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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-15 20:23:34 +08:00
added pos message and corrected rot vec errror
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@@ -576,8 +576,19 @@ FixedwingPositionINDIControl::Run()
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// Publish actuator controls only once in OFFBOARD
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if (_vehicle_status.nav_state == vehicle_status_s::NAVIGATION_STATE_OFFBOARD) {
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// ========================================
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// publish controller position in ENU frame
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// ========================================
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_soaring_controller_position.timestamp = hrt_absolute_time();
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for (int i=0; i<3; i++){
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_soaring_controller_position.pos[i] = _pos(i);
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_soaring_controller_position.vel[i] = _vel(i);
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_soaring_controller_position.acc[i] = _acc(i);
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}
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_soaring_controller_position_pub.publish(_soaring_controller_position);
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// ====================================
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// publish high level control variables
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// publish controller position setpoint
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// ====================================
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_soaring_controller_position_setpoint.timestamp = hrt_absolute_time();
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for (int i=0; i<3; i++){
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@@ -636,7 +647,7 @@ FixedwingPositionINDIControl::Run()
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if (_counter==100) {
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_counter = 0;
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PX4_INFO("frequency: \t%.3f", (double)(1000000*100)/(hrt_absolute_time()-_last_time));
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//PX4_INFO("frequency: \t%.3f", (double)(1000000*100)/(hrt_absolute_time()-_last_time));
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_last_time = hrt_absolute_time();
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}
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else {
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@@ -997,7 +1008,19 @@ FixedwingPositionINDIControl::_compute_NDI_stage_1(Vector3f pos_ref, Vector3f ve
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Dcmf R_ref_true(R_ref.transpose()*R_ib);
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// get required rotation vector (in body frame)
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AxisAnglef q_err(R_ref_true);
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Vector3f w_err = -q_err.angle()*q_err.axis();
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Vector3f w_err;
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if (abs(q_err.angle())<M_PI_F){
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w_err = -q_err.angle()*q_err.axis();
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}
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else{
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if (q_err.angle()>0.f){
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w_err = (2*M_PI_F-q_err.angle())*q_err.axis();
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}
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else{
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w_err = (-2*M_PI_F-q_err.angle())*q_err.axis();
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}
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}
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// =========================================
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// apply PD control law on the body attitude
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@@ -1024,6 +1047,9 @@ FixedwingPositionINDIControl::_compute_NDI_stage_1(Vector3f pos_ref, Vector3f ve
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//PX4_INFO("force command: \t%.2f\t%.2f\t%.2f", (double)f_command(0), (double)f_command(1), (double)f_command(2));
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//PX4_INFO("FRD body frame rotation vec: \t%.2f\t%.2f\t%.2f", (double)w_err(0), (double)w_err(1), (double)w_err(2));
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if (sqrtf(w_err(0)*w_err(0) + w_err(1)*w_err(1) + w_err(2)*w_err(2))>M_PI_F){
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PX4_ERR("rotation angle larger than pi: \t%.2f", (double)sqrtf(w_err(0)*w_err(0) + w_err(1)*w_err(1) + w_err(2)*w_err(2)));
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}
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return rot_acc_command;
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}
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