0, 0, 0, 0);
HAL_Delay(50);
/* 正向电压脉冲 60ms,期间平均陀螺 z 角速度 */
/* 正向电流脉冲 60ms,期间平均陀螺 z 角速度 */
float sum = 0.0f;
dji_motor_send_current_high(&hcan2, GIMBAL_YAW_DETECT_VOLTAGE, 0, 0, 0);
dji_motor_send_gm6020_current_low(&hcan2, GIMBAL_YAW_DETECT_CURRENT, 0, 0, 0);
for (uint16_t i = 0; i < 60; i++)
{
sum += bmi088_gyro[2]; // rad/s(z 轴向上为正)
HAL_Delay(1);
}
dji_motor_send_current_high(&hcan2, 0, 0, 0, 0);
dji_motor_send_gm6020_current_low(&hcan2, 0, 0, 0, 0);
HAL_Delay(80); // 回稳,随后 gimbal_task 的首次控制会同步目标角
const float rate_dps = sum / 60.0f * RAD_TO_ANGLE;
if (rate_dps > GIMBAL_YAW_DETECT_RATE_MIN)
{
yaw_sign_f = 1.0f; // 正电压->陀螺正转,装配增益 G>0
yaw_sign_f = 1.0f; // 正电流->陀螺正转,装配增益 G>0
yaw_sign_valid = 1;
}
else if (rate_dps < -GIMBAL_YAW_DETECT_RATE_MIN)
@@ -119,7 +133,7 @@ float gimbal_yaw_sign(void)
int8_t gimbal_encoder_ccw(void)
{
/* 自检:电压正脉冲 -> 陀螺 z 正转(云台 CCW),而电压正方向即编码器
/* 自检:电流正脉冲 -> 陀螺 z 正转(云台 CCW),而电流正方向即编码器
* tick 增大方向,故 tick 增方向 = sign(gimbal 旋转) */
if (!yaw_sign_valid)
return 0;
@@ -133,24 +147,35 @@ void gimbal_control(float yaw_delta, float pitch_delta, uint8_t reset_flag)
const float yaw_meas = sign * att_deg_yaw; // °
const float yaw_rate_meas = sign * (bmi088_gyro[2] * RAD_TO_ANGLE); // °/s
/* 首次进入控制:目标角同步为当前姿态(否则 Yaw 目标仍为初始 0°,
* 一闭环就会朝 0° 猛转) */
/* 首次进入控制或复位:将目标角设定为设定的编码器零位朝向(类似 Pitch 上电归位) */
static uint8_t first_run = 1;
if (first_run)
if (first_run || reset_flag)
{
first_run = 0;
yaw_target_deg = yaw_meas;
pitch_target_deg = 0;
}
if (reset_flag)
{
yaw_target_deg = yaw_meas; // Yaw 复位为当前角度
pitch_target_deg = 0; // Pitch 复位为上电位置
PID_PositionClean(&yaw_angle_pid);
PID_PositionClean(&yaw_speed_pid);
PID_PositionClean(&pitch_angle_pid);
PID_PositionClean(&pitch_speed_pid);
/* 计算当前编码器距离设定零位的最短差值(-4096 ~ +4096) */
int16_t ecd_diff = (int16_t)motor_yaw_gimbal.fdb.raw_angle - (int16_t)YAW_GM6020_ENCODER_ZERO;
if (ecd_diff > 4096)
ecd_diff -= 8192;
else if (ecd_diff < -4096)
ecd_diff += 8192;
/* 将编码器 tick 差折算为机械角度偏差(°)，补偿给世界系目标角 */
const float ecd_err_deg = (float)ecd_diff * (360.0f / 8192.0f);
yaw_target_deg = yaw_meas - ecd_err_deg;
/* Pitch: 计算当前编码器距离机械零位的差值，折算为角度偏差补偿给目标角(上电自动归位到零位) */
int16_t pitch_ecd_diff = (int16_t)motor_pitch_gimbal.fdb.raw_angle - (int16_t)PITCH_GM6020_ENCODER_ZERO;
const float pitch_ecd_err_deg = (float)pitch_ecd_diff * (360.0f / 8192.0f);
pitch_target_deg = -att_deg_roll - pitch_ecd_err_deg;
if (reset_flag)
{
PID_PositionClean(&yaw_angle_pid);
PID_PositionClean(&yaw_speed_pid);
PID_PositionClean(&pitch_angle_pid);
PID_PositionClean(&pitch_speed_pid);
}
}
yaw_target_deg += yaw_delta;
@@ -160,28 +185,130 @@ void gimbal_control(float yaw_delta, float pitch_delta, uint8_t reset_flag)
yaw_angle_pid.Need_Value = yaw_target_deg;
PID_PositionCalc(&yaw_angle_pid, yaw_meas);
/* Yaw 速度环:°/s -> 电压(反馈为带符号陀螺角速度,双环符号自洽) */
/* Yaw 速度环:°/s -> 电流(反馈为带符号陀螺角速度,双环符号自洽) */
yaw_speed_pid.Need_Value = yaw_angle_pid.OUT;
PID_PositionCalc(&yaw_speed_pid, yaw_rate_meas);
yaw_voltage = yaw_speed_pid.OUT;
/* Pitch 串级闭环,位置环反馈为 AHRS Roll(legacy 语义) */
/* 小陀螺底盘自旋解耦前馈:根据底盘相对转速补偿动摩擦与反电动势拖拽，消除同向/反向手感不对称 */
float spin_feedforward = 0.0f;
if (cmd_robot.spin_flag || dr16.s2 == 1 || dr16.s2 == 2)
{
spin_feedforward = GIMBAL_YAW_SPIN_FEEDFORWARD_K * (float)motor_yaw_gimbal.fdb.rotor_speed;
}
yaw_current = yaw_speed_pid.OUT + spin_feedforward;
if (yaw_current > GIMBAL_YAW_SPEED_OUT_LIMIT)
yaw_current = GIMBAL_YAW_SPEED_OUT_LIMIT;
else if (yaw_current < -GIMBAL_YAW_SPEED_OUT_LIMIT)
yaw_current = -GIMBAL_YAW_SPEED_OUT_LIMIT;
/* Pitch 串级闭环,位置环反馈为 AHRS Roll */
#if 0
/* ===== 2026-10-15 台架调参临时改动(已停用,保留备查) =====
* 启用时:先算编码器角与上下软限位,做台架偏置的限位安全门控(轴距限位
* 不足 GIMBAL_BENCH_PITCH_SAFE_MARGIN_DEG 时不施加阶跃),并把下面一行
* 改为 pitch_angle_pid.Need_Value = pitch_target_deg + pitch_applied_offset; */
const float pitch_ecd_deg = ((float)motor_pitch_gimbal.fdb.raw_angle -
(float)PITCH_GM6020_ENCODER_ZERO) * (360.0f / 8192.0f);
const float pitch_lim_up_deg = ((float)PITCH_GM6020_POSITION_UPPER_LIMIT -
(float)PITCH_GM6020_ENCODER_ZERO) * (360.0f / 8192.0f);
const float pitch_lim_dn_deg = ((float)PITCH_GM6020_POSITION_LOWER_LIMIT -
(float)PITCH_GM6020_ENCODER_ZERO) * (360.0f / 8192.0f);
pitch_applied_offset = gimbal_bench_pitch_offset;
if (pitch_ecd_deg < pitch_lim_up_deg + GIMBAL_BENCH_PITCH_SAFE_MARGIN_DEG ||
pitch_ecd_deg > pitch_lim_dn_deg - GIMBAL_BENCH_PITCH_SAFE_MARGIN_DEG)
pitch_applied_offset = 0.0f;
#endif
pitch_angle_pid.Need_Value = pitch_target_deg;
PID_PositionCalc(&pitch_angle_pid, att_deg_roll);
PID_PositionCalc(&pitch_angle_pid, -att_deg_roll);
pitch_speed_pid.Need_Value = pitch_angle_pid.OUT;
PID_PositionCalc(&pitch_speed_pid, motor_pitch_gimbal.fdb.rotor_speed);
pitch_voltage = pitch_speed_pid.OUT;
pitch_pid = pitch_speed_pid.OUT;
/* 发送:CAN2 0x1FF 槽1 = Yaw 电压;CAN1 0x1FF 槽2 = Pitch 电压,槽3 = 拨弹电流 */
dji_motor_send_current_high(&hcan2, (int16_t)yaw_voltage, 0, 0, 0);
dji_motor_send_current_high(&hcan1, 0, (int16_t)pitch_voltage, rammer_current_shared, 0);
/* Pitch 重力拟合前馈补偿:
* a 为当前物理编码值减去 3200*360/8192 的数值(折算为弧度送入三角函数)
* I = 3105.88 * cos(a) + 3565.50 * sin(a) + 64.31
* 最终电流输出 pitch_out = pitch_pid + pitch_g (速度环不代入 pitch_g) */
const float a_deg = ((float)motor_pitch_gimbal.fdb.raw_angle - GIMBAL_PITCH_GRAVITY_ZERO_ECD) * (360.0f / 8192.0f);
const float a_rad = a_deg * ANGLE_TO_RAD;
pitch_g = GIMBAL_PITCH_GRAVITY_K_COS * cosf(a_rad) +
GIMBAL_PITCH_GRAVITY_K_SIN * sinf(a_rad) +
GIMBAL_PITCH_GRAVITY_K_CONST;
pitch_current = pitch_pid + pitch_g;
if (pitch_current > 16384.0f)
pitch_current = 16384.0f;
else if (pitch_current < -16384.0f)
pitch_current = -16384.0f;
#if 0
/* ===== 2026-10-15 台架调参临时改动:Pitch 软限位/堵转保护(已停用,保留备查) =====
* 背景:原设计的上下限位只作用于遥控输入路径(robot_cmd_task),控制环自身的
* 目标角/前馈没有任何限位约束。台架烧录会失力矩十几秒~几分钟,轴会掉到限位,
* 若不加保护,原逻辑会持续输出大电流顶着限位(GM6020 直驱堵转 = 持续过载发热)。
* 做法:越限位时只允许"离开限位"方向的电流(正电流 = 抬头/编码器减小,故下限位
* 只留正向、上限位只留负向),反方向清零;限位外连续 GIMBAL_PITCH_LIMIT_STALL_MS
* 编码器不动则判堵转,电流降到涓流上限。轴回到软限位内后闭环自动恢复正常。 */
if (pitch_ecd_deg >= pitch_lim_dn_deg || pitch_ecd_deg <= pitch_lim_up_deg)
{
/* 堵转计时:相对基准编码值移动超过 10 个刻度(0.44°)才算"在动"。
* 阈值取 10 而不是 2:陀螺/结构微振会让编码器抖 2~3 个刻度,阈值太小会把
* 静止误判成在动,保护永远不生效(实测踩过);慢速抬升 5°/s 在 300ms 内
* 也能走 34 个刻度,不会被误判。 */
static uint16_t lim_stall = 0;
static uint16_t lim_ref_ecd = 0;
const int16_t d_ecd = (int16_t)((int16_t)motor_pitch_gimbal.fdb.raw_angle -
(int16_t)lim_ref_ecd);
if (d_ecd > 10 || d_ecd < -10)
{
lim_ref_ecd = motor_pitch_gimbal.fdb.raw_angle;
lim_stall = 0;
}
else if (lim_stall < 60000u)
lim_stall++;
const float cap = (lim_stall * 2u >= (uint16_t)GIMBAL_PITCH_LIMIT_STALL_MS)
? GIMBAL_PITCH_LIMIT_CURRENT
: GIMBAL_PITCH_LIMIT_CURRENT_RECOVER;
if (pitch_ecd_deg >= pitch_lim_dn_deg) /* 轴过低:只许抬升 */
{
if (pitch_current < 0.0f)
pitch_current = 0.0f;
else if (pitch_current > cap)
pitch_current = cap;
}
else /* 轴过高:只许下压 */
{
if (pitch_current > 0.0f)
pitch_current = 0.0f;
else if (pitch_current < -cap)
pitch_current = -cap;
}
PID_PositionClean(&pitch_speed_pid);
}
#endif
/* ===== 停用块结束 ===== */
/* 发送:CAN2 0x1FE 槽1 = Yaw 电流;CAN1 0x1FE 槽2 = Pitch 电流 */
dji_motor_send_gm6020_current_low(&hcan2, (int16_t)yaw_current, 0, 0, 0);
dji_motor_send_gm6020_current_low(&hcan1, 0, (int16_t)pitch_current, 0, 0);
}
void shoot_share_rammer_current(int16_t current)
#if 0
/* ===== 2026-10-15 台架调参临时接口(已停用,保留备查) ===== */
/* Pitch 位置环实际设定值(°) = 真实目标角 + 经限位门控后的台架偏置 */
float gimbal_pitch_setpoint_deg(void)
{
rammer_current_shared = current;
return pitch_target_deg + pitch_applied_offset;
}
/* Pitch 位置环输出 = 速度环目标(°/s),用于判断内环是否被限幅 */
float gimbal_pitch_speed_ref(void)
{
return pitch_angle_pid.OUT;
}
#endif
uint8_t gimbal_motor_offline(void)
{
uint32_t now = HAL_GetTick();
@@ -199,7 +326,8 @@ uint8_t gimbal_motor_offline(void)
void gimbal_output_zero(void)
{
dji_motor_send_current_high(&hcan2, 0, 0, 0, 0);
dji_motor_send_current_high(&hcan1, 0, 0, 0, 0);
dji_motor_send_gm6020_current_low(&hcan2, 0, 0, 0, 0);
dji_motor_send_gm6020_current_low(&hcan1, 0, 0, 0, 0);
dji_motor_send_current_low(&hcan1, 0, 0, 0, 0);
dji_motor_send_current_low(&hcan2, 0, 0, 0, 0);
}
云台/modules/control/gimbal.h
+20 -8
View File
@@ -4,13 +4,13 @@
/* 云台双轴控制(串级 PID)
* Yaw (2026-09 重写):双环都以陀螺仪为反馈——
* 位置环:QEKF 多圈 yaw(°) -> 目标角速度(°/s)
* 速度环:陀螺 z 轴角速度(°/s) -> GM6020 电压
* 速度环:陀螺 z 轴角速度(°/s) -> GM6020 电流
* 装配符号由上电自检自动测定(gimbal_detect_yaw_sign),
* 两环共用同一符号,不可能再出现"两传感器符号打架"
* Pitch:位置环用 QEKF 的 Roll(安装方向所致,勿改),速度环转子转速
* 电机: Yaw=GM6020 CAN2 0x205(电压,0x1FF CAN2 槽1)
* Pitch=GM6020 CAN1 0x206(电压,与拨弹共帧 0x1FF CAN1 槽2/3,legacy 方案)
* 摩擦轮 M3508 0x201/0x202 与拨弹 M2006 0x207 的实例也在此初始化 */
* 电机: Yaw=GM6020 CAN2 0x205(电流,0x1FE CAN2 槽1)
* Pitch=GM6020 CAN1 0x206(电流,0x1FE CAN1 槽2)
* 摩擦轮 M3508 0x201/0x202(CAN1) 与拨弹 M2006 0x201(CAN2) 的实例也在此初始化 */
#include "dji_motor.h"
@@ -19,12 +19,15 @@ extern dji_motor_t motor_yaw_gimbal; // Yaw GM6020,CAN2 0x205
extern dji_motor_t motor_pitch_gimbal; // Pitch GM6020,CAN1 0x206
extern dji_motor_t motor_friction_l; // 左摩擦轮 M3508,CAN1 0x201
extern dji_motor_t motor_friction_r; // 右摩擦轮 M3508,CAN1 0x202
extern dji_motor_t motor_rammer; // 拨弹 M2006,CAN1 0x207
extern dji_motor_t motor_rammer; // 拨弹 M2006,CAN2 0x201
extern float pitch_pid; // Pitch PID 输出分量(仅速度环反馈计算)
extern float pitch_g; // Pitch 重力拟合前馈分量
extern float pitch_current; // Pitch GM6020 最终电流控制输出(pitch_pid + pitch_g, ±16384)
/* 初始化电机实例与 PID(can_start 之后调用) */
extern void gimbal_motor_init(void);
/* Yaw 装配符号自检:给 Yaw 电机正向小电压脉冲,按陀螺 z 轴响应方向
/* Yaw 装配符号自检:给 Yaw 电机正向小电流脉冲,按陀螺 z 轴响应方向
* 测定符号。阻塞约 200ms(HAL_Delay),检测期间云台会轻转几度。
* 返回 1-成功(gimbal_yaw_sign() 可用) 0-失败(被按住/电机离线/无响应) */
extern uint8_t gimbal_detect_yaw_sign(void);
@@ -36,13 +39,22 @@ extern float gimbal_yaw_sign(void);
* 0=尚未自检。随 0x1A9 flags bit1 下发,供底盘跟随符号自动综合 */
extern int8_t gimbal_encoder_ccw(void);
/* 云台轴控制:根据 cmd 增量更新目标角并计算电压输出(2ms 调用)
* 内部发送 CAN2 0x1FF(Yaw)与 CAN1 0x1FF(Pitch+拨弹) */
/* 云台轴控制:根据 cmd 增量更新目标角并计算电流输出(2ms 调用)
* 内部发送 CAN2 0x1FE(Yaw)与 CAN1 0x1FE(Pitch) */
extern void gimbal_control(float yaw_delta, float pitch_delta, uint8_t reset_flag);
/* 云台任一电机掉线返回 1 */
extern uint8_t gimbal_motor_offline(void);
/* ===== 2026-10-15 台架调参临时接口(已停用,保留备查) =====
* 启用时把 #if 0 改 #if 1,并同步启用 gimbal.c / gimbal_task.c / robot_param.h
* / debug_task.c 里的同名停用块 */
#if 0
extern float gimbal_bench_pitch_offset; // 位置环设定值附加偏置(°),台架方波发生器写入
extern float gimbal_pitch_setpoint_deg(void); // 位置环实际设定值(°),供调参遥测读取
extern float gimbal_pitch_speed_ref(void); // 位置环输出=速度环目标(°/s),判断内环是否限幅
#endif
/* 云台输出清零(停车) */
extern void gimbal_output_zero(void);
云台/modules/control/shoot.c
+8 -7
View File
@@ -1,10 +1,10 @@
/* =============================================================================
* shoot.c - 发射机构:摩擦轮 2xM3508(0x200 CAN1 槽1/2)+ 拨弹 M2006
* shoot.c - 发射机构:摩擦轮 2xM3508(0x200 CAN1 槽1/2)+ 拨弹 M2006(0x200 CAN2 槽1)
* 逻辑(与 legacy 一致):
* 摩擦轮开关受发射机构上电状态门控(可由 DEBUG_SHOOT_WITHOUT_REFEREE 绕过),
* 开启时联动激光(PC8=TIM3_CH3 PWM,占空比 0/满 对应关/开)
* 拨弹仅在摩擦轮开启后允许;fire=GIMBAL_RAMMER_SPEED(-5400),eject 反向
* 拨弹电流经 shoot_share_rammer_current() 交给云台共帧发送(0x1FF CAN1)
* 拨弹电流经 shoot_send_cmd() 经 CAN2 0x200 帧直接发送(ID 1)
* ========================================================================== */
#include "shoot.h"
#include "gimbal.h"
@@ -43,7 +43,7 @@ void shoot_init(void)
PID_PositionStructureInit(&rammer_pid, GIMBAL_RAMMER_SPEED);
PID_PositionSetParameter(&rammer_pid, GIMBAL_RAMMER_KP, GIMBAL_RAMMER_KI, GIMBAL_RAMMER_KD);
PID_PositionSetEkRange(&rammer_pid, -20, 20);
PID_PositionSetOUTRange(&rammer_pid, -30000, 30000);
PID_PositionSetOUTRange(&rammer_pid, -10000, 10000);
laser_init();
}
@@ -67,7 +67,7 @@ void shoot_control(uint8_t friction_on, uint8_t fire, uint8_t eject, uint8_t sho
shoot_friction_flag = 0;
}
/* 拨弹:仅在摩擦轮开启时允许 */
/* 拨弹:仅在摩擦轮开启后允许 */
if (shoot_friction_flag)
{
if (fire)
@@ -83,19 +83,20 @@ void shoot_control(uint8_t friction_on, uint8_t fire, uint8_t eject, uint8_t sho
PID_PositionCalc(&friction_l_pid, motor_friction_l.fdb.rotor_speed);
PID_PositionCalc(&friction_r_pid, motor_friction_r.fdb.rotor_speed);
PID_PositionCalc(&rammer_pid, motor_rammer.fdb.rotor_speed);
/* 拨弹电流交给云台控制帧统一发送(0x1FF CAN1 共帧) */
shoot_share_rammer_current((int16_t)rammer_pid.OUT);
}
void shoot_send_cmd(void)
{
/* 摩擦轮 2×M3508:CAN1 0x200 槽1/2 */
dji_motor_send_current_low(&hcan1, (int16_t)friction_l_pid.OUT, (int16_t)friction_r_pid.OUT, 0, 0);
/* 拨弹盘 M2006(ID 1):CAN2 0x200 槽1 */
dji_motor_send_current_low(&hcan2, (int16_t)rammer_pid.OUT, 0, 0, 0);
}
void shoot_output_zero(void)
{
dji_motor_send_current_low(&hcan1, 0, 0, 0, 0);
dji_motor_send_current_low(&hcan2, 0, 0, 0, 0);
LASER_OFF();
shoot_friction_flag = 0;
}
云台/modules/control/shoot.h
+2 -4
View File
@@ -3,7 +3,7 @@
#include <stdint.h>
/* 发射机构:摩擦轮 2×M3508(0x200 CAN1 槽1/2)+ 拨弹 M2006(电流由云台共帧发送)
/* 发射机构:摩擦轮 2×M3508(0x200 CAN1 槽1/2)+ 拨弹 M2006(0x200 CAN2 槽1)
* 摩擦轮开启时联动激光(PC8,经 TIM3 CH3 PWM) */
/* 初始化摩擦轮/拨弹 PID(can_start 之后调用) */
@@ -14,7 +14,7 @@ extern void shoot_init(void);
* shooter_power_on:发射机构上电状态(来自底盘 0x019) */
extern void shoot_control(uint8_t friction_on, uint8_t fire, uint8_t eject, uint8_t shooter_power_on);
/* 发送摩擦轮电流帧(0x200 CAN1) */
/* 发送摩擦轮(0x200 CAN1)与拨弹(0x200 CAN2)电流帧 */
extern void shoot_send_cmd(void);
/* 摩擦轮输出清零 */
@@ -23,6 +23,4 @@ extern void shoot_output_zero(void);
/* 摩擦轮当前开关状态(供激光联动与调试) */
extern uint8_t shoot_friction_flag;
/* 拨弹电流写入共享变量(由 shoot 模块调用,云台共帧发送) */
extern void shoot_share_rammer_current(int16_t current);
#endif
云台/modules/dev/buzzer.c
+63 -10
View File
@@ -6,6 +6,7 @@
* ========================================================================== */
#include "buzzer.h"
#include "tim.h"
#include "robot_param.h"
extern TIM_HandleTypeDef htim4;
@@ -32,7 +33,8 @@ void buzzer_on(buzzer_tone_e tone)
{
__HAL_TIM_SET_PRESCALER(&htim4, buzzer_tone_freq[tone]);
HAL_TIM_GenerateEvent(&htim4, TIM_EVENTSOURCE_UPDATE); // 立即装载 PSC
__HAL_TIM_SET_COMPARE(&htim4, TIM_CHANNEL_3, 5); // 占空比 50%
/* 占空比 30%:抑制高次尖锐谐波,使吉他拨弦音色圆润纯净 */
__HAL_TIM_SET_COMPARE(&htim4, TIM_CHANNEL_3, 3);
}
else
__HAL_TIM_SET_COMPARE(&htim4, TIM_CHANNEL_3, 0);
@@ -44,21 +46,72 @@ void buzzer_off(void)
}
/* ==========================================================================
* 调试用旋律(见 buzzer.h):每步 100ms,空拍 BUZZER_P 为静音。
* 无源蜂鸣器只有单音,这里用"上行分解和弦 + 回落"拼成一句短旋律;选音限定
* 在中音 3 ~ 高音 2,避免刺耳。循环播放不会漏掉"有设备掉线"这一事实,
* 因为红灯常亮由 monitor_task 独立控制,与该旋律无关。
* 改旋律:直接增删这里的音符即可,长度会自动生效。
* 周杰伦《晴天》- 标志性吉他前奏伴奏 Solo (纯享循环版)
* 调式: 1=C,处于 C 板蜂鸣器最佳频响区间(500~1000Hz)
* 结构: 完整还原原曲前奏 4 小节经典木吉他单音分解
* [小节1: Em] 3 2 1 1 2 1 5_ 1 2
* [小节2: C ] 3 2 1 1 2 1 6_ 1 2
* [小节3: G ] 3 2 1 1 2 1 5_ 1 2
* [小节4: D ] 3 2 1 1 2 1 2 3 5 3 2 1 2 -
* 吐音设计: 每个音符保留 BUZZER_P 间隔,模拟吉他真实的清脆拨弦与泛音
* ========================================================================== */
static const buzzer_tone_e buzzer_melody[] = {
BUZZER_M3, BUZZER_M5, BUZZER_M6, BUZZER_H1, BUZZER_P,
BUZZER_M6, BUZZER_H1, BUZZER_H2, BUZZER_P,
BUZZER_H1, BUZZER_M6, BUZZER_M5, BUZZER_M3, BUZZER_P,
/* ---- 小节 1 (Em): 3 2 1 1 2 1 | 5_ 1 2 ---- */
BUZZER_M3, BUZZER_P, // 3 (Mi)
BUZZER_M2, BUZZER_P, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_L5, BUZZER_P, // 低音 5 (Sol)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
/* ---- 小节 2 (C): 3 2 1 1 2 1 | 6_ 1 2 ---- */
BUZZER_M3, BUZZER_P, // 3 (Mi)
BUZZER_M2, BUZZER_P, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_L6, BUZZER_P, // 低音 6 (La)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
/* ---- 小节 3 (G): 3 2 1 1 2 1 | 5_ 1 2 ---- */
BUZZER_M3, BUZZER_P, // 3 (Mi)
BUZZER_M2, BUZZER_P, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_L5, BUZZER_P, // 低音 5 (Sol)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
/* ---- 小节 4 (D): 3 2 1 1 2 1 | 2 3 5 3 2 1 2 - ---- */
BUZZER_M3, BUZZER_P, // 3 (Mi)
BUZZER_M2, BUZZER_P, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M2, BUZZER_P, // 2 (Re)
BUZZER_M3, // 3 (Mi)
BUZZER_M5, // 5 (Sol)
BUZZER_M3, // 3 (Mi)
BUZZER_M2, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M2, BUZZER_M2, BUZZER_M2, BUZZER_M2, BUZZER_M2, BUZZER_P, // 2 (Re 长音结音)
BUZZER_P, BUZZER_P, BUZZER_P, BUZZER_P, // 尾部休止 400ms 后循环
};
void buzzer_play_melody(uint16_t step)
{
const uint16_t steps =
(uint16_t)(sizeof(buzzer_melody) / sizeof(buzzer_melody[0]));
buzzer_on(buzzer_melody[step % steps]);
#ifndef BUZZER_MELODY_SPEED_DIV
#define BUZZER_MELODY_SPEED_DIV 1
#endif
buzzer_on(buzzer_melody[(step / BUZZER_MELODY_SPEED_DIV) % steps]);
}
云台/modules/motor/dji_motor.c
+32 -10
View File
@@ -6,9 +6,8 @@
* (无 legacy 的 +-1 圈限制,底盘小陀螺时 Yaw 可连续旋转),
* 记录 last_online_tick 供掉线检测
* 控制路径(任务上下文):
* dji_motor_send_current_low/high() 0x200 / 0x1FF 电流帧(+/-16384 = 20A/10A)
* dji_motor_send_voltage_high() 0x2FF 电压帧(GM6020 ID5~7)
* 注意 0x1FF 帧为 M3508/M2006 高位电流与 GM6020 低位电压共用,按槽位区分
* dji_motor_send_current_low/high() 0x200 / 0x1FF 电流帧(+/-16384 = 20A/10A)
* dji_motor_send_gm6020_current_low/high() 0x1FE / 0x2FE GM6020 电流帧(+/-16384 = 3A)
* ========================================================================== */
#include "dji_motor.h"
@@ -20,7 +19,8 @@
static dji_motor_t * dji_motor_list[DJI_MOTOR_MAX];
static uint8_t dji_motor_count = 0;
static void dji_motor_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc);
static void dji_motor_can1_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc);
static void dji_motor_can2_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc);
/* 解析一帧反馈,多圈累计(无 ±1 圈限制,底盘小陀螺时 Yaw 电机可连续旋转) */
static void dji_motor_parse(dji_motor_t * motor, const uint8_t data[8])
@@ -71,16 +71,32 @@ void dji_motor_init(dji_motor_t * motor, hcan_t * hcan, uint16_t rx_id, dji_moto
if (dji_motor_count < DJI_MOTOR_MAX)
{
dji_motor_list[dji_motor_count++] = motor;
can_rx_register(hcan, rx_id, dji_motor_rx_callback);
if (hcan == &hcan1)
can_rx_register(hcan, rx_id, dji_motor_can1_rx_callback);
else
can_rx_register(hcan, rx_id, dji_motor_can2_rx_callback);
}
}
static void dji_motor_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc)
static void dji_motor_can1_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc)
{
(void)dlc;
for (uint8_t i = 0; i < dji_motor_count; i++)
{
if (dji_motor_list[i]->rx_id == std_id)
if (dji_motor_list[i]->hcan == &hcan1 && dji_motor_list[i]->rx_id == std_id)
{
dji_motor_parse(dji_motor_list[i], rx_data);
return;
}
}
}
static void dji_motor_can2_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc)
{
(void)dlc;
for (uint8_t i = 0; i < dji_motor_count; i++)
{
if (dji_motor_list[i]->hcan == &hcan2 && dji_motor_list[i]->rx_id == std_id)
{
dji_motor_parse(dji_motor_list[i], rx_data);
return;
@@ -119,8 +135,14 @@ void dji_motor_send_current_high(hcan_t * hcan, int16_t i5, int16_t i6, int16_t
dji_motor_send_int16x4(hcan, 0x1FF, v);
}
void dji_motor_send_voltage_high(hcan_t * hcan, int16_t v5, int16_t v6, int16_t v7)
void dji_motor_send_gm6020_current_low(hcan_t * hcan, int16_t i1, int16_t i2, int16_t i3, int16_t i4)
{
const int16_t v[4] = {v5, v6, v7, 0};
dji_motor_send_int16x4(hcan, 0x2FF, v);
const int16_t v[4] = {i1, i2, i3, i4};
dji_motor_send_int16x4(hcan, 0x1FE, v);
}
void dji_motor_send_gm6020_current_high(hcan_t * hcan, int16_t i5, int16_t i6, int16_t i7, int16_t i8)
{
const int16_t v[4] = {i5, i6, i7, i8};
dji_motor_send_int16x4(hcan, 0x2FE, v);
}
云台/modules/motor/dji_motor.h
+7 -6
View File
@@ -5,13 +5,13 @@
/* DJI 电机(M3508/M2006/GM6020)统一驱动
* - 反馈:can_start() 后通过 can_rx_register 按 rx_id 注册,接收中断内解析(多圈累计)
* - 控制:组装 0x200/0x1FF/0x2FF 控制帧,经 CAN_SendTxMessage 发送 */
* - 控制:组装 0x200/0x1FF/0x1FE/0x2FE 控制帧,经 CAN_SendTxMessage 发送 */
typedef enum
{
DJI_MOTOR_3508, // 减速比 3591:187(≈19:1), 转矩常数 0.3N·m/A
DJI_MOTOR_2006, // 减速比 36:1, 转矩常数 0.18N·m/A
DJI_MOTOR_6020, // 直驱, 电压控制
DJI_MOTOR_6020, // 直驱, 电流控制(ID1~4 为 0x1FE 帧, ±16384 对应 ±3A)
} dji_motor_type_e;
typedef struct
@@ -20,7 +20,7 @@ typedef struct
int64_t total_tick; // 累计角度位置原始数据(8192*圈数+raw,无 ±1 圈限制)
float rotor_angle_deg; // 累计转子机械角(°)
int16_t rotor_speed; // 转子转速(RPM)
int16_t raw_torque; // 转矩电流/转矩电压原始数据
int16_t raw_torque; // 转矩电流原始数据
float torque_current; // 转矩电流(A)
uint8_t temperature; // 电机温度(℃)
uint32_t last_online_tick; // 最近一次收到反馈的 tick(HAL_GetTick)
@@ -39,11 +39,12 @@ extern void dji_motor_init(dji_motor_t * motor, hcan_t * hcan, uint16_t rx_id, d
/* ---- 控制帧发送 ----
* M3508/M2006 ID1~4:0x200 电流帧(±16384 对应 ±20A/±10A)
* M3508/M2006 ID5~8:0x1FF 电流帧;GM6020 ID1~4:0x1FF 电压帧(±25000)
* GM6020 ID5~7:0x2FF 电压帧 */
* M3508/M2006 ID5~8:0x1FF 电流帧(±16384)
* GM6020 电流控制:ID1~4 为 0x1FE 电流帧(±16384 对应 ±3A),ID5~8 为 0x2FE 电流帧(±16384) */
extern void dji_motor_send_current_low(hcan_t * hcan, int16_t i1, int16_t i2, int16_t i3, int16_t i4);
extern void dji_motor_send_current_high(hcan_t * hcan, int16_t i5, int16_t i6, int16_t i7, int16_t i8);
extern void dji_motor_send_voltage_high(hcan_t * hcan, int16_t v5, int16_t v6, int16_t v7);
extern void dji_motor_send_gm6020_current_low(hcan_t * hcan, int16_t i1, int16_t i2, int16_t i3, int16_t i4);
extern void dji_motor_send_gm6020_current_high(hcan_t * hcan, int16_t i5, int16_t i6, int16_t i7, int16_t i8);
/* 通用 int16x4 发送(板间通讯等复用) */
extern void dji_motor_send_int16x4(hcan_t * hcan, uint32_t std_id, const int16_t val[4]);
底盘/Application/Task/Src/chassis_task.c
+10 -1
View File
@@ -17,6 +17,7 @@
#include "robot_typedef.h"
#include "chassis.h"
#include "attitude.h"
#include "bmi088.h"
#include "referee.h"
#include "c_comm.h"
#include "robot_param.h"
@@ -120,6 +121,14 @@ void chassis_task(void const * argument)
float vx = cmd_robot.vx * boost;
float vy = cmd_robot.vy * boost;
/* 坐标系旋转投影:将以云台枪口为准的平移速度转换到底盘坐标系，并叠加 kw 前馈 */
float chassis_vx = vx;
float chassis_vy = vy;
/* 跟随模式下无持续自旋，前馈量为0；小陀螺模式下代入实际自旋角速度 w */
float w_feedforward = (cmd_robot.chassis_mode == CHASSIS_MODE_FOLLOW) ? 0.0f : bmi088_gyro[2];
chassis_vector_to_body(vx, vy, w_feedforward, &chassis_vx, &chassis_vy);
/* 简易功率限制:缓冲能量线性映射为缩放系数 */
float scale = 1.0f;
if (referee.buffer_energy < POWER_LIMIT_BUFFER_LOW)
@@ -130,7 +139,7 @@ void chassis_task(void const * argument)
else if (scale > 1.0f)
scale = 1.0f;
chassis_control(vx, vy, w, scale);
chassis_control(chassis_vx, chassis_vy, w, scale);
}
else
{
底盘/Application/Task/Src/debug_task.c
+54 -7
View File
@@ -1,5 +1,5 @@
/* =============================================================================
* debug_task.c - USB 虚拟串口(CDC)姿态输出(欧拉角 + 姿态链路诊断)
* debug_task.c - USB 虚拟串口(CDC)姿态输出(欧拉角 + 姿态链路诊断 + 控制量/模式)
* 每 DEBUG_OUT_PERIOD_MS 输出一行。单位: 角度 ° / 加速度 m/s² / 角速度 rad/s
*
* ---- 欧拉角(QuaternionEKF 解算结果,见 modules/ins) ----
@@ -25,7 +25,20 @@
* se bmi088_spi_errors:SPI/DMA 出错次数;st=bmi088_spi_state()
* (1=READY,非 1 说明 SPI 被卡住,数据路会因此停摆)
*
* 开关: DEBUG_ATT_HEALTH=0 只输出三个欧拉角;DEBUG_ATT_DIAG=0 去掉诊断位。
* ---- 控制量 / 控制模式(DEBUG_CMD_OUT=1 时追加) ----
* mode 底盘模式 0=OFF 1=MANUAL 2=FOLLOW 3=SPIN_SLOW 4=SPIN_FAST
* (由本板依据收到的 s2/spin 推出;模式逻辑见 robot_cmd_task.c)
* online 1=板间通讯(CToC)在线 —— 本板唯一的"控制源在线"判据
* vx/vy 底盘平移速度指令(世界系映射值) wz [已废弃,恒 0]
* spin **收到的**小陀螺使能(0x189 bit2,云台侧做 Ctrl 沿检测)
* s2 **收到的**遥控 S2 档位(小陀螺为真时它被覆盖)
* reset 跟随朝向重锁请求(跟随模式重连时置位)
* 注意:本板拿不到"遥控器还是键鼠"这一信息——0x149/0x189 不带该位,
* robot_cmd_task 里 cmd_robot.source 恒被置 0,故这里不输出假字段。
* 与姿态同源(cmd_robot/ctoc_remote),一起看才能判断"模式对不对、量给没给"。
*
* 开关: DEBUG_ATT_HEALTH=0 只输出三个欧拉角;DEBUG_ATT_DIAG=0 去掉诊断位;
* DEBUG_CMD_OUT=1 追加控制量/控制模式。
* ========================================================================== */
#include "debug_task.h"
#include "cmsis_os.h"
@@ -35,6 +48,8 @@
#include "attitude.h"
#include "ins.h"
#include "bmi088.h"
#include "robot_typedef.h"
#include "c_comm.h"
#include <stdio.h>
#include <math.h>
@@ -42,13 +57,31 @@
#define DEBUG_ATT_HEALTH 1
/* 1-再附加原始陀螺/零偏/采样计数(排障用); 0-只留上面的通用健康位 */
#define DEBUG_ATT_DIAG 1
/* 1-追加控制量/控制模式(见文件头); 0-保持原姿态输出不变 */
#define DEBUG_CMD_OUT 1
/* 输出周期(ms)。姿态观测建议 100ms(10Hz) */
#define DEBUG_OUT_PERIOD_MS 100
#if DEBUG_CMD_OUT
/* 底盘模式名(便于人读;数值定义见 robot_typedef.h 的 chassis_mode_e) */
static const char * cmd_mode_name(chassis_mode_e m)
{
switch (m)
{
case CHASSIS_MODE_OFF: return "OFF";
case CHASSIS_MODE_MANUAL: return "MANUAL";
case CHASSIS_MODE_FOLLOW: return "FOLLOW";
case CHASSIS_MODE_SPIN_SLOW: return "SPIN_SLOW";
case CHASSIS_MODE_SPIN_FAST: return "SPIN_FAST";
default: return "?";
}
}
#endif
void debug_task(void const * argument)
{
char line[192];
char line[448];
char tail[112];
for (;;)
@@ -70,15 +103,29 @@ void debug_task(void const * argument)
(unsigned long)bmi088_spi_errors, (unsigned)bmi088_spi_state());
#endif
#if DEBUG_CMD_OUT
char ctl[192];
snprintf(ctl, sizeof(ctl),
" mode=%s online=%u vx=%.3f vy=%.3f wz=%.3f spin=%u s2=%u reset=%u",
cmd_mode_name(cmd_robot.chassis_mode),
(unsigned)cmd_robot.online,
cmd_robot.vx, cmd_robot.vy, cmd_robot.wz_manual,
(unsigned)ctoc_remote.spin_flag,
(unsigned)ctoc_remote.s2,
(unsigned)cmd_robot.gimbal_reset);
#else
const char * ctl = "";
#endif
#if DEBUG_ATT_HEALTH
int len = snprintf(line, sizeof(line),
"yaw=%.2f pitch=%.2f roll=%.2f cvg=%u rdy=%u imu=%u an=%.2f gn=%.3f%s\r\n",
"yaw=%.2f pitch=%.2f roll=%.2f cvg=%u rdy=%u imu=%u an=%.2f gn=%.3f%s%s\r\n",
att_deg_yaw, att_deg_pitch, att_deg_roll,
(unsigned)INS.ConvergeFlag, (unsigned)att_ready,
(unsigned)bmi088_online, an, gn, tail);
(unsigned)bmi088_online, an, gn, tail, ctl);
#else
int len = snprintf(line, sizeof(line), "yaw=%.2f pitch=%.2f roll=%.2f\r\n",
att_deg_yaw, att_deg_pitch, att_deg_roll);
int len = snprintf(line, sizeof(line), "yaw=%.2f pitch=%.2f roll=%.2f%s\r\n",
att_deg_yaw, att_deg_pitch, att_deg_roll, ctl);
#endif
if (len > 0)
底盘/Application/Task/Src/monitor_task.c
+2 -2
View File
@@ -85,8 +85,8 @@ static int8_t linkcheck_first_offline(void)
{
uint32_t now = HAL_GetTick();
#if defined(ROBOT_TYPE_GIMBAL)
/* 设备序号:0 摩擦轮L(0x201) 1 摩擦轮R(0x202) 2 Pitch(0x206)
* 3 Yaw(0x205) 4 拨弹(0x207,安装时) 5 底盘回传(0x019) */
/* 设备序号:0 摩擦轮L(CAN1 0x201) 1 摩擦轮R(CAN1 0x202) 2 Pitch(CAN1 0x206)
* 3 Yaw(CAN2 0x205) 4 拨弹(CAN2 0x201,安装时) 5 底盘回传(0x019) */
if (LINK_OFFLINE(motor_friction_l.fdb.last_online_tick))
return 0;
if (LINK_OFFLINE(motor_friction_r.fdb.last_online_tick))
底盘/Application/Task/Src/referee_task.c
+34
View File
@@ -7,6 +7,9 @@
#include "cmsis_os.h"
#include "bsp_usart.h"
#include "referee.h"
#include "referee_ui.h"
#include "c_comm.h"
#include "attitude.h"
#include "robot_param.h"
/* referee_task:裁判系统链路监测
@@ -29,6 +32,37 @@ void referee_task(void const * argument)
HAL_GetTick() - referee.last_update_tick > DEVICE_OFFLINE_TIME_MS * 10)
referee.link_status = 0;
/* ---- 自定义UI:机器人 -> 裁判系统 -> 选手端 ------------------------
* 本任务 100ms 一轮,内部按 UI_SEND_HZ 分频(5Hz:约 40 图形/帧,
* 115200 链路上约 3.8KB/s)。数据来源:
* 底盘本地 = att_deg_yaw(朝向) + referee(功率/电容)
* 云台 CToC = pitch + 摩擦轮 L/R 转速(0x1B9) + 云台 yaw(0x1A9) + 陀螺位(0x189)
* ------------------------------------------------------------------ */
{
static uint8_t ui_div = 0;
if (++ui_div >= (uint8_t)(10 / UI_SEND_HZ))
{
ui_div = 0;
ui_data_t ui;
ui.pitch_deg = ctoc_ui_pitch_deg;
ui.yaw_deg = ctoc_gimbal_yaw;
ui.hdg_deg = att_deg_yaw;
ui.pwr_w = referee.chassis_power;
ui.pwr_limit_w = (float)referee.chassis_power_limit;
ui.buf_j = referee.buffer_energy;
ui.cap_pct = (uint8_t)(referee.buffer_energy >= 60.0f
? 100
: (referee.buffer_energy * 100.0f / 60.0f));
ui.fric_l_rpm = ctoc_ui_fric_l_rpm;
ui.fric_r_rpm = ctoc_ui_fric_r_rpm;
ui.spin_on = ctoc_remote.spin_flag;
ui.ref_online = referee.link_status;
referee_ui_update(&ui);
}
}
monitor_heartbeat(HB_REFEREE);
osDelay(100);
}
底盘/Application/Task/Src/robot_cmd_task.c
+7 -7
View File
@@ -97,8 +97,8 @@ void robot_cmd_task(void const * argument)
if (!keyboard_online)
{
/* 遥控器:左摇杆,输出与摇杆偏量成比例(legacy 为过死区即全速,
* 体感过灵敏),限位门控与方向保持 legacy */
/* 遥控器:左摇杆向上(>1050)为抬头(pitch_delta减小,pos向2260减小),门控须 pos > UPPER_LIMIT(2260);
* 左摇杆向下(<1000)为低头(pitch_delta增大,pos向3950增大),门控须 pos < LOWER_LIMIT(3950) */
if (dr16.rc_l_UD > 1050 && pos > PITCH_GM6020_POSITION_UPPER_LIMIT)
pitch_delta -= GIMBAL_PITCH_LEVER_RATE / 8192.0f * 360.0f *
((float)dr16.rc_l_UD - 1024.0f) / 660.0f;
@@ -113,13 +113,13 @@ void robot_cmd_task(void const * argument)
}
else
{
/* 键鼠:同改为比例输出 */
if (keyboard_data.mouse_du < -8 && pos > PITCH_GM6020_POSITION_UPPER_LIMIT)
/* 键鼠:鼠标前推(>8)为抬头(pitch_delta减小),门控须 pos > UPPER_LIMIT;鼠标后拉(<-8)为低头(pitch_delta增大),门控须 pos < LOWER_LIMIT */
if (keyboard_data.mouse_du > 8 && pos > PITCH_GM6020_POSITION_UPPER_LIMIT)
pitch_delta -= GIMBAL_PITCH_LEVER_RATE / 8192.0f * 360.0f *
(-(float)keyboard_data.mouse_du * PC_MOUSE_DU_SENSITIVITY) / 660.0f;
else if (keyboard_data.mouse_du > 8 && pos < PITCH_GM6020_POSITION_LOWER_LIMIT)
pitch_delta += GIMBAL_PITCH_LEVER_RATE / 8192.0f * 360.0f *
((float)keyboard_data.mouse_du * PC_MOUSE_DU_SENSITIVITY) / 660.0f;
else if (keyboard_data.mouse_du < -8 && pos < PITCH_GM6020_POSITION_LOWER_LIMIT)
pitch_delta += GIMBAL_PITCH_LEVER_RATE / 8192.0f * 360.0f *
(-(float)keyboard_data.mouse_du * PC_MOUSE_DU_SENSITIVITY) / 660.0f;
if (keyboard_data.mouse_rl != 0)
yaw_delta -= GIMBAL_LEVER_SPEED_MAP_RATE * GIMBAL_YAW_PITCH_SPEED_RATE *
底盘/Application/robot_param.h
+35 -24
View File
@@ -9,9 +9,11 @@
#define ROBOT_PARAM_H
/* ============================ 云台 ============================ */
#define PITCH_GM6020_POSITION_LOWER_LIMIT 3990 // Pitch 轴编码器值下限(云台抬起方向)
#define PITCH_GM6020_POSITION_UPPER_LIMIT 2220 // Pitch 轴编码器值上限(云台压低方向)
#define PITCH_GM6020_ENCODER_ZERO 3245 // Pitch 轴编码器零位
#define PITCH_GM6020_POSITION_UPPER_LIMIT 2260 // Pitch 轴抬起极限(最高位,编码器较小值;实测2203撞死限位,留余量设2260)
#define PITCH_GM6020_POSITION_LOWER_LIMIT 3950 // Pitch 轴压低极限(最低位,编码器较大值;实测4234撞死限位,留余量设3950)
#define PITCH_GM6020_ENCODER_ZERO 3200 // Pitch 轴编码器水平零位
#define YAW_GM6020_ENCODER_ZERO 7730 // Yaw 轴编码器零位(机械正前方,0~8191)
#define CHASSIS_SPIN_FEEDFORWARD_K 0.008f // 小陀螺解算时延前馈补偿系数(s)
#define GIMBAL_FRICTION_WHEEL_SPEED 5500.0f // 摩擦轮转速(RPM)
#define GIMBAL_RAMMER_SPEED -5400.0f// 拨弹盘转速(RPM,负向发射)
@@ -29,35 +31,43 @@
* 这是反复"疯转"的根源,已废弃;
* - 现在两环共用陀螺,整条链只有一个装配符号,由上电自检自动测定
* (GIMBAL_YAW_DETECT 见下),无需人工猜;
* - 单位:角度环 误差° -> 目标角速度°/s;速度环 误差°/s -> 电压。
* - 单位:角度环 误差° -> 目标角速度°/s;速度环 误差°/s -> 电流。
* 调参顺序:先速度环(点动不振荡),再位置环(刚性)——见移植 README §8.1 */
#define GIMBAL_YAW_ANGLE_KP 15.0f // ° -> °/s:10° 误差给 150°/s
#define GIMBAL_YAW_ANGLE_KP 20.0f // ° -> °/s:10° 误差给 150°/s
#define GIMBAL_YAW_ANGLE_KI 0.0f
#define GIMBAL_YAW_ANGLE_KD 0.0f // 速度环本身即微分,不再叠加
#define GIMBAL_YAW_ANGLE_EK_DEADBAND 0.05f // 误差死区(°),QEKF 噪声小可用窄死区
#define GIMBAL_YAW_ANGLE_OUT_LIMIT 360.0f // 目标角速度上限(°/s)
#define GIMBAL_YAW_SPEED_KP 60.0f // °/s -> 电压:100°/s 误差给 6000(约 24% 满电压)
#define GIMBAL_YAW_SPEED_KP 85.0f // °/s -> 电流:100°/s 误差给 6000(约 36% 满电流)
#define GIMBAL_YAW_SPEED_KI 0.0f // 稳定后可回填 0.5~2 消速度稳态差
#define GIMBAL_YAW_SPEED_KD 0.0f // 陀螺速率反馈噪声小,先不用 D
#define GIMBAL_YAW_SPEED_OUT_LIMIT 25000.0f// GM6020 电压限幅
#define GIMBAL_YAW_SPEED_OUT_LIMIT 16384.0f// GM6020 电流限幅(±16384 对应 ±3A)
#define GIMBAL_YAW_SPIN_FEEDFORWARD_K 24.0f // 小陀螺底盘自旋解耦前馈系数(RPM->电流)
/* Yaw 装配符号自动检测:上电自检时给 Yaw 电机一个正向小电压脉冲,
/* Yaw 装配符号自动检测:上电自检时给 Yaw 电机一个正向小电流脉冲,
* 看陀螺 z 轴往哪边转——脉冲引起同向转动则符号 +1,反向则 -1。
* 检测时云台会轻转几度,勿扶云台;失败(被按住/电机离线)时用 FALLBACK */
#define GIMBAL_YAW_SIGN_AUTO 1 // 1=上电自动检测 0=直接用 FALLBACK
#define GIMBAL_YAW_SIGN_FALLBACK (1.0f)
#define GIMBAL_YAW_DETECT_VOLTAGE 5000 // 检测脉冲电压(约 20% 满电压)
#define GIMBAL_YAW_DETECT_CURRENT 3500 // 检测脉冲电流(约 21% 满电流 16384)
#define GIMBAL_YAW_DETECT_RATE_MIN 20.0f // 判定转动的陀螺速率阈值(°/s)
/* ---- Pitch(位置环陀螺 Roll,速度环转子转速——Pitch 无符号史问题,维持原案) ---- */
#define GIMBAL_PITCH_ANGLE_EK_DEADBAND 0.3f // 位置环误差死区(°)
#define GIMBAL_PITCH_ANGLE_KP 15.0f
#define GIMBAL_PITCH_ANGLE_EK_DEADBAND 0.05f // 误差死区(°),收窄死区消除边缘阶跃
#define GIMBAL_PITCH_ANGLE_KP 40.0f
#define GIMBAL_PITCH_ANGLE_KI 0.0f
#define GIMBAL_PITCH_ANGLE_KD 100.0f
#define GIMBAL_PITCH_SPEED_KP 150.0f
#define GIMBAL_PITCH_SPEED_KI 0.001f
#define GIMBAL_PITCH_SPEED_KD 5.0f
#define GIMBAL_PITCH_ANGLE_KD 0.0f // 原100.0f是万级电流振颤主因!清零以消除剧烈振荡
#define GIMBAL_PITCH_SPEED_KP 100.0f // 速度/电流环Kp
#define GIMBAL_PITCH_SPEED_KI 0.0f
#define GIMBAL_PITCH_SPEED_KD 0.0f
/* Pitch 重力拟合前馈参数: I_g = K_COS * cos(a) + K_SIN * sin(a) + K_CONST
* 其中 a = (raw_angle - ZERO_ECD) * 360 / 8192 (°) */
#define GIMBAL_PITCH_GRAVITY_ZERO_ECD 3200.0f // 重力补偿拟合基准编码值
#define GIMBAL_PITCH_GRAVITY_K_COS 2856.1f// cos 项系数
#define GIMBAL_PITCH_GRAVITY_K_SIN 4340.3f// sin 项系数
#define GIMBAL_PITCH_GRAVITY_K_CONST 2826.5f // 常数偏置项
#define GIMBAL_FRICTION_WHEEL_KP 16.0f
#define GIMBAL_FRICTION_WHEEL_KI 0.0f
@@ -91,10 +101,10 @@
* err = wrap180(云台yaw - 底盘yaw)
* 不再依赖底盘侧 GM6020(0x205) 反馈,皮带虚位不在环内,无基准锁定时序坑。
* 两板 INS 各自上电零点任意,但差值只随相对转动变化,天然正确 */
#define CHASSIS_FOLLOW_KP 0.4f // w 量纲/°:10° 偏差给 w=4
#define CHASSIS_FOLLOW_KP 0.4678f // w 量纲/°:10° 偏差给 w=4
#define CHASSIS_FOLLOW_KI 0.0f // 调试期 0,同旧教训(积分残留)
#define CHASSIS_FOLLOW_KD 0.0f
#define CHASSIS_FOLLOW_OUT_LIMIT 4.0f // 输出限幅(介于慢/快陀螺之间)
#define CHASSIS_FOLLOW_KD 24.452f
#define CHASSIS_FOLLOW_OUT_LIMIT 5.5f // 输出限幅(介于慢/快陀螺之间)
#define CHASSIS_FOLLOW_DEADBAND 1.0f // 误差死区(°)
/* 跟随符号全自动综合:云台自检(0x1A9 flags)下发编码器 tick 增向,
@@ -114,10 +124,11 @@
#define CTOC_SLAVE_ID1 0x149 // 云台->底盘:摇杆数据
#define CTOC_SLAVE_ID2 0x189 // 云台->底盘:控制状态+故障/陀螺使能位
#define CTOC_SLAVE_ID3 0x1A9 // 云台->底盘:云台世界系 yaw(float)+att_ready
#define CTOC_SLAVE_ID4 0x1B9 // 云台->底盘:UI 数据(pitch + 摩擦轮 L/R 转速)
/* ============================ CAN ID ============================ */
/* 云台板:CAN1 = Pitch GM6020(0x206)+摩擦轮 M3508(0x201/0x202)
* CAN2 = Yaw GM6020(0x205)+底盘回传(0x019)
/* 云台板:CAN1 = Pitch GM6020(0x206,0x1FE)+摩擦轮 M3508(0x201/0x202,0x200)
* CAN2 = Yaw GM6020(0x205,0x1FE)+拨弹 M2006(0x201,0x200)+底盘回传(0x019)
* 底盘板:CAN1 = 四轮 M3508(0x201~0x204)
* CAN2 = 云台数据(0x149/0x189/0x1A9) */
@@ -125,10 +136,10 @@
#define DEBUG_SHOOT_WITHOUT_REFEREE 1 // 1=无裁判系统时也允许开摩擦轮(台架调试用),比赛请改 0
#define GIMBAL_RAMMER_INSTALLED 0 // 1=拨弹 M2006 已安装;0=暂缺,不参与掉线判定
/* 1=调试模式:把 CAN 掉线警告音替换成循环播放的旋律(台架调试时避免连续滴滴声
* 干扰)。红灯常亮与其它灯语完全不变,仍能看出是哪台设备掉线;比赛请改 0。
* 旋律音符表见 modules/BUZZER/buzzer.c 的 buzzer_melody[] */
#define DEBUG_BUZZER_MELODY 1
/* 1=把 CAN 掉线警告音替换成循环播放的旋律《你》(RM动画片尾曲),报警时播放;
* 旋律音符表见 modules/dev/buzzer.c 的 buzzer_melody[] */
#define DEBUG_BUZZER_MELODY 0
#define BUZZER_MELODY_SPEED_DIV 1 // 旋律降速分频(默认1:每步100ms精准匹配原版带吐音断音节拍)
/* ============================ 掉线检测 ============================ */
#define DEVICE_OFFLINE_TIME_MS 100 // CAN 设备/裁判系统掉线判定时间
底盘/MDK-ARM/Simba-ELCT-FrameWork.uvoptx
+27 -15
View File
@@ -103,7 +103,7 @@
<bEvRecOn>1</bEvRecOn>
<bSchkAxf>0</bSchkAxf>
<bTchkAxf>0</bTchkAxf>
<nTsel>3</nTsel>
<nTsel>2</nTsel>
<sDll></sDll>
<sDllPa></sDllPa>
<sDlgDll></sDlgDll>
@@ -1246,6 +1246,18 @@
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
<bDave2>0</bDave2>
<PathWithFileName>..\modules\comms\referee_ui.c</PathWithFileName>
<FilenameWithoutPath>referee_ui.c</FilenameWithoutPath>
<RteFlg>0</RteFlg>
<bShared>0</bShared>
</File>
<File>
<GroupNumber>10</GroupNumber>
<FileNumber>82</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
<bDave2>0</bDave2>
<PathWithFileName>..\modules\dev\led.c</PathWithFileName>
<FilenameWithoutPath>led.c</FilenameWithoutPath>
<RteFlg>0</RteFlg>
@@ -1253,7 +1265,7 @@
</File>
<File>
<GroupNumber>10</GroupNumber>
<FileNumber>82</FileNumber>
<FileNumber>83</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1265,7 +1277,7 @@
</File>
<File>
<GroupNumber>10</GroupNumber>
<FileNumber>83</FileNumber>
<FileNumber>84</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1277,7 +1289,7 @@
</File>
<File>
<GroupNumber>10</GroupNumber>
<FileNumber>84</FileNumber>
<FileNumber>85</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1289,7 +1301,7 @@
</File>
<File>
<GroupNumber>10</GroupNumber>
<FileNumber>85</FileNumber>
<FileNumber>86</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1301,7 +1313,7 @@
</File>
<File>
<GroupNumber>10</GroupNumber>
<FileNumber>86</FileNumber>
<FileNumber>87</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1313,7 +1325,7 @@
</File>
<File>
<GroupNumber>10</GroupNumber>
<FileNumber>87</FileNumber>
<FileNumber>88</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1325,7 +1337,7 @@
</File>
<File>
<GroupNumber>10</GroupNumber>
<FileNumber>88</FileNumber>
<FileNumber>89</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1337,7 +1349,7 @@
</File>
<File>
<GroupNumber>10</GroupNumber>
<FileNumber>89</FileNumber>
<FileNumber>90</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1349,7 +1361,7 @@
</File>
<File>
<GroupNumber>10</GroupNumber>
<FileNumber>90</FileNumber>
<FileNumber>91</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1369,7 +1381,7 @@
<RteFlg>0</RteFlg>
<File>
<GroupNumber>11</GroupNumber>
<FileNumber>91</FileNumber>
<FileNumber>92</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1381,7 +1393,7 @@
</File>
<File>
<GroupNumber>11</GroupNumber>
<FileNumber>92</FileNumber>
<FileNumber>93</FileNumber>
<FileType>1</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1393,7 +1405,7 @@
</File>
<File>
<GroupNumber>11</GroupNumber>
<FileNumber>93</FileNumber>
<FileNumber>94</FileNumber>
<FileType>5</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1405,7 +1417,7 @@
</File>
<File>
<GroupNumber>11</GroupNumber>
<FileNumber>94</FileNumber>
<FileNumber>95</FileNumber>
<FileType>5</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
@@ -1425,7 +1437,7 @@
<RteFlg>0</RteFlg>
<File>
<GroupNumber>12</GroupNumber>
<FileNumber>95</FileNumber>
<FileNumber>96</FileNumber>
<FileType>4</FileType>
<tvExp>0</tvExp>
<tvExpOptDlg>0</tvExpOptDlg>
底盘/MDK-ARM/Simba-ELCT-FrameWork.uvprojx
+5
View File
@@ -2363,6 +2363,11 @@
<FileType>1</FileType>
<FilePath>..\modules\comms\referee.c</FilePath>
</File>
<File>
<FileName>referee_ui.c</FileName>
<FileType>1</FileType>
<FilePath>..\modules\comms\referee_ui.c</FilePath>
</File>
<File>
<FileName>led.c</FileName>
<FileType>1</FileType>
底盘/modules/comms/c_comm.c
+22
View File
@@ -23,6 +23,13 @@ static volatile uint32_t ctoc_att_last_tick = 0;
/* 云台自检下发的编码器方向:+1=tick增向CCW -1=CW 0=未检测(0x1A9 flags) */
volatile int8_t ctoc_encoder_ccw = 0;
/* ---- 0x1B9 自定义UI 专用量(云台提供,底盘本地没有) ---- */
volatile float ctoc_ui_pitch_deg = 0.0f;
volatile float ctoc_ui_fric_l_rpm = 0.0f;
volatile float ctoc_ui_fric_r_rpm = 0.0f;
volatile uint8_t ctoc_ui_spin_flag = 0;
volatile uint32_t ctoc_ui_last_tick = 0;
/* 0x1A9 帧新鲜判定(两板公共:底盘跟随用它门控,云台留作诊断) */
uint8_t ctoc_att_fresh(void)
{
@@ -179,11 +186,26 @@ static void c_comm_rx_0x1a9(uint32_t std_id, const uint8_t rx_data[8], uint32_t
ctoc_att_last_tick = HAL_GetTick();
}
/* 0x1B9 云台->底盘:自定义UI 需要而底盘本地没有的量
* [0..1] pitch(0.01°) [2..3] 左摩擦轮(rpm/100) [4..5] 右摩擦轮(rpm/100)
* [6] bit0=小陀螺使能 */
static void c_comm_rx_0x1b9(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc)
{
(void)std_id;
(void)dlc;
ctoc_ui_pitch_deg = (float)(int16_t)(((uint16_t)rx_data[1] << 8) | rx_data[0]) * 0.01f;
ctoc_ui_fric_l_rpm = (float)(int16_t)(((uint16_t)rx_data[3] << 8) | rx_data[2]) * 100.0f;
ctoc_ui_fric_r_rpm = (float)(int16_t)(((uint16_t)rx_data[5] << 8) | rx_data[4]) * 100.0f;
ctoc_ui_spin_flag = rx_data[6] & 0x01;
ctoc_ui_last_tick = HAL_GetTick();
}
void c_comm_init(void)
{
can_rx_register(&hcan2, CTOC_SLAVE_ID1, c_comm_rx_0x149);
can_rx_register(&hcan2, CTOC_SLAVE_ID2, c_comm_rx_0x189);
can_rx_register(&hcan2, CTOC_SLAVE_ID3, c_comm_rx_0x1a9);
can_rx_register(&hcan2, CTOC_SLAVE_ID4, c_comm_rx_0x1b9);
}
void c_comm_slave_send(uint8_t motor_fault)
底盘/modules/comms/c_comm.h
+12
View File
@@ -63,6 +63,18 @@ extern volatile int8_t ctoc_encoder_ccw;
/* 底盘板:0x1A9 帧是否新鲜(掉线检测) */
extern uint8_t ctoc_att_fresh(void);
/* ---- 0x1B9 云台->底盘:自定义UI 专用数据 ---------------------------------
* 底盘本地没有、但 UI 要显示的量(见 referee_ui):pitch 角度与左右摩擦轮转速。
* 单位:0.01° / rpm(×100 压缩成 int16 传输) */
extern volatile float ctoc_ui_pitch_deg;
extern volatile float ctoc_ui_fric_l_rpm;
extern volatile float ctoc_ui_fric_r_rpm;
extern volatile uint8_t ctoc_ui_spin_flag;
extern volatile uint32_t ctoc_ui_last_tick;
/* 云台板:发送 0x1B9 UI 数据帧(2ms 周期或按需,c_comm_task 调用) */
extern void c_comm_master_send_ui(float pitch_deg, float fric_l_rpm, float fric_r_rpm, uint8_t spin_on);
/* 注册 CAN 接收回调(can_start() 之后调用) */
extern void c_comm_init(void);
底盘/modules/comms/referee.c
+45
View File
@@ -216,3 +216,48 @@ void referee_parse_bytes(const uint8_t * data, uint16_t len)
while (len--)
referee_parse_byte(*data++);
}
/* ============================================================================
* 发送:裁判系统帧(机器人 -> 裁判系统 -> 选手端)
* 帧: A5 | data_length(2,LE,=payload 字节数,不含 cmd_id) | seq | CRC8
* | cmd_id(2,LE) | data | CRC16(2,LE,低字节先)
* CRC8 覆盖前 4 字节;CRC16 覆盖除末 2 字节外全部。
* 自定义UI 走 cmd 0x0301(payload 首 6 字节为 data_cmd_id/sender_ID/receiver_ID)。
* USART6 TX DMA:静态缓冲,发送期间不得被覆盖;UI 刷新率 5Hz 远低于链路能力。
* ==========================================================================*/
#include "bsp_usart.h"
static uint8_t ref_tx_seq = 0;
void referee_send_frame(uint16_t cmd_id, const uint8_t * data, uint16_t len)
{
static uint8_t frame[REF_FRAME_MAX_LEN];
uint16_t i = 0;
if (len > (uint16_t)(REF_FRAME_MAX_LEN - 9) || data == NULL)
return;
frame[i++] = 0xA5;
frame[i++] = (uint8_t)(len & 0xFF);
frame[i++] = (uint8_t)(len >> 8);
frame[i++] = ref_tx_seq++;
uint8_t crc8 = 0xFF;
for (uint16_t k = 0; k < 4; k++)
crc8 = crc8_update(crc8, frame[k]);
frame[i++] = crc8;
frame[i++] = (uint8_t)(cmd_id & 0xFF);
frame[i++] = (uint8_t)(cmd_id >> 8);
for (uint16_t k = 0; k < len; k++)
frame[i++] = data[k];
uint16_t crc16 = 0xFFFF;
for (uint16_t k = 0; k < i; k++)
crc16 = crc16_update(crc16, frame[k]);
frame[i++] = (uint8_t)(crc16 & 0xFF);
frame[i++] = (uint8_t)(crc16 >> 8);
usart6_tx_dma_enable(frame, i);
}
底盘/modules/comms/referee.h
+6
View File
@@ -30,4 +30,10 @@ extern void referee_parse_bytes(const uint8_t * data, uint16_t len);
typedef void (*referee_keyboard_hook_f)(const uint8_t data[12]);
extern void referee_set_keyboard_hook(referee_keyboard_hook_f hook);
/* ---- 发送(机器人 -> 裁判系统/选手端) -------------------------------------
* 用于自定义UI(0x0301 机器人交互数据)。data_length 取 payload 字节数(不含 cmd_id,
* 与解析器一致);CRC8 覆盖前 4 字节,CRC16 覆盖除末 2 字节外全部(低字节先)。
* 内部静态缓冲 + USART6 TX DMA,立即返回,勿高频调用(链路 115200)。 */
extern void referee_send_frame(uint16_t cmd_id, const uint8_t * data, uint16_t len);
#endif
底盘/modules/comms/referee_ui.c
+243
View File
@@ -0,0 +1,243 @@
/* =============================================================================
* referee_ui.c - 裁判系统自定义UI组包与发送(版式见 referee_ui.h / hud_mock5.png)
*
* 组包: 每包 = ext_student_interactive_header_data_t{data_cmd_id, sender_ID,
* receiver_ID} + N×15 字节图形数据,N 由 data_cmd_id 决定(1/2/5/7)。
* 图形名用 3 字符自增计数器(base36)保证唯一;首轮 ADD,之后 MODIFY。
* 发送: referee_send_frame(0x0301, payload, 6 + N*15) -> USART6 DMA
* ==========================================================================*/
#include "referee_ui.h"
#include "referee.h"
#include "robot_param.h"
#include <string.h>
/* 协议要求:图形数据恰好 15 字节(头 11 + 尾 4)。若 pack(1) 失效或位域被重排,
* 这里直接编译失败,而不是把错位的图形发给选手端。 */
_Static_assert(sizeof(ui_head_t) == 11, "ui_head_t 必须是 11 字节");
_Static_assert(sizeof(ui_draw_t) == 15, "ui_draw_t 必须是 15 字节");
_Static_assert(sizeof(ui_num_t) == 15, "ui_num_t 必须是 15 字节");
_Static_assert(sizeof(ui_graphic_t) == 15, "ui_graphic_t 必须是 15 字节");
/* ---- 图形名生成:base26 三字符(17576 个组合,足够) ---- */
static uint16_t ui_name_seq = 0;
static void ui_next_name(uint8_t name[3])
{
uint16_t v = ui_name_seq++;
name[0] = (uint8_t)('A' + (v / 676) % 26);
name[1] = (uint8_t)('A' + (v / 26) % 26);
name[2] = (uint8_t)('A' + v % 26);
}
/* ---- 打包缓冲 ---- */
#define UI_PAYLOAD_MAX (6 + UI_MAX_PER_PACKET * sizeof(ui_graphic_t))
static uint8_t ui_pkt[UI_PAYLOAD_MAX];
static uint8_t ui_pkt_n; /* 当前包里的图形个数 */
static uint8_t ui_op = UI_OP_ADD; /* 首轮 ADD,之后 MOD */
static uint8_t ui_ready = 0; /* 首轮是否已发完 */
static void ui_flush(void)
{
if (ui_pkt_n == 0)
return;
uint16_t cmd;
switch (ui_pkt_n)
{
case 1: cmd = UI_CMD_1; break;
case 2: cmd = UI_CMD_2; break;
case 5: cmd = UI_CMD_5; break;
case 7: cmd = UI_CMD_7; break;
default: return; /* 协议只支持 1/2/5/7,不该发生 */
}
/* header: data_cmd_id / sender_ID / receiver_ID,均小端 */
ui_pkt[0] = (uint8_t)(cmd & 0xFF);
ui_pkt[1] = (uint8_t)(cmd >> 8);
uint16_t sid = (uint16_t)referee.robot_id;
ui_pkt[2] = (uint8_t)(sid & 0xFF);
ui_pkt[3] = (uint8_t)(sid >> 8);
ui_pkt[4] = (uint8_t)(UI_RECEIVER_ID & 0xFF);
ui_pkt[5] = (uint8_t)(UI_RECEIVER_ID >> 8);
referee_send_frame(UI_CMD_BASE, ui_pkt, (uint16_t)(6 + ui_pkt_n * sizeof(ui_graphic_t)));
ui_pkt_n = 0;
}
static ui_graphic_t * ui_new(uint8_t type, uint8_t layer, uint8_t color)
{
if (ui_pkt_n >= UI_MAX_PER_PACKET)
ui_flush();
ui_graphic_t * g = (ui_graphic_t *)&ui_pkt[6 + ui_pkt_n * sizeof(ui_graphic_t)];
memset(g, 0, sizeof(*g));
ui_next_name(g->d.h.name); /* d.h 与 n.h 同址 */
g->d.h.type = type;
g->d.h.layer = layer;
g->d.h.color = color;
g->d.h.operate = ui_op;
ui_pkt_n++;
return g;
}
/* ---- 图元封装(绘制类写 d.*,数值类写 n.val) ---- */
static void ui_line(uint8_t layer, uint8_t color, int x0, int y0, int x1, int y1, int w)
{
ui_graphic_t * g = ui_new(UI_T_LINE, layer, color);
g->d.h.x0 = (uint32_t)x0; g->d.h.y0 = (uint32_t)y0;
g->d.x1 = (uint32_t)x1; g->d.y1 = (uint32_t)y1;
g->d.h.width = (uint32_t)w;
}
static void ui_rect(uint8_t layer, uint8_t color, int x0, int y0, int x1, int y1)
{
ui_graphic_t * g = ui_new(UI_T_RECT, layer, color);
g->d.h.x0 = (uint32_t)x0; g->d.h.y0 = (uint32_t)y0;
g->d.x1 = (uint32_t)x1; g->d.y1 = (uint32_t)y1;
}
static void ui_fval(uint8_t layer, uint8_t color, int x, int y, float v, int digits)
{
ui_graphic_t * g = ui_new(UI_T_FLOAT, layer, color);
g->n.h.x0 = (uint32_t)x; g->n.h.y0 = (uint32_t)y;
g->n.h.width = (uint32_t)digits; /* 浮点:小数位数 */
g->n.val.f = v;
}
static void ui_ival(uint8_t layer, uint8_t color, int x, int y, int32_t v)
{
ui_graphic_t * g = ui_new(UI_T_INT, layer, color);
g->n.h.x0 = (uint32_t)x; g->n.h.y0 = (uint32_t)y;
g->n.val.i = v;
}
static void ui_char(uint8_t layer, uint8_t color, int x, int y, const char * s)
{
ui_graphic_t * g = ui_new(UI_T_CHAR, layer, color);
g->n.h.x0 = (uint32_t)x; g->n.h.y0 = (uint32_t)y;
g->n.h.width = (uint32_t)strlen(s);
for (int i = 0; i < 4; i++) /* 最多 4 字节 ASCII */
g->n.val.s[i] = s[i];
}
/* 角度归一到 [0,360) */
static float ui_norm360(float a)
{
while (a < 0.0f) a += 360.0f;
while (a >= 360.0f) a -= 360.0f;
return a;
}
void referee_ui_update(const ui_data_t * d)
{
if (d == NULL)
return;
/* 裁判系统离线:发一轮删除图层,然后停发(避免选手端残留最后一帧) */
if (!d->ref_online)
{
if (ui_ready)
{
ui_pkt_n = 0;
ui_graphic_t * g = ui_new(UI_T_RECT, UI_L_FRAME, UI_C_BLACK);
g->d.h.operate = UI_OP_DEL;
g->d.h.x0 = 0; g->d.h.y0 = 0; g->d.x1 = 0; g->d.y1 = 0;
ui_flush();
ui_ready = 0;
ui_name_seq = 0;
ui_op = UI_OP_ADD;
}
return;
}
/* ---------------- 左上:预估底盘功率 ---------------- */
uint8_t pw_col = (d->pwr_w > d->pwr_limit_w) ? UI_C_RED
: (d->pwr_w > d->pwr_limit_w * 0.8f) ? UI_C_ORANGE : UI_C_GREEN;
ui_rect(UI_L_FRAME, UI_C_CYAN, UI_PWR_X0, UI_PWR_Y0, UI_PWR_X1, UI_PWR_Y0 + 4);
ui_char(UI_L_TEXT, UI_C_CYAN, UI_PWR_X0 + 20, UI_PWR_Y0 + 30, "PWR");
ui_fval(UI_L_TEXT, UI_C_WHITE, UI_PWR_X0 + 20, UI_PWR_Y0 + 64, d->pwr_w, 1);
ui_char(UI_L_TEXT, UI_C_WHITE, UI_PWR_X0 + 210, UI_PWR_Y0 + 84, "W");
int pw_w_px = (int)((UI_PWR_X1 - UI_PWR_X0 - 40) * (d->pwr_w / (d->pwr_limit_w > 1.0f ? d->pwr_limit_w : 1.0f)));
if (pw_w_px > UI_PWR_X1 - UI_PWR_X0 - 40) pw_w_px = UI_PWR_X1 - UI_PWR_X0 - 40;
if (pw_w_px < 0) pw_w_px = 0;
ui_rect(UI_L_GAUGE, pw_col, UI_PWR_X0 + 20, UI_PWR_Y0 + 120, UI_PWR_X0 + 20 + pw_w_px, UI_PWR_Y0 + 142);
ui_line(UI_L_GAUGE, UI_C_WHITE, UI_PWR_X0 + 20 + (UI_PWR_X1 - UI_PWR_X0 - 40) - 3, UI_PWR_Y0 + 116,
UI_PWR_X0 + 20 + (UI_PWR_X1 - UI_PWR_X0 - 40) - 3, UI_PWR_Y0 + 146, 2);
/* ---------------- 左中:超级电容 ---------------- */
uint8_t cap_col = (d->cap_pct < 15) ? UI_C_RED : (d->cap_pct < 40) ? UI_C_ORANGE : UI_C_CYAN;
ui_rect(UI_L_FRAME, cap_col, UI_CAP_X0, UI_CAP_Y0, UI_CAP_X1, UI_CAP_Y0 + 4);
ui_char(UI_L_TEXT, cap_col, UI_CAP_X0 + 20, UI_CAP_Y0 + 30, "CAP");
ui_ival(UI_L_TEXT, UI_C_WHITE, UI_CAP_X0 + 20, UI_CAP_Y0 + 64, (int32_t)d->cap_pct);
ui_char(UI_L_TEXT, UI_C_WHITE, UI_CAP_X0 + 130, UI_CAP_Y0 + 84, "%");
int cap_px = (int)((UI_CAP_X1 - UI_CAP_X0 - 40) * (d->cap_pct / 100.0f));
ui_rect(UI_L_GAUGE, cap_col, UI_CAP_X0 + 20, UI_CAP_Y0 + 118, UI_CAP_X0 + 20 + cap_px, UI_CAP_Y0 + 140);
/* ---------------- 顶部:罗盘刻度带(底盘正方向朝向) ---------------- */
{
float h = ui_norm360(d->hdg_deg);
ui_rect(UI_L_FRAME, UI_C_CYAN, UI_HDG_X0, UI_HDG_Y0, UI_HDG_X1, UI_HDG_Y0 + 4);
ui_line(UI_L_FRAME, UI_C_CYAN, UI_HDG_X0 + 20, UI_HDG_Y0 + 62, UI_HDG_X1 - 20, UI_HDG_Y0 + 62, 2);
int cx = (UI_HDG_X0 + UI_HDG_X1) / 2;
for (int k = -1; k <= 1; k++) /* 3 条刻度 */
{
int x = cx + k * (UI_HDG_TAPE_HALF / 2);
ui_line(UI_L_FRAME, UI_C_CYAN, x, UI_HDG_Y0 + 40, x, UI_HDG_Y0 + 62, k == 0 ? 3 : 2);
}
ui_ival(UI_L_TEXT, UI_C_CYAN, cx - UI_HDG_TAPE_HALF / 2 - 24, UI_HDG_Y0 + 18,
(int32_t)ui_norm360(h - 30.0f));
ui_ival(UI_L_TEXT, UI_C_CYAN, cx + UI_HDG_TAPE_HALF / 2 - 24, UI_HDG_Y0 + 18,
(int32_t)ui_norm360(h + 30.0f));
ui_line(UI_L_FRAME, UI_C_WHITE, cx, UI_HDG_Y0 + 62, cx - 8, UI_HDG_Y0 + 50, 2);
ui_line(UI_L_FRAME, UI_C_WHITE, cx, UI_HDG_Y0 + 62, cx + 8, UI_HDG_Y0 + 50, 2);
ui_char(UI_L_TEXT, UI_C_CYAN, UI_HDG_X0 + 24, UI_HDG_Y0 + 70, "HDG");
ui_ival(UI_L_TEXT, UI_C_WHITE, UI_HDG_X0 + 90, UI_HDG_Y0 + 66, (int32_t)h);
ui_char(UI_L_TEXT, UI_C_CYAN, UI_HDG_X1 - 170, UI_HDG_Y0 + 70, "YAW");
ui_ival(UI_L_TEXT, UI_C_WHITE, UI_HDG_X1 - 104, UI_HDG_Y0 + 66, (int32_t)ui_norm360(d->yaw_deg));
}
/* ---------------- 中央:俯仰梯 ---------------- */
ui_line(UI_L_FRAME, UI_C_WHITE, UI_LAD_CX - 44, UI_LAD_CY, UI_LAD_CX - 14, UI_LAD_CY, 4);
ui_line(UI_L_FRAME, UI_C_WHITE, UI_LAD_CX + 14, UI_LAD_CY, UI_LAD_CX + 44, UI_LAD_CY, 4);
for (int i = -2; i <= 2; i++) /* ±10/±5/0 五条梯线 */
{
if (i == 0) continue;
int v = i * 5;
int yy = UI_LAD_CY - v * UI_LAD_PX_PER_DEG;
int half = (i % 2 == 0) ? UI_LAD_HALF_LONG : UI_LAD_HALF_SHORT;
ui_line(UI_L_GAUGE, UI_C_CYAN, UI_LAD_CX - half, yy, UI_LAD_CX - 18, yy, 2);
ui_line(UI_L_GAUGE, UI_C_CYAN, UI_LAD_CX + 18, yy, UI_LAD_CX + half, yy, 2);
}
ui_ival(UI_L_TEXT, UI_C_CYAN, UI_LAD_CX - UI_LAD_HALF_SHORT - 40, UI_LAD_CY - 10 * UI_LAD_PX_PER_DEG - 10, 10);
ui_ival(UI_L_TEXT, UI_C_CYAN, UI_LAD_CX + UI_LAD_HALF_SHORT + 12, UI_LAD_CY - 10 * UI_LAD_PX_PER_DEG - 10, 10);
{
int py = UI_LAD_CY - (int)(d->pitch_deg * UI_LAD_PX_PER_DEG);
ui_line(UI_L_GAUGE, UI_C_ORANGE, UI_LAD_CX - UI_LAD_HALF_LONG - 20, py, UI_LAD_CX - UI_LAD_HALF_LONG - 4, py, 4);
ui_char(UI_L_TEXT, UI_C_ORANGE, UI_LAD_CX - UI_LAD_HALF_LONG - 132, py - 10, "PIT");
ui_fval(UI_L_TEXT, UI_C_WHITE, UI_LAD_CX - UI_LAD_HALF_LONG - 76, py - 14, d->pitch_deg, 1);
}
/* ---------------- 右上:摩擦轮速度 ---------------- */
{
uint8_t f_col = (d->fric_l_rpm > 1000.0f && d->fric_r_rpm > 1000.0f) ? UI_C_GREEN : UI_C_ORANGE;
ui_rect(UI_L_FRAME, f_col, UI_FRIC_X0, UI_FRIC_Y0, UI_FRIC_X1, UI_FRIC_Y0 + 4);
ui_char(UI_L_TEXT, UI_C_CYAN, UI_FRIC_X0 + 24, UI_FRIC_Y0 + 34, "FRIC");
ui_ival(UI_L_TEXT, UI_C_WHITE, UI_FRIC_X0 + 24, UI_FRIC_Y0 + 74, (int32_t)d->fric_l_rpm);
ui_ival(UI_L_TEXT, UI_C_WHITE, UI_FRIC_X0 + 250, UI_FRIC_Y0 + 74, (int32_t)d->fric_r_rpm);
ui_char(UI_L_TEXT, f_col, UI_FRIC_X0 + 24, UI_FRIC_Y1 - 60,
(d->fric_l_rpm > 1000.0f && d->fric_r_rpm > 1000.0f) ? "ARMED" : "IDLE");
int bl = (int)((UI_FRIC_Y1 - UI_FRIC_Y0 - 140) * (d->fric_l_rpm / 7000.0f));
int br = (int)((UI_FRIC_Y1 - UI_FRIC_Y0 - 140) * (d->fric_r_rpm / 7000.0f));
if (bl < 0) bl = 0; if (bl > UI_FRIC_Y1 - UI_FRIC_Y0 - 140) bl = UI_FRIC_Y1 - UI_FRIC_Y0 - 140;
if (br < 0) br = 0; if (br > UI_FRIC_Y1 - UI_FRIC_Y0 - 140) br = UI_FRIC_Y1 - UI_FRIC_Y0 - 140;
ui_rect(UI_L_GAUGE, UI_C_GREEN, UI_FRIC_X0 + 30, UI_FRIC_Y1 - 40 - bl, UI_FRIC_X0 + 74, UI_FRIC_Y1 - 40);
ui_rect(UI_L_GAUGE, UI_C_GREEN, UI_FRIC_X0 + 256, UI_FRIC_Y1 - 40 - br, UI_FRIC_X0 + 300, UI_FRIC_Y1 - 40);
}
/* ---------------- 底部:小陀螺状态 ---------------- */
ui_rect(UI_L_FRAME, d->spin_on ? UI_C_GREEN : UI_C_CYAN, UI_SPIN_X0, UI_SPIN_Y0, UI_SPIN_X1, UI_SPIN_Y0 + 4);
ui_char(UI_L_TEXT, UI_C_CYAN, UI_SPIN_X0 + 24, UI_SPIN_Y0 + 34, "SPIN");
if (d->spin_on)
ui_rect(UI_L_GAUGE, UI_C_GREEN, UI_SPIN_X0 + 160, UI_SPIN_Y0 + 26, UI_SPIN_X0 + 268, UI_SPIN_Y0 + 66);
ui_char(UI_L_TEXT, d->spin_on ? UI_C_BLACK : UI_C_WHITE, UI_SPIN_X0 + 184, UI_SPIN_Y0 + 36,
d->spin_on ? "ON" : "OFF");
/* 收尾:最后一包;首轮发完切换为 MODIFY */
ui_flush();
if (!ui_ready)
{
ui_ready = 1;
ui_op = UI_OP_MOD;
}
}
底盘/modules/comms/referee_ui.h
+159
View File
@@ -0,0 +1,159 @@
#ifndef REFEREE_UI_H
#define REFEREE_UI_H
#include <stdint.h>
/* ============================================================================
* referee_ui.h - 裁判系统"自定义UI"(机器人 -> 选手端 图形绘制)
*
* 通道: 底盘板 USART6(裁判系统) --cmd 0x0301 机器人交互数据--> 选手端叠加显示
* 依据: 裁判系统串口协议 自定义UI 章节 + ARUW Taproot / Triton TR-mbed 两套实现
* 版式: 详见 E:\\ELCT\\_mcp_recon\\hud_mock5.png(坐标与本文 UI_* 宏一一对应)
*
* 硬约束(协议):
* 1. 一条消息最多携带 7 个图形(0x0101/0x0102/0x0103/0x0104 = 1/2/5/7 个)
* 2. 图形总数有限,且图形用"名称"标识 -> 首轮用 ADD,之后一律 MODIFY,
* 否则会在选手端把图形表撑爆
* 3. 图层数 0~9;坐标原点在屏幕左上角,x 向右、y 向下,画布 1920x1080
* 4. 不得绘制官方保留区(顶部比分条 / 左下小地图 / 右下战车模块 / 中部两块保留)
* 5. 协议无"圆角矩形/渐变/图标"原语,只能用 线/矩形/圆/椭圆/弧 + 数值/字符
* ==========================================================================*/
/* ---- 图形数据 -------------------------------------------------------------
* 绘制类(线/矩形/圆/椭圆/弧) 与 数值类(浮点/整型/字符) 都是 15 字节:
* 头 11 字节(所有类型共用): name[3] + operate:3 type:3 layer:4 color:4
* sa:9 ea:9 width:10 x0:11 y0:11
* 后 4 字节: 绘制类 = radius:10 x1:11 y1:11;数值类 = 一个 float/int32/char[4]
* 所以用"共用头 + 联合体"表达,两种视图都是 15 字节。
* 必须 pack(1):否则位域会对齐到 4 字节,整体变 16 字节。 */
#pragma pack(push, 1)
typedef struct
{
uint8_t name[3]; /* 图形名(3 字节 ASCII) */
uint32_t operate : 3; /* UI_OP_* 空/加/改/删 */
uint32_t type : 3; /* UI_T_* 图形类型 */
uint32_t layer : 4; /* UI_L_* 图层 0~9 */
uint32_t color : 4; /* UI_C_* 颜色 */
uint32_t sa : 9; /* 起始角(弧/椭圆) */
uint32_t ea : 9; /* 结束角 */
uint32_t width : 10; /* 线宽 / 小数位 / 字符串长度 */
uint32_t x0 : 11; /* 起点 x */
uint32_t y0 : 11; /* 起点 y */
} ui_head_t; /* 3 + 8 = 11 字节 */
typedef struct { ui_head_t h; uint32_t radius : 10, x1 : 11, y1 : 11; } ui_draw_t;
typedef struct { ui_head_t h; union { float f; int32_t i; char s[4]; } val; } ui_num_t;
typedef union
{
ui_draw_t d; /* 绘制类视图 */
ui_num_t n; /* 数值类视图 */
uint8_t raw[15];
} ui_graphic_t;
#pragma pack(pop)
/* ---- 命令 / 操作码 / 图形类型 -------------------------------------------- */
#define UI_CMD_BASE 0x0301 /* 机器人交互数据 */
#define UI_CMD_1 0x0101
#define UI_CMD_2 0x0102
#define UI_CMD_5 0x0103
#define UI_CMD_7 0x0104
#define UI_MAX_PER_PACKET 7
#define UI_OP_NOP 0
#define UI_OP_ADD 1
#define UI_OP_MOD 2 /* 稳态刷新一律用它 */
#define UI_OP_DEL 3
#define UI_T_LINE 0
#define UI_T_RECT 1
#define UI_T_CIRCLE 2
#define UI_T_ELLIPSE 3
#define UI_T_ARC 4
#define UI_T_FLOAT 5
#define UI_T_INT 6
#define UI_T_CHAR 7
/* ---- 颜色(官方 0~8) ------------------------------------------------------ */
#define UI_C_RED 0
#define UI_C_YELLOW 1
#define UI_C_GREEN 2
#define UI_C_ORANGE 3
#define UI_C_PURPLE 4
#define UI_C_PINK 5
#define UI_C_CYAN 6
#define UI_C_BLACK 7
#define UI_C_WHITE 8
/* ---- 图层(协议 0~9) ------------------------------------------------------ */
#define UI_L_FRAME 0 /* 卡片边框/刻度 */
#define UI_L_GAUGE 1 /* 能量条/进度条 */
#define UI_L_TEXT 2 /* 数值/字符 */
/* ---- 刷新率:5Hz 约 3.8KB/s(115200 链路),协议允许再调高 ---------------- */
#define UI_SEND_HZ 5
/* ---- 发送/接收方 ID -----------------------------------------------------
* sender = 本机机器人 ID(referee.robot_id,无裁判系统时用 0)
* receiver= 选手端/客户端(官方 UI 约定 0x8080);若你的协议版本要求填机器人 ID,
* 改这里一处即可。 */
#define UI_RECEIVER_ID 0x8080
/* ---- 画布 ---------------------------------------------------------------- */
#define UI_SCREEN_W 1920
#define UI_SCREEN_H 1080
/* ---- 版式坐标(与 hud_mock5.png 对应,全部避开官方保留区) ---------------- */
/* 左上:预估底盘功率 */ /* 左上 x56..520 y176..386 */
#define UI_PWR_X0 56
#define UI_PWR_Y0 176
#define UI_PWR_X1 520
#define UI_PWR_Y1 386
/* 左中:超级电容 */ /* x56..520 y404..566 */
#define UI_CAP_X0 56
#define UI_CAP_Y0 404
#define UI_CAP_X1 520
#define UI_CAP_Y1 566
/* 顶部:罗盘刻度带(底盘正方向) */ /* x626..1258 y186..270 */
#define UI_HDG_X0 626
#define UI_HDG_Y0 186
#define UI_HDG_X1 1258
#define UI_HDG_Y1 270
#define UI_HDG_TAPE_HALF 216 /* 刻度带半宽(像素,对应 ±30°) */
/* 中央:俯仰梯 */ /* 以屏幕中心为基准 */
#define UI_LAD_CX 960
#define UI_LAD_CY 540
#define UI_LAD_PX_PER_DEG 11 /* 每度 11 像素 */
#define UI_LAD_HALF_LONG 96
#define UI_LAD_HALF_SHORT 62
/* 右上:摩擦轮速度 */ /* x1420..1864 y176..520 */
#define UI_FRIC_X0 1420
#define UI_FRIC_Y0 176
#define UI_FRIC_X1 1864
#define UI_FRIC_Y1 520
/* 底部:小陀螺状态 */ /* x700..1220 y874..1000 */
#define UI_SPIN_X0 700
#define UI_SPIN_Y0 874
#define UI_SPIN_X1 1220
#define UI_SPIN_Y1 1000
/* ---- 输入数据(referee_task 每周期填) ----------------------------------- */
typedef struct
{
float pitch_deg; /* 云台 pitch(来自 CToC) */
float yaw_deg; /* 云台 yaw(来自 CToC 姿态帧) */
float hdg_deg; /* 底盘正方向朝向(本板 att_deg_yaw) */
float pwr_w; /* 底盘实时功率(裁判 0x0202) */
float pwr_limit_w; /* 功率上限(裁判 0x0201) */
float buf_j; /* 缓冲能量/超级电容(J) */
uint8_t cap_pct; /* 电容百分比(0~100) */
float fric_l_rpm; /* 左摩擦轮转速(来自 CToC) */
float fric_r_rpm; /* 右摩擦轮转速 */
uint8_t spin_on; /* 小陀螺使能 */
uint8_t ref_online; /* 裁判系统在线(离线时整屏删图形) */
} ui_data_t;
/* 周期调用(建议 5Hz):组包并发送;裁判系统离线时发一次"删除全部图层" */
extern void referee_ui_update(const ui_data_t * d);
#endif
底盘/modules/control/chassis.c
+51 -13
View File
@@ -14,6 +14,7 @@
* 功率: chassis_control() 的 power_scale 直接缩放四轮输出电流
* ========================================================================== */
#include "chassis.h"
#include <math.h>
#include "pid.h"
#include "filter.h"
#include "attitude.h"
@@ -153,32 +154,30 @@ float chassis_follow_sign(void)
return dbg_follow_sign * (float)ctoc_encoder_ccw;
}
/* 跟随一步:反馈为 Yaw GM6020 编码器相对角(零漂移),输出 w */
/* 跟随一步:反馈为 Yaw GM6020 编码器对齐设定机械零位(4050),输出 w */
float chassis_follow_w(void)
{
/* 尚未收到 0x205 反馈时不锁定基准(避免首帧假偏差),输出 0 */
/* 尚未收到 0x205 反馈时输出 0 */
if (motor_yaw_follow.fdb.last_online_tick == 0)
{
follow_latched = 0;
return 0;
}
if (follow_reset_request || !follow_latched)
if (follow_reset_request)
{
follow_reset_request = 0;
follow_target_tick = (float)motor_yaw_follow.fdb.total_tick;
follow_latched = 1;
PID_PositionClean(&follow_pid);
}
/* 计算当前机械编码值距离设定零位(4050)的最短差值(-4096 ~ +4096) */
int16_t tick_diff = (int16_t)motor_yaw_follow.fdb.raw_angle - (int16_t)YAW_GM6020_ENCODER_ZERO;
if (tick_diff > 4096)
tick_diff -= 8192;
else if (tick_diff < -4096)
tick_diff += 8192;
/* 相对角误差(°):tick 增向按云台自检结果折算为 CCW 正 */
float err_deg = ((float)motor_yaw_follow.fdb.total_tick - follow_target_tick) * 360.0f / 8192.0f;
float err_deg = (float)tick_diff * (360.0f / 8192.0f);
if (ctoc_encoder_ccw < 0)
err_deg = -err_deg;
if (err_deg > 180.0f)
err_deg -= 360.0f;
else if (err_deg < -180.0f)
err_deg += 360.0f;
if (err_deg > -CHASSIS_FOLLOW_DEADBAND && err_deg < CHASSIS_FOLLOW_DEADBAND)
err_deg = 0;
@@ -195,3 +194,42 @@ void chassis_output_zero(void)
{
dji_motor_send_current_low(&hcan1, 0, 0, 0, 0);
}
#ifndef PI
#define PI 3.14159265358979323846f
#endif
void chassis_vector_to_body(float vx_g, float vy_g, float w, float * vx_c, float * vy_c)
{
/* 电机掉线兜底:若无云台编码器反馈,直接直通输出 */
if (motor_yaw_follow.fdb.last_online_tick == 0)
{
*vx_c = vx_g;
*vy_c = vy_g;
return;
}
/* 1. 计算当前机械编码值距离设定零位的最短差值(-4096 ~ +4096) */
int16_t tick_diff = (int16_t)motor_yaw_follow.fdb.raw_angle - (int16_t)YAW_GM6020_ENCODER_ZERO;
if (tick_diff > 4096)
tick_diff -= 8192;
else if (tick_diff < -4096)
tick_diff += 8192;
/* 2. 相对机械角误差(rad):tick 增向按云台自检结果折算为 CCW 正 */
float alpha_rad = (float)tick_diff * (2.0f * PI / 8192.0f);
int8_t enc_sign = (ctoc_encoder_ccw != 0) ? ctoc_encoder_ccw : 1;
if (enc_sign < 0)
alpha_rad = -alpha_rad;
/* 3. 叠加角速度前馈补偿(-kw 消除通信及响应时延滞后) */
float alpha_comp = alpha_rad - (CHASSIS_SPIN_FEEDFORWARD_K * w);
/* 4. 二维旋转矩阵投影(修正正负号: 适配 vx<0前进, vy>0向左 的坐标系定义) */
float cos_a = cosf(alpha_comp);
float sin_a = sinf(alpha_comp);
*vx_c = vx_g * cos_a + vy_g * sin_a;
*vy_c = -vx_g * sin_a + vy_g * cos_a;
}
底盘/modules/control/chassis.h
+5 -1
View File
@@ -46,4 +46,8 @@ extern volatile float dbg_follow_err_deg;
extern volatile float dbg_follow_out;
extern volatile float dbg_follow_sign;
#endif
/* 将以云台为基准的平移速度(vx_g, vy_g)旋转投影到底盘自身坐标系(vx_c, vy_c)
* 无论底盘是否处于小陀螺自旋状态，使 vx_g 始终代表沿云台枪口方向前进 */
extern void chassis_vector_to_body(float vx_g, float vy_g, float w, float * vx_c, float * vy_c);
#endif
底盘/modules/dev/buzzer.c
+63 -10
View File
@@ -6,6 +6,7 @@
* ========================================================================== */
#include "buzzer.h"
#include "tim.h"
#include "robot_param.h"
extern TIM_HandleTypeDef htim4;
@@ -32,7 +33,8 @@ void buzzer_on(buzzer_tone_e tone)
{
__HAL_TIM_SET_PRESCALER(&htim4, buzzer_tone_freq[tone]);
HAL_TIM_GenerateEvent(&htim4, TIM_EVENTSOURCE_UPDATE); // 立即装载 PSC
__HAL_TIM_SET_COMPARE(&htim4, TIM_CHANNEL_3, 5); // 占空比 50%
/* 占空比 30%:抑制高次尖锐谐波,使吉他拨弦音色圆润纯净 */
__HAL_TIM_SET_COMPARE(&htim4, TIM_CHANNEL_3, 3);
}
else
__HAL_TIM_SET_COMPARE(&htim4, TIM_CHANNEL_3, 0);
@@ -44,21 +46,72 @@ void buzzer_off(void)
}
/* ==========================================================================
* 调试用旋律(见 buzzer.h):每步 100ms,空拍 BUZZER_P 为静音。
* 无源蜂鸣器只有单音,这里用"上行分解和弦 + 回落"拼成一句短旋律;选音限定
* 在中音 3 ~ 高音 2,避免刺耳。循环播放不会漏掉"有设备掉线"这一事实,
* 因为红灯常亮由 monitor_task 独立控制,与该旋律无关。
* 改旋律:直接增删这里的音符即可,长度会自动生效。
* 周杰伦《晴天》- 标志性吉他前奏伴奏 Solo (纯享循环版)
* 调式: 1=C,处于 C 板蜂鸣器最佳频响区间(500~1000Hz)
* 结构: 完整还原原曲前奏 4 小节经典木吉他单音分解
* [小节1: Em] 3 2 1 1 2 1 5_ 1 2
* [小节2: C ] 3 2 1 1 2 1 6_ 1 2
* [小节3: G ] 3 2 1 1 2 1 5_ 1 2
* [小节4: D ] 3 2 1 1 2 1 2 3 5 3 2 1 2 -
* 吐音设计: 每个音符保留 BUZZER_P 间隔,模拟吉他真实的清脆拨弦与泛音
* ========================================================================== */
static const buzzer_tone_e buzzer_melody[] = {
BUZZER_M3, BUZZER_M5, BUZZER_M6, BUZZER_H1, BUZZER_P,
BUZZER_M6, BUZZER_H1, BUZZER_H2, BUZZER_P,
BUZZER_H1, BUZZER_M6, BUZZER_M5, BUZZER_M3, BUZZER_P,
/* ---- 小节 1 (Em): 3 2 1 1 2 1 | 5_ 1 2 ---- */
BUZZER_M3, BUZZER_P, // 3 (Mi)
BUZZER_M2, BUZZER_P, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_L5, BUZZER_P, // 低音 5 (Sol)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
/* ---- 小节 2 (C): 3 2 1 1 2 1 | 6_ 1 2 ---- */
BUZZER_M3, BUZZER_P, // 3 (Mi)
BUZZER_M2, BUZZER_P, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_L6, BUZZER_P, // 低音 6 (La)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
/* ---- 小节 3 (G): 3 2 1 1 2 1 | 5_ 1 2 ---- */
BUZZER_M3, BUZZER_P, // 3 (Mi)
BUZZER_M2, BUZZER_P, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_L5, BUZZER_P, // 低音 5 (Sol)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
/* ---- 小节 4 (D): 3 2 1 1 2 1 | 2 3 5 3 2 1 2 - ---- */
BUZZER_M3, BUZZER_P, // 3 (Mi)
BUZZER_M2, BUZZER_P, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M1, // 1 (Do)
BUZZER_M2, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M2, BUZZER_P, // 2 (Re)
BUZZER_M3, // 3 (Mi)
BUZZER_M5, // 5 (Sol)
BUZZER_M3, // 3 (Mi)
BUZZER_M2, // 2 (Re)
BUZZER_M1, BUZZER_P, // 1 (Do)
BUZZER_M2, BUZZER_M2, BUZZER_M2, BUZZER_M2, BUZZER_M2, BUZZER_P, // 2 (Re 长音结音)
BUZZER_P, BUZZER_P, BUZZER_P, BUZZER_P, // 尾部休止 400ms 后循环
};
void buzzer_play_melody(uint16_t step)
{
const uint16_t steps =
(uint16_t)(sizeof(buzzer_melody) / sizeof(buzzer_melody[0]));
buzzer_on(buzzer_melody[step % steps]);
#ifndef BUZZER_MELODY_SPEED_DIV
#define BUZZER_MELODY_SPEED_DIV 1
#endif
buzzer_on(buzzer_melody[(step / BUZZER_MELODY_SPEED_DIV) % steps]);
}
底盘/modules/motor/dji_motor.c
+32 -10
View File
@@ -6,9 +6,8 @@
* (无 legacy 的 +-1 圈限制,底盘小陀螺时 Yaw 可连续旋转),
* 记录 last_online_tick 供掉线检测
* 控制路径(任务上下文):
* dji_motor_send_current_low/high() 0x200 / 0x1FF 电流帧(+/-16384 = 20A/10A)
* dji_motor_send_voltage_high() 0x2FF 电压帧(GM6020 ID5~7)
* 注意 0x1FF 帧为 M3508/M2006 高位电流与 GM6020 低位电压共用,按槽位区分
* dji_motor_send_current_low/high() 0x200 / 0x1FF 电流帧(+/-16384 = 20A/10A)
* dji_motor_send_gm6020_current_low/high() 0x1FE / 0x2FE GM6020 电流帧(+/-16384 = 3A)
* ========================================================================== */
#include "dji_motor.h"
@@ -20,7 +19,8 @@
static dji_motor_t * dji_motor_list[DJI_MOTOR_MAX];
static uint8_t dji_motor_count = 0;
static void dji_motor_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc);
static void dji_motor_can1_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc);
static void dji_motor_can2_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc);
/* 解析一帧反馈,多圈累计(无 ±1 圈限制,底盘小陀螺时 Yaw 电机可连续旋转) */
static void dji_motor_parse(dji_motor_t * motor, const uint8_t data[8])
@@ -71,16 +71,32 @@ void dji_motor_init(dji_motor_t * motor, hcan_t * hcan, uint16_t rx_id, dji_moto
if (dji_motor_count < DJI_MOTOR_MAX)
{
dji_motor_list[dji_motor_count++] = motor;
can_rx_register(hcan, rx_id, dji_motor_rx_callback);
if (hcan == &hcan1)
can_rx_register(hcan, rx_id, dji_motor_can1_rx_callback);
else
can_rx_register(hcan, rx_id, dji_motor_can2_rx_callback);
}
}
static void dji_motor_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc)
static void dji_motor_can1_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc)
{
(void)dlc;
for (uint8_t i = 0; i < dji_motor_count; i++)
{
if (dji_motor_list[i]->rx_id == std_id)
if (dji_motor_list[i]->hcan == &hcan1 && dji_motor_list[i]->rx_id == std_id)
{
dji_motor_parse(dji_motor_list[i], rx_data);
return;
}
}
}
static void dji_motor_can2_rx_callback(uint32_t std_id, const uint8_t rx_data[8], uint32_t dlc)
{
(void)dlc;
for (uint8_t i = 0; i < dji_motor_count; i++)
{
if (dji_motor_list[i]->hcan == &hcan2 && dji_motor_list[i]->rx_id == std_id)
{
dji_motor_parse(dji_motor_list[i], rx_data);
return;
@@ -119,8 +135,14 @@ void dji_motor_send_current_high(hcan_t * hcan, int16_t i5, int16_t i6, int16_t
dji_motor_send_int16x4(hcan, 0x1FF, v);
}
void dji_motor_send_voltage_high(hcan_t * hcan, int16_t v5, int16_t v6, int16_t v7)
void dji_motor_send_gm6020_current_low(hcan_t * hcan, int16_t i1, int16_t i2, int16_t i3, int16_t i4)
{
const int16_t v[4] = {v5, v6, v7, 0};
dji_motor_send_int16x4(hcan, 0x2FF, v);
const int16_t v[4] = {i1, i2, i3, i4};
dji_motor_send_int16x4(hcan, 0x1FE, v);
}
void dji_motor_send_gm6020_current_high(hcan_t * hcan, int16_t i5, int16_t i6, int16_t i7, int16_t i8)
{
const int16_t v[4] = {i5, i6, i7, i8};
dji_motor_send_int16x4(hcan, 0x2FE, v);
}
底盘/modules/motor/dji_motor.h
+7 -6
View File
@@ -5,13 +5,13 @@
/* DJI 电机(M3508/M2006/GM6020)统一驱动
* - 反馈:can_start() 后通过 can_rx_register 按 rx_id 注册,接收中断内解析(多圈累计)
* - 控制:组装 0x200/0x1FF/0x2FF 控制帧,经 CAN_SendTxMessage 发送 */
* - 控制:组装 0x200/0x1FF/0x1FE/0x2FE 控制帧,经 CAN_SendTxMessage 发送 */
typedef enum
{
DJI_MOTOR_3508, // 减速比 3591:187(≈19:1), 转矩常数 0.3N·m/A
DJI_MOTOR_2006, // 减速比 36:1, 转矩常数 0.18N·m/A
DJI_MOTOR_6020, // 直驱, 电压控制
DJI_MOTOR_6020, // 直驱, 电流控制(ID1~4 为 0x1FE 帧, ±16384 对应 ±3A)
} dji_motor_type_e;
typedef struct
@@ -20,7 +20,7 @@ typedef struct
int64_t total_tick; // 累计角度位置原始数据(8192*圈数+raw,无 ±1 圈限制)
float rotor_angle_deg; // 累计转子机械角(°)
int16_t rotor_speed; // 转子转速(RPM)
int16_t raw_torque; // 转矩电流/转矩电压原始数据
int16_t raw_torque; // 转矩电流原始数据
float torque_current; // 转矩电流(A)
uint8_t temperature; // 电机温度(℃)
uint32_t last_online_tick; // 最近一次收到反馈的 tick(HAL_GetTick)
@@ -39,11 +39,12 @@ extern void dji_motor_init(dji_motor_t * motor, hcan_t * hcan, uint16_t rx_id, d
/* ---- 控制帧发送 ----
* M3508/M2006 ID1~4:0x200 电流帧(±16384 对应 ±20A/±10A)
* M3508/M2006 ID5~8:0x1FF 电流帧;GM6020 ID1~4:0x1FF 电压帧(±25000)
* GM6020 ID5~7:0x2FF 电压帧 */
* M3508/M2006 ID5~8:0x1FF 电流帧(±16384)
* GM6020 电流控制:ID1~4 为 0x1FE 电流帧(±16384 对应 ±3A),ID5~8 为 0x2FE 电流帧(±16384) */
extern void dji_motor_send_current_low(hcan_t * hcan, int16_t i1, int16_t i2, int16_t i3, int16_t i4);
extern void dji_motor_send_current_high(hcan_t * hcan, int16_t i5, int16_t i6, int16_t i7, int16_t i8);
extern void dji_motor_send_voltage_high(hcan_t * hcan, int16_t v5, int16_t v6, int16_t v7);
extern void dji_motor_send_gm6020_current_low(hcan_t * hcan, int16_t i1, int16_t i2, int16_t i3, int16_t i4);
extern void dji_motor_send_gm6020_current_high(hcan_t * hcan, int16_t i5, int16_t i6, int16_t i7, int16_t i8);
/* 通用 int16x4 发送(板间通讯等复用) */
extern void dji_motor_send_int16x4(hcan_t * hcan, uint32_t std_id, const int16_t val[4]);