forked from Archive/PX4-Autopilot
correctly hooked up setpoints in fixed wing control app, pending validation
This commit is contained in:
parent
ddb5ba221d
commit
246f8fd3bd
|
@ -133,8 +133,8 @@ typedef struct {
|
|||
|
||||
/* Next waypoint*/
|
||||
|
||||
float wp_x;
|
||||
float wp_y;
|
||||
double wp_x;
|
||||
double wp_y;
|
||||
float wp_z;
|
||||
|
||||
/* Setpoints */
|
||||
|
@ -349,9 +349,6 @@ static void get_parameters(plane_data_t * pdata)
|
|||
param_get(att_awu, &(pdata->intmax_att));
|
||||
param_get(pos_awu, &(pdata->intmax_pos));
|
||||
pdata->airspeed = 10;
|
||||
pdata->wp_x = 48;
|
||||
pdata->wp_y = 8;
|
||||
pdata->wp_z = 100;
|
||||
pdata->mode = 1;
|
||||
}
|
||||
|
||||
|
@ -686,7 +683,6 @@ int fixedwing_control_main(int argc, char *argv[])
|
|||
|
||||
/* output structs */
|
||||
struct actuator_controls_s actuators;
|
||||
struct actuator_armed_s armed;
|
||||
struct vehicle_attitude_setpoint_s att_sp;
|
||||
memset(&att_sp, 0, sizeof(att_sp));
|
||||
|
||||
|
@ -694,8 +690,6 @@ int fixedwing_control_main(int argc, char *argv[])
|
|||
for (unsigned i = 0; i < NUM_ACTUATOR_CONTROLS; i++)
|
||||
actuators.control[i] = 0.0f;
|
||||
orb_advert_t actuator_pub = orb_advertise(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, &actuators);
|
||||
armed.armed = false;
|
||||
orb_advert_t armed_pub = orb_advertise(ORB_ID(actuator_armed), &armed);
|
||||
orb_advert_t att_sp_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint), &att_sp);
|
||||
|
||||
/* Subscribe to global position, attitude and rc */
|
||||
|
@ -771,6 +765,10 @@ int fixedwing_control_main(int argc, char *argv[])
|
|||
plane_data.pitchspeed = att.pitchspeed;
|
||||
plane_data.yawspeed = att.yawspeed;
|
||||
|
||||
plane_data.wp_x = global_setpoint.lat / (double)1e7;
|
||||
plane_data.wp_y = global_setpoint.lon / (double)1e7;
|
||||
plane_data.wp_z = global_setpoint.altitude;
|
||||
|
||||
/* parameter values */
|
||||
if (loopcounter % 20 == 0) {
|
||||
get_parameters(&plane_data);
|
||||
|
@ -841,10 +839,6 @@ int fixedwing_control_main(int argc, char *argv[])
|
|||
orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp);
|
||||
|
||||
/* publish actuator setpoints (for mixer) */
|
||||
|
||||
/* arming state depends on commander arming state */
|
||||
armed.armed = state.flag_system_armed;
|
||||
orb_publish(ORB_ID(actuator_armed), armed_pub, &armed);
|
||||
orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators);
|
||||
|
||||
loopcounter++;
|
||||
|
|
Loading…
Reference in New Issue