forked from Archive/PX4-Autopilot
minor code cleanup, not changing functionality
This commit is contained in:
parent
9fa628c668
commit
00b79764d7
|
@ -597,7 +597,7 @@ uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_
|
||||||
publish_armed_status(current_status);
|
publish_armed_status(current_status);
|
||||||
printf("[commander] Enabling HIL, locking down all actuators for safety.\n\t(Arming the system will not activate them while in HIL mode)\n");
|
printf("[commander] Enabling HIL, locking down all actuators for safety.\n\t(Arming the system will not activate them while in HIL mode)\n");
|
||||||
} else if (current_status->state_machine != SYSTEM_STATE_STANDBY) {
|
} else if (current_status->state_machine != SYSTEM_STATE_STANDBY) {
|
||||||
mavlink_log_critical(mavlink_fd, "[commander] REJECTING switch to HIL, not in standby.")
|
mavlink_log_critical(mavlink_fd, "[commander] REJECTING HIL, not in standby.")
|
||||||
}
|
}
|
||||||
|
|
||||||
/* NEVER actually switch off HIL without reboot */
|
/* NEVER actually switch off HIL without reboot */
|
||||||
|
|
|
@ -297,19 +297,12 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[])
|
||||||
|
|
||||||
if (global_sp_updated) {
|
if (global_sp_updated) {
|
||||||
orb_copy(ORB_ID(vehicle_global_position_setpoint), global_setpoint_sub, &global_setpoint);
|
orb_copy(ORB_ID(vehicle_global_position_setpoint), global_setpoint_sub, &global_setpoint);
|
||||||
// printf("xtrack_err.distance %.4f ", (double)xtrack_err.distance);
|
|
||||||
|
|
||||||
float delta_psi_c = pid_calculate(&offtrack_controller, 0, xtrack_err.distance, 0.0f, 0.0f); //p.xtrack_p * xtrack_err.distance
|
|
||||||
|
|
||||||
// printf("delta_psi_c %.4f ", (double)delta_psi_c);
|
|
||||||
|
|
||||||
start_pos = global_pos; //for now using the current position as the startpoint (= approx. last waypoint because the setpoint switch occurs at the waypoint)
|
start_pos = global_pos; //for now using the current position as the startpoint (= approx. last waypoint because the setpoint switch occurs at the waypoint)
|
||||||
global_sp_updated_set_once = true;
|
global_sp_updated_set_once = true;
|
||||||
psi_track = get_bearing_to_next_waypoint((double)global_pos.lat / (double)1e7d, (double)global_pos.lon / (double)1e7d,
|
psi_track = get_bearing_to_next_waypoint((double)global_pos.lat / (double)1e7d, (double)global_pos.lon / (double)1e7d,
|
||||||
(double)global_setpoint.lat / (double)1e7d, (double)global_setpoint.lon / (double)1e7d);
|
(double)global_setpoint.lat / (double)1e7d, (double)global_setpoint.lon / (double)1e7d);
|
||||||
|
|
||||||
if (verbose)
|
printf("next wp direction: %0.4f\n", (double)psi_track);
|
||||||
printf("psi_track: %0.4f\n", (double)psi_track);
|
|
||||||
}
|
}
|
||||||
|
|
||||||
/* Simple Horizontal Control */
|
/* Simple Horizontal Control */
|
||||||
|
@ -332,6 +325,9 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[])
|
||||||
float psi_c = psi_track + delta_psi_c;
|
float psi_c = psi_track + delta_psi_c;
|
||||||
float psi_e = psi_c - att.yaw;
|
float psi_e = psi_c - att.yaw;
|
||||||
|
|
||||||
|
/* wrap difference back onto -pi..pi range */
|
||||||
|
psi_e = _wrap_pi(psi_e);
|
||||||
|
|
||||||
if (verbose) {
|
if (verbose) {
|
||||||
printf("xtrack_err.distance %.4f ", (double)xtrack_err.distance);
|
printf("xtrack_err.distance %.4f ", (double)xtrack_err.distance);
|
||||||
printf("delta_psi_c %.4f ", (double)delta_psi_c);
|
printf("delta_psi_c %.4f ", (double)delta_psi_c);
|
||||||
|
@ -340,9 +336,6 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[])
|
||||||
printf("psi_e %.4f ", (double)psi_e);
|
printf("psi_e %.4f ", (double)psi_e);
|
||||||
}
|
}
|
||||||
|
|
||||||
/* shift error to prevent wrapping issues */
|
|
||||||
psi_e = _wrap_pi(psi_e);
|
|
||||||
|
|
||||||
/* calculate roll setpoint, do this artificially around zero */
|
/* calculate roll setpoint, do this artificially around zero */
|
||||||
float delta_psi_rate_c = pid_calculate(&heading_controller, psi_e, 0.0f, 0.0f, 0.0f);
|
float delta_psi_rate_c = pid_calculate(&heading_controller, psi_e, 0.0f, 0.0f, 0.0f);
|
||||||
float psi_rate_track = 0; //=V_gr/r_track , this will be needed for implementation of arc following
|
float psi_rate_track = 0; //=V_gr/r_track , this will be needed for implementation of arc following
|
||||||
|
|
Loading…
Reference in New Issue