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2026-03-31 23:30:33 +08:00
commit 760043c8e7
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App/nav/corridor_ctrl.c Normal file
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#include "corridor_ctrl.h"
#include <math.h>
#include <stdbool.h>
/* ====================== 内部状态 ====================== */
static CorridorCtrlConfig_t s_cfg;
static bool s_initialized = false;
/* 辅助:浮点数限幅 */
static inline float clampf(float val, float lo, float hi)
{
if (val < lo) return lo;
if (val > hi) return hi;
return val;
}
void CorridorCtrl_Init(const CorridorCtrlConfig_t *config)
{
s_cfg = *config;
s_initialized = true;
}
void CorridorCtrl_Compute(const CorridorState_t *state,
const CorridorObs_t *obs,
float imu_wz,
RawCmd_t *out_cmd)
{
if (!s_initialized) {
out_cmd->v = 0.0f;
out_cmd->w = 0.0f;
out_cmd->flags = 0U;
return;
}
/* ========================================================
* 核心控制律:
* w_cmd = kp_theta * e_th + kd_theta * (-imu_wz) + kp_y * e_y
*
* - kp_theta * e_th : 比例项,车头偏了就回转
* - kd_theta * (-imu_wz) : 微分阻尼,等价于"阻止车头继续转"
* 用 IMU 直接读数做微分项,比差分 e_th 更丝滑无噪声
* - kp_y * e_y : 横向纠偏,车身偏了就产生角速度拉回来
* ======================================================== */
float w_cmd = s_cfg.kp_theta * state->e_th
+ s_cfg.kd_theta * (-imu_wz)
+ s_cfg.kp_y * state->e_y;
/* 角速度限幅:防止 PD 溢出导致原地打转 */
w_cmd = clampf(w_cmd, -s_cfg.w_max, s_cfg.w_max);
/* ========================================================
* 线速度策略:
* 基础巡航速度 v_cruise
* 当角速度偏大时适当降速(弯道减速),保持运动学协调
* 公式: v = v_cruise * (1 - k * |w/w_max|)
* k 取 0.3~0.5 较保守
* ======================================================== */
float speed_reduction = s_cfg.speed_reduction_k * fabsf(w_cmd) / s_cfg.w_max;
float v_cmd = s_cfg.v_cruise * (1.0f - speed_reduction);
/* 线速度限幅:不允许倒车,不允许超速 */
v_cmd = clampf(v_cmd, 0.0f, s_cfg.v_max);
/* ========================================================
* 置信度降级保护:
* 当滤波器健康度 conf 过低(两边雷达全瞎),
* 说明走廊参照完全丢失,降低线速度防止盲飞
* ======================================================== */
if (state->conf < 0.3f) {
/* 健康度极低:速度打三折,保持航向惯性滑行 */
v_cmd *= 0.3f;
} else if (state->conf < 0.6f) {
/* 健康度较低(单侧退化):速度打七折 */
v_cmd *= 0.7f;
}
/* 输出赋值 */
out_cmd->t_ms = state->t_ms;
out_cmd->v = v_cmd;
out_cmd->w = w_cmd;
out_cmd->flags = 0U;
}