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- #include "Sub.h"
- #define PI 3.141592653589793238462643383279502884
- // stabilize_init - initialise stabilize controller
- bool Sub::stabilize_init()
- {
- // set target altitude to zero for reporting
- pos_control.relax_alt_hold_controllers();//目标高度为当前高度,目标速度和上次速度 当前速度
-
- last_roll_s = 0;
- last_pitch_s = 0;
- updowmgain =0.5;
- delaygain = 401;
- continuous_count=0;
- continuous_countdec=0;
- last_continuous = 0;
- last_yaw_s = ahrs.yaw_sensor;
- //last_input_ms = AP_HAL::millis();
- last_input_ms_stable = AP_HAL::millis();
- pitch_input_inc=0;
-
- prepare_state = Horizontal;
- return true;
- }
- // stabilize_run - runs the main stabilize controller
- // should be called at 100hz or more
- extern mavlink_rov_state_monitoring_t rov_message;
- void Sub::handle_attitude_stablize(){
-
- uint32_t tnow = AP_HAL::millis();
- motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
- // get pilot desired lean angles
- float target_roll, target_pitch, target_yaw;
- // Check if set_attitude_target_no_gps is valid
- if (tnow - sub.set_attitude_target_no_gps.last_message_ms < 5000) {
- Quaternion(
- set_attitude_target_no_gps.packet.q
- ).to_euler(
- target_roll,
- target_pitch,
- target_yaw
- );
- target_roll = 100 * degrees(target_roll);
- target_pitch = 100 * degrees(target_pitch);
- target_yaw = 100 * degrees(target_yaw);
- last_roll_s = target_roll;
- last_pitch_s = target_pitch;
- last_yaw_s = target_yaw;
-
- attitude_control.input_euler_angle_roll_pitch_yaw(target_roll, target_pitch, target_yaw, true);
- } else {
-
- int32_t pitch_input = 0;
-
- if (prepare_state == Horizontal)
- {
- pitch_input = 0;
- target_roll = 0;
- last_roll_s = 0;
- target_yaw = get_pilot_desired_yaw_rate(channel_yaw->get_control_in()*1.0);
-
- }else if(prepare_state == Vertical)
- {
- pitch_input = 8000;
- //target_roll = ((float)channel_yaw->get_control_in()*0.4);
- target_roll = 0;
- target_yaw = ((float)channel_yaw->get_control_in()*0.4);
- }
- else{
- pitch_input = 0;
- }
- pitch_input_inc = constrain_int32(pitch_input,-9000,9000);
- //-------------------------------------
-
- if (abs(target_roll) > 300 ){
- attitude_control.input_rate_bf_roll_pitch_yaw(target_roll, 0, 0);
- last_yaw_s = ahrs.yaw_sensor;
- last_roll_s = ahrs.roll_sensor;
- last_input_ms_stable = tnow;
-
- }else if (abs(target_yaw) > 300) {
- // if only yaw is being controlled, don't update pitch and roll
- attitude_control.input_rate_bf_roll_pitch_yaw(0, 0, target_yaw);
- last_yaw_s = ahrs.yaw_sensor;
-
- last_input_ms_stable = tnow;
- } else if (tnow < last_input_ms_stable + 250) {
- // just brake for a few mooments so we don't bounce
- last_yaw_s = ahrs.yaw_sensor;
-
- attitude_control.input_rate_bf_roll_pitch_yaw(0, 0, 0);
- } else {
- // Lock attitude
- attitude_control.input_euler_angle_roll_pitch_yaw(last_roll_s, (float)pitch_input_inc, last_yaw_s, true);
-
- }//--------------------------------------------------------------------------------------------------------------
- static int f = 0;
- f++;
- if(f>800)
- {
-
- //gcs().send_text(MAV_SEVERITY_INFO, " stableinput %f %f,%f ",(float)last_roll_s,(float)pitch_input_inc,(float)last_yaw_s);
- f=0;
- }
-
- }
- }
- void Sub::stabilize_run()
- {
- // if not armed set throttle to zero and exit immediately
- if (!motors.armed()) {
- motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::GROUND_IDLE);
- attitude_control.set_throttle_out(0,true,g.throttle_filt);
- attitude_control.relax_attitude_controllers();
- pos_control.relax_alt_hold_controllers();//目标高度为当前高度,目标速度和上次速度 当前速度
- last_roll_s = 0;
- last_pitch_s = 0;
- updowmgain =0.5;
- delaygain = 401;
-
- continuous_count=0;
- continuous_countdec=0;
- last_continuous = 0;
- last_yaw_s = ahrs.yaw_sensor;
- PressLevel_f =5.0;//压力分级复位
- PressLevel = no;
- //yaw_press = (int16_t)(ahrs.yaw_sensor/100);//记住方位
- pitch_input_inc=0;
- prepare_state = Horizontal;
- return;
- }
- motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
- handle_attitude_stablize();
- if(stable_alt_control){
- altcontrol();
- }
- else{
- //防止交叉
- float _forward = channel_forward->norm_input();
- float _lateral =channel_lateral->norm_input();
- if (fabsf(_forward)>=fabsf(_lateral))
- {
- _lateral = 0.0;
- }else{
- _forward = 0.0;
- }
- motors.set_forward(constrain_float(getgainfstatble(_forward),-1.0,1.0));
- motors.set_lateral(constrain_float(getgainfstatble(_lateral),-1.0,1.0));
-
- attitude_control.set_throttle_out(gaindelay(1.0-(float)PressLevel_f*0.1), false, g.throttle_filt);//压力分级
- static uint16_t count = 0;
- count++;
- if (count>400)
- {
- count = 0;
- gcs().send_text(MAV_SEVERITY_INFO, "set_throttle_out %f %f \n",gaindelay(1.0-(float)PressLevel_f*0.1),motors.get_throttle());
-
- }
-
- rov_message.pressure_level = int(PressLevel);
- }
- }
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