fly316/PX4-Autopilot
7
0
Fork 0
mirror of https://gitee.com/mirrors_PX4/PX4-Autopilot.git synced 2026-10-18 02:23:35 +08:00
Code Issues Packages Projects Releases Wiki Activity

Cleaned up PI wrapping code, still subject to testing

Browse Source
This commit is contained in:
Lorenz Meier
2012-11-20 15:19:51 +01:00
parent 129e6d73de
commit 6ff4520904
10 changed files with 121 additions and 174 deletions
Download Patch File Download Diff File Expand all files Collapse all files
apps/fixedwing_pos_control/fixedwing_pos_control.h
-19
View File
@@ -42,26 +42,7 @@
#ifndef FIXEDWING_POS_CONTROL_H_
#define FIXEDWING_POS_CONTROL_H_
#include <uORB/uORB.h>
#include <uORB/topics/vehicle_attitude.h>
#include <uORB/topics/vehicle_attitude_setpoint.h>
#include <uORB/topics/vehicle_rates_setpoint.h>
#include <uORB/topics/actuator_controls.h>
#endif
struct planned_path_segments_s {
bool segment_type;
double start_lat; // Start of line or center of arc
double start_lon;
double end_lat;
double end_lon;
float radius; // Radius of arc
float arc_start_bearing; // Bearing from center to start of arc
float arc_sweep; // Angle (radians) swept out by arc around center.
// Positive for clockwise, negative for counter-clockwise
};
float _wrap180(float bearing);
apps/fixedwing_pos_control/fixedwing_pos_control_main.c
+24 -72
View File
@@ -91,6 +91,19 @@ struct fw_pos_control_param_handles {
};
struct planned_path_segments_s {
bool segment_type;
double start_lat; // Start of line or center of arc
double start_lon;
double end_lat;
double end_lon;
float radius; // Radius of arc
float arc_start_bearing; // Bearing from center to start of arc
float arc_sweep; // Angle (radians) swept out by arc around center.
// Positive for clockwise, negative for counter-clockwise
};
/* Prototypes */
/* Internal Prototypes */
static int parameters_init(struct fw_pos_control_param_handles *h);
@@ -177,9 +190,9 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[])
memset(&attitude_setpoint, 0, sizeof(attitude_setpoint));
/* publish attitude setpoint */
attitude_setpoint.roll_tait_bryan = 0.0f;
attitude_setpoint.pitch_tait_bryan = 0.0f;
attitude_setpoint.yaw_tait_bryan = 0.0f;
attitude_setpoint.roll_body = 0.0f;
attitude_setpoint.pitch_body = 0.0f;
attitude_setpoint.yaw_body = 0.0f;
orb_advert_t attitude_setpoint_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint), &attitude_setpoint);
/* subscribe */
@@ -243,7 +256,7 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[])
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,
(double)global_setpoint.lat / (double)1e7d, (double)global_setpoint.lon / (double)1e7d);
printf("psi_track: %0.4f\n", psi_track);
printf("psi_track: %0.4f\n", (double)psi_track);
}
/* Control */
@@ -265,21 +278,21 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[])
float delta_psi_c = -p.xtrack_p * xtrack_err.distance; //(-) because z axis points downwards
if(delta_psi_c > 60.0f*M_DEG_TO_RAD)
delta_psi_c = 60.0f*M_DEG_TO_RAD;
if(delta_psi_c > 60.0f*M_DEG_TO_RAD_F)
delta_psi_c = 60.0f*M_DEG_TO_RAD_F;
if(delta_psi_c < -60.0f*M_DEG_TO_RAD)
delta_psi_c = -60.0f*M_DEG_TO_RAD;
if(delta_psi_c < -60.0f*M_DEG_TO_RAD_F)
delta_psi_c = -60.0f*M_DEG_TO_RAD_F;
float psi_c = psi_track + delta_psi_c;
float psi_e = psi_c - att.yaw;
/* shift error to prevent wrapping issues */
psi_e = _wrapPI(psi_e);
psi_e = _wrap_pi(psi_e);
/* calculate roll setpoint, do this artificially around zero */
attitude_setpoint.roll_tait_bryan = pid_calculate(&heading_controller, psi_e, 0.0f, 0.0f, 0.0f);
attitude_setpoint.roll_body = pid_calculate(&heading_controller, psi_e, 0.0f, 0.0f, 0.0f);
// if (counter % 100 == 0)
// printf("xtrack_err.distance: %0.4f, delta_psi_c: %0.4f\n",xtrack_err.distance, delta_psi_c);
@@ -296,7 +309,7 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[])
{
//TODO: take care of relative vs. ab. altitude
attitude_setpoint.pitch_tait_bryan = pid_calculate(&altitude_controller, global_setpoint.altitude, global_pos.alt, 0.0f, 0.0f);
attitude_setpoint.pitch_body = pid_calculate(&altitude_controller, global_setpoint.altitude, global_pos.alt, 0.0f, 0.0f);
}
/*Publish the attitude setpoint */
@@ -378,64 +391,3 @@ int fixedwing_pos_control_main(int argc, char *argv[])
usage("unrecognized command");
exit(1);
}
float _wrapPI(float bearing)
{
while (bearing > M_PI_F) {
bearing = bearing - M_TWOPI_F;
}
while (bearing <= -M_PI_F) {
bearing = bearing + M_TWOPI_F;
}
return bearing;
}
float _wrap2PI(float bearing)
{
while (bearing >= M_TWOPI_F) {
bearing = bearing - M_TWOPI_F;
}
while (bearing < 0.0f) {
bearing = bearing + M_TWOPI_F;
}
return bearing;
}
float _wrap180(float bearing)
{
while (bearing > 180.0f) {
bearing = bearing - 360.0f;
}
while (bearing <= -180.0f) {
bearing = bearing + 360.0f;
}
return bearing;
}
float _wrap360(float bearing)
{
while (bearing >= 360.0f) {
bearing = bearing - 360.0f;
}
while (bearing < 0.0f) {
bearing = bearing + 360.0f;
}
return bearing;
}