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- #include "Sub.h"
- //#include "/AP_Math/AP_Math.h"
- #define PI 3.141592653589793238462643383279502884
- extern mavlink_rov_state_monitoring_t rov_message;
- Quaternion attitude_desired_quat_;
- //Matrix3f last_desired;
- /*
- * control_althold.pde - init and run calls for althold, flight mode
- */
- // althold_init - initialise althold controller
- bool Sub::sport_init()
- {
- attitude_control.set_throttle_out(0.5 ,true, g.throttle_filt);
- //holding_depth = false;
- //检查是否有深度计存在
- if(!control_check_barometer()) {
- return false;
- }
- // initialize vertical speeds and leash lengths
- // sets the maximum speed up and down returned by position controller
- //get_pilot_speed_dn QGC PILOT 设置的值
- pos_control.set_max_speed_z(-get_pilot_speed_dn(), g.pilot_speed_up);//(-500,500)设置最大最小速度 和刹车长度
- pos_control.set_max_accel_z(g.pilot_accel_z);//设置最大加速度值 和刹车长度
- 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
- pos_control.reset_I();
- //pos_control.set_target_to_stopping_point_z();//刹车长度 根据当前速度估计目标深度
- pos_control.calc_leash_length_z();//刹车长度 12.19
- pos_control.set_alt_target(barometer.get_altitude()*100);//当前深度12.19
- holding_depth = true;
- //ahrs.get_quat_body_to_ned(attitude_desired_quat_);//12.19 使用roll pitch =0的姿态
-
- attitude_desired_quat_.from_euler(0.0, 0.0,ahrs.yaw);//初始化
- rotpitch.identity();
- attitude_desired_quat_.rotation_matrix(rotyaw);
-
- last_roll = 0;
- last_pitch = 0;
-
- updowmgain =0.5;
- delaygain = 401;
-
- continuous_count=0;
- continuous_countdec=0;
- last_continuous = 0;
- last_yaw = ahrs.yaw_sensor;
- last_input_ms = AP_HAL::millis();
- last_input_ms_stable = AP_HAL::millis();
- //updown_gain = 0.0;
-
-
- return true;
- }
- void Sub::handle_attitude_sport(){
- uint32_t tnow = AP_HAL::millis();
- // 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 = target_roll;
- last_pitch = target_pitch;
- last_yaw = target_yaw;
-
- attitude_control.input_euler_angle_roll_pitch_yaw(target_roll, target_pitch, target_yaw, true);
- } else {
- float throttle = 2*(0.5-channel_throttle->norm_input());
- float yaw = channel_yaw->norm_input();
- if (fabsf(throttle)>=fabsf(yaw))
- {
- yaw = 0.0;
- }else{
- throttle = 0.0;
- yaw = channel_yaw->get_control_in()*0.35;
- }
- get_pilot_desired_lean_angles(0, (int16_t)(throttle/1.5*5700), target_roll, target_pitch, attitude_control.get_althold_lean_angle_max());
- target_yaw = get_pilot_desired_yaw_rate(yaw);//*0.6 变慢
-
- if ( abs(target_pitch) > 300) {
-
- last_input_ms = tnow;
- attitude_control.input_rate_bf_roll_pitch_yaw(0, target_pitch, 0);
-
- //ahrs.get_quat_body_to_ned(attitude_desired_quat_);
-
-
- Matrix3f mat_body = ahrs.get_rotation_body_to_ned();//03.17
- float pitch_ang = get_pitch_to_ned(mat_body);
-
- rotpitch.from_euler(0,pitch_ang,0);//pitch 旋转矩阵
-
-
- } 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);
-
- Matrix3f mat_body = ahrs.get_rotation_body_to_ned();//03.17
- get_heading_to_ned(rotyaw,mat_body);//yaw旋转矩阵
-
-
-
- //ahrs.get_quat_body_to_ned(attitude_desired_quat_);
-
- last_input_ms = tnow;
- } else if (tnow < last_input_ms + 250) {
-
- // just brake for a few mooments so we don't bounce
- Matrix3f mat_body = ahrs.get_rotation_body_to_ned();//03.17
- get_heading_to_ned(rotyaw,mat_body);//yaw旋转矩阵
-
- attitude_control.input_rate_bf_roll_pitch_yaw(0, 0, 0);
- } else {
- // Lock attitude
-
- float depth = barometer.get_altitude()*100; // cm
- if(fabsf(depth)<50){//水面附近
- float maxsinpitch = constrain_float(fabsf(depth)/50.0,0.0,1.0);//40深度传感器到体长+10 余量 可以允许的最大pitch角的绝对值
- float nowsinpitch = rotpitch.a.z;//当前的pitch角
- Matrix3f rotpitch_limit;
- if (fabsf(nowsinpitch)>maxsinpitch)//说明比允许的大 姿态应该是恢复水平一些
- {
- float pitch_ang = get_pitch_to_ned(rotpitch);//目前的pith
- if (fabsf(pitch_ang)<PI/2)
- {
- pitch_ang = asinf(maxsinpitch);
- }else{
- pitch_ang = (PI- asinf(maxsinpitch))*sign_in(pitch_ang);
- }
- rotpitch_limit .from_euler(0,pitch_ang,0);//pitch 旋转矩阵
- }else{//保持原来的姿态
- rotpitch_limit = rotpitch;//pitch 旋转矩阵
- }
- attitude_desired_quat_.from_rotation_matrix(rotyaw*rotpitch_limit);
- static uint16_t count = 0;
- count++;
- if (count>400)
- {
- count = 0;
- // gcs().send_text(MAV_SEVERITY_INFO, "ahr %f %f %f \n",nowsinpitch,maxsinpitch,get_pitch_to_ned(rotpitch_limit));
- }
- }else{
- attitude_desired_quat_.from_rotation_matrix(rotyaw*rotpitch);
- }
- attitude_control.input_quaternion(attitude_desired_quat_);
- //attitude_desired_quat_.from_rotation_matrix(rotyaw*rotpitch);
- //attitude_control.input_quaternion(attitude_desired_quat_);
- }
- }
- }
- void Sub::sport_run_alt(void){
-
-
- // When unarmed, disable motors and stabilization
- if (!motors.armed()) {
-
- motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::GROUND_IDLE);
- // Sub vehicles do not stabilize roll/pitch/yaw when not auto-armed (i.e. on the ground, pilot has never raised throttle)
- attitude_control.set_throttle_out(0.5 ,true, g.throttle_filt);
- attitude_control.relax_attitude_controllers();
- pos_control.relax_alt_hold_controllers();
- pos_control.reset_I();
- pos_control.set_alt_target(barometer.get_altitude()*100);//当前深度
-
- updowmgain =0.5;
- last_roll = 0;
- last_pitch = 0;
- last_yaw = ahrs.yaw_sensor;
- holding_depth = false;
-
- rotpitch.identity();
- attitude_desired_quat_.from_euler(0.0, 0.0,ahrs.yaw);//初始化
- attitude_desired_quat_.rotation_matrix(rotyaw);
- delaygain = 401;
-
- continuous_count=0;
- continuous_countdec=0;
- last_continuous = 0;
-
- return;
- }
- motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
- handle_attitude_sport();
- //pos_control.update_z_controller();//输出了set_throttle_out
- Matrix3f mat_body = ahrs.get_rotation_body_to_ned();
- Matrix3f mat_half;
- get_heading_to_ned(mat_half,mat_body);//得到half状态
- // mat 地到half状态
- Matrix3f rc_vehicle_frame = ahrs.get_rotation_body_to_ned().transposed()*mat_half;//rc_vehicle_frame(half)到body
- //防止手柄交叉
- float forward = channel_forward->norm_input();
- float lateral =channel_lateral->norm_input();
- if (fabsf(forward)>=fabsf(lateral))
- {
- lateral = 0.0;
- }else{
- forward = 0.0;
- }
- //手柄转到机体系------------------------
- float joystick_z = 2*(gaindelay(1.0-(float)PressLevel_f*0.1)-0.5);//-1~1
-
- Vector3f rc_throttle_forward = Vector3f(getgainf(forward),0, 0);//手柄的值
- Vector3f rc_throttle_lateral = Vector3f(0, getgainf(lateral), 0);//手柄的值
- Vector3f rc_throttle = Vector3f(0, 0, joystick_z);//手柄的值
-
-
- Vector3f rc_throttle_vehicle_frame1 = rc_vehicle_frame*rc_throttle_forward;//手柄从half系到body系
- Vector3f rc_throttle_vehicle_frame2 = rc_vehicle_frame*rc_throttle_lateral;//手柄从half系到body系
- Vector3f rc_throttle_vehicle_frame3 = rc_vehicle_frame*rc_throttle;//手柄从half系到body系
-
- Vector3f rc_throttle_vehicle_frame;
- rc_throttle_vehicle_frame.x = rc_throttle_vehicle_frame1.x + rc_throttle_vehicle_frame2.x - rc_throttle_vehicle_frame3.x;
- rc_throttle_vehicle_frame.y = rc_throttle_vehicle_frame1.y + rc_throttle_vehicle_frame2.y - rc_throttle_vehicle_frame3.y;
- rc_throttle_vehicle_frame.z = -rc_throttle_vehicle_frame1.z - rc_throttle_vehicle_frame2.z + rc_throttle_vehicle_frame3.z;
- //----------------------------------------------------
- // Read the output of the z controller and rotate it so it always points up
- //深度保持控制
- float z_throttle = pos_control.update_z_controller_f();//输出了垂直变化量
- //将深度保持控制的对地系转到机体系
- Vector3f throttle_vehicle_frame = ahrs.get_rotation_body_to_ned().transposed() * Vector3f(0, 0, z_throttle);//变到机体坐标系
-
- //手柄控制和深度保持的Z轴输出的叠加
- motors.set_forward(-throttle_vehicle_frame.x +rc_throttle_vehicle_frame.x);
- motors.set_lateral(-throttle_vehicle_frame.y +rc_throttle_vehicle_frame.y);
- motors.set_throttle(throttle_vehicle_frame.z +rc_throttle_vehicle_frame.z/2+0.5);
-
- rov_message.pressure_level = int(PressLevel);
-
- Vector3f earth_frame_rc_inputs = Vector3f(0.0, 0.0, joystick_z);//仅仅与竖直有关 手柄是在half系 Z轴
-
- bottom_detectorgain();
-
- if (fabsf(earth_frame_rc_inputs.z) > 0.05f) { // Throttle input above 5%
- // reset z targets to current values
- holding_depth = false;
- pos_control.relax_alt_hold_controllers();
-
-
-
- } else { // hold z
- if (ap.at_surface) { //最大油门不能向上动
-
- pos_control.set_alt_target(surface_depth_use()*100 - 10.0f); // set target to 5cm below surface level
-
- holding_depth = true;
-
-
- } else if (ap.at_bottom||bottom_set) {//最大油门不能向下动
- //pos_control.set_alt_target(inertial_nav.get_altitude() + 20.0f); // set target to 10 cm above bottom
- pos_control.set_alt_target(barometer.get_altitude()*100 +10);//cm
- holding_depth = true;
-
-
- } else if (!holding_depth) {
-
- pos_control.calc_leash_length_z();//刹车长度 12.19
- // pos_control.set_target_to_stopping_point_z();//有对位置的付值
- pos_control.set_alt_target(barometer.get_altitude()*100);//cm 当前深度
-
- holding_depth = true;
-
- }
- }
- static bool lastdepth = holding_depth;
- if(lastdepth !=holding_depth){
- lastdepth = holding_depth;
-
-
- //gcs().send_text(MAV_SEVERITY_INFO, "get_alt %d %f %f\n",(int)holding_depth,pos_control.get_alt_target(),barometer.get_altitude()*100);
-
- }
- static uint16_t count = 0;
- count++;
- if (count>400)
- {
- count = 0;
- // gcs().send_text(MAV_SEVERITY_INFO, "surf %d %d %d %f\n",(int)ap.at_surface,(int)ap.at_bottom,(int)motors.limit.throttle_upper,(float)motors.get_throttle());
-
- // gcs().send_text(MAV_SEVERITY_INFO, "alt %f %f %f %f\n",pos_control.get_alt_target(),barometer.get_altitude()*100,pos_control.alt_rate.get(),joystick_z);
- }
- }
- void Sub::altcontrol(){//相对机体系的手柄控制
- //深度控制
- float z_throttle = pos_control.update_z_controller_f();//输出了set_throttle_out
- //变到机体坐标系
- Vector3f throttle_vehicle_frame = ahrs.get_rotation_body_to_ned().transposed() * Vector3f(0, 0, z_throttle);
- // Output the Z controller + pilot input to all motors.
- float z_throttle_joystic = gaindelay(1.0-(float)PressLevel_f*0.1);//0~1
- motors.set_throttle(throttle_vehicle_frame.z + z_throttle_joystic);//Z轴油门
-
- rov_message.pressure_level = int(PressLevel);
- //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;
- }
- //变换到集体轴
- if (control_mode == SPORT)
- {
- motors.set_forward(constrain_float(-throttle_vehicle_frame.x + getgainf(forward),-0.8,0.8));//*0.6 变慢
- motors.set_lateral(constrain_float(-throttle_vehicle_frame.y + getgainf(lateral),-0.8,0.8));//*0.6 变慢
- }else{
- motors.set_forward(constrain_float(-throttle_vehicle_frame.x + getgainfstatble(forward),-1.0,1.0));//
- motors.set_lateral(constrain_float(-throttle_vehicle_frame.y + getgainfstatble(lateral),-1.0,1.0));//
- }
-
-
- Vector3f earth_frame_rc_inputs1 = ahrs.get_rotation_body_to_ned() * Vector3f(channel_forward->norm_input(), 0.0, (z_throttle_joystic-0.5)*2);//去掉侧移影响
- bottom_detectorgain();
-
- if (fabsf(earth_frame_rc_inputs1.z) > 0.05f) { // Throttle input above 5%
- // reset z targets to current values
- holding_depth = false;
- pos_control.relax_alt_hold_controllers();
-
- } else { // hold z
- if (ap.at_surface) { //最大油门不能向上动
- pos_control.set_alt_target(surface_depth_use()*100 - 10.0f); // set target to 5cm below surface level
-
- holding_depth = true;
- } else if (ap.at_bottom||bottom_set) {//最大油门不能向下动
- pos_control.set_alt_target(barometer.get_altitude()*100+10);//cm
- holding_depth = true;
-
- } else if (!holding_depth) {
- pos_control.calc_leash_length_z();//刹车长度 12.19
- pos_control.set_alt_target(barometer.get_altitude()*100);//cm 当前深度
- holding_depth = true;
- }
- }
- static bool lastdepth = holding_depth;
- if(lastdepth !=holding_depth){
- lastdepth = holding_depth;
- gcs().send_text(MAV_SEVERITY_INFO, " get_alt_target %d %f \n",(int)holding_depth,motors.get_throttle());
- }
-
- static uint16_t count = 0;
- count++;
- if (count>300)
- {
- count = 0;
- gcs().send_text(MAV_SEVERITY_INFO, " surface %d %d %d\n",(int)ap.at_surface,(int)ap.at_bottom,(int)motors.limit.throttle_upper);
- gcs().send_text(MAV_SEVERITY_INFO, " altitude %f %f %f\n",pos_control.get_alt_target(),barometer.get_altitude()*100,motors.get_throttle());
-
- }
- }
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