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https://github.com/PX4/PX4-Autopilot.git
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Merge branch 'respect_takeoff_alt'
This commit is contained in:
@@ -46,6 +46,7 @@
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#include <systemlib/param/param.h>
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PARAM_DEFINE_FLOAT(NAV_TAKEOFF_ALT, 5.0f);
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PARAM_DEFINE_FLOAT(NAV_TAKEOFF_GAP, 3.0f);
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PARAM_DEFINE_FLOAT(TRIM_ROLL, 0.0f);
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PARAM_DEFINE_FLOAT(TRIM_PITCH, 0.0f);
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PARAM_DEFINE_FLOAT(TRIM_YAW, 0.0f);
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@@ -227,7 +227,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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hrt_abstime t_prev = 0;
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const float alt_ctl_dz = 0.2f;
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const float pos_ctl_dz = 0.05f;
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const float takeoff_alt_default = 10.0f;
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float ref_alt = 0.0f;
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hrt_abstime ref_alt_t = 0;
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uint64_t local_ref_timestamp = 0;
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@@ -244,6 +244,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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parameters_init(¶ms_h);
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parameters_update(¶ms_h, ¶ms);
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for (int i = 0; i < 2; i++) {
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pid_init(&(xy_pos_pids[i]), params.xy_p, 0.0f, params.xy_d, 1.0f, 0.0f, PID_MODE_DERIVATIV_SET, 0.02f);
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pid_init(&(xy_vel_pids[i]), params.xy_vel_p, params.xy_vel_i, params.xy_vel_d, 1.0f, params.tilt_max, PID_MODE_DERIVATIV_CALC_NO_SP, 0.02f);
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@@ -350,7 +351,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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if (reset_sp_z) {
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reset_sp_z = false;
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local_pos_sp.z = local_pos.z;
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mavlink_log_info(mavlink_fd, "[mpc] reset alt sp: %.2f", (double)-local_pos_sp.z);
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mavlink_log_info(mavlink_fd, "[mpc] reset alt sp: %.2f", (double) - local_pos_sp.z);
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}
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/* move altitude setpoint with throttle stick */
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@@ -423,12 +424,12 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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if (reset_auto_pos) {
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local_pos_sp.x = local_pos.x;
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local_pos_sp.y = local_pos.y;
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local_pos_sp.z = -takeoff_alt_default;
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local_pos_sp.z = - params.takeoff_alt - params.takeoff_gap;
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local_pos_sp.yaw = att.yaw;
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local_pos_sp_valid = true;
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att_sp.yaw_body = att.yaw;
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reset_auto_pos = false;
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mavlink_log_info(mavlink_fd, "[mpc] takeoff sp: %.2f %.2f %.2f", (double)local_pos_sp.x, (double)local_pos_sp.y, (double)-local_pos_sp.z);
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mavlink_log_info(mavlink_fd, "[mpc] takeoff sp: %.2f %.2f %.2f", (double)local_pos_sp.x, (double)local_pos_sp.y, (double) - local_pos_sp.z);
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}
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} else if (control_mode.auto_state == NAVIGATION_STATE_AUTO_RTL) {
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@@ -504,7 +505,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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/* set altitude setpoint to 5m under ground,
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* don't set it too deep to avoid unexpected landing in case of false "landed" signal */
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local_pos_sp.z = 5.0f;
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mavlink_log_info(mavlink_fd, "[mpc] landed, set alt: %.2f", (double)-local_pos_sp.z);
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mavlink_log_info(mavlink_fd, "[mpc] landed, set alt: %.2f", (double) - local_pos_sp.z);
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}
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reset_sp_z = true;
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@@ -514,7 +515,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
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if (reset_sp_z) {
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reset_sp_z = false;
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local_pos_sp.z = local_pos.z;
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mavlink_log_info(mavlink_fd, "[mpc] set loiter alt: %.2f", (double)-local_pos_sp.z);
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mavlink_log_info(mavlink_fd, "[mpc] set loiter alt: %.2f", (double) - local_pos_sp.z);
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}
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}
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@@ -59,6 +59,8 @@ PARAM_DEFINE_FLOAT(MPC_TILT_MAX, 0.5f);
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int parameters_init(struct multirotor_position_control_param_handles *h)
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{
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h->takeoff_alt = param_find("NAV_TAKEOFF_ALT");
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h->takeoff_gap = param_find("NAV_TAKEOFF_GAP");
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h->thr_min = param_find("MPC_THR_MIN");
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h->thr_max = param_find("MPC_THR_MAX");
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h->z_p = param_find("MPC_Z_P");
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@@ -84,6 +86,8 @@ int parameters_init(struct multirotor_position_control_param_handles *h)
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int parameters_update(const struct multirotor_position_control_param_handles *h, struct multirotor_position_control_params *p)
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{
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param_get(h->takeoff_alt, &(p->takeoff_alt));
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param_get(h->takeoff_gap, &(p->takeoff_gap));
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param_get(h->thr_min, &(p->thr_min));
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param_get(h->thr_max, &(p->thr_max));
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param_get(h->z_p, &(p->z_p));
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@@ -41,6 +41,8 @@
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#include <systemlib/param/param.h>
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struct multirotor_position_control_params {
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float takeoff_alt;
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float takeoff_gap;
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float thr_min;
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float thr_max;
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float z_p;
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@@ -63,6 +65,8 @@ struct multirotor_position_control_params {
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};
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struct multirotor_position_control_param_handles {
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param_t takeoff_alt;
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param_t takeoff_gap;
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param_t thr_min;
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param_t thr_max;
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param_t z_p;
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