/************************************************************* throttle control ****************************************************************/ // user input: // ----------- void output_manual_throttle() { rc_3.servo_out = rc_3.control_in; rc_3.servo_out = (float)rc_3.servo_out * angle_boost(); } // Autopilot // --------- void output_auto_throttle() { rc_3.servo_out = (float)nav_throttle * angle_boost(); rc_3.servo_out = max(rc_3.servo_out, 1); } // Jason void calc_nav_throttle() { long err = constrain (altitude_error, -300, 300); //+-3 meters long temp = pid_throttle.get_pid(err, deltaMiliSeconds, 1.0); nav_throttle = (float)(throttle_cruise + temp) * angle_boost(); } float angle_boost() { //static byte flipper; float temp = 1 / (cos(dcm.roll) * cos(dcm.pitch)); temp *= .5; if(temp > 1.2) temp = 1.2; return temp; } /************************************************************* yaw control ****************************************************************/ void input_yaw_hold_2() { if(rc_3.control_in == 0){ // Reset the yaw hold nav_yaw = yaw_sensor; }else if(rc_4.control_in == 0){ // do nothing }else{ // create up to 60° of yaw error nav_yaw = yaw_sensor + rc_4.control_in; nav_yaw = wrap_360(nav_yaw); } } void input_yaw_hold() { if(rc_3.control_in == 0){ // Reset the yaw hold nav_yaw = yaw_sensor; }else if(rc_4.control_in == 0){ // do nothing }else{ // create up to 60° of yaw error nav_yaw += ((long)rc_4.control_in * (long)deltaMiliSeconds) / 500; // we'll get 60° * 2 or 120° per second nav_yaw = wrap_360(nav_yaw); } } /*void output_yaw_stabilize() { rc_4.servo_out = rc_4.control_in; rc_4.servo_out = constrain(rc_4.servo_out, -MAX_SERVO_OUTPUT, MAX_SERVO_OUTPUT); }*/ /************************************************************* picth and roll control ****************************************************************/ // how hard to tilt towards the target // ----------------------------------- void calc_nav_pid() { nav_angle = pid_nav.get_pid(wp_distance * 100, dTnav, 1.0); nav_angle = constrain(nav_angle, -pitch_max, pitch_max); } // distribute the pitch angle based on our orientation // --------------------------------------------------- void calc_nav_pitch() { long b_err = bearing_error; bool rev = false; float roll_out; if(b_err > 18000){ b_err -= 18000; rev = true; } roll_out = abs(b_err - 18000); roll_out = (9000.0 - roll_out) / 9000.0; roll_out = (rev) ? roll_out : -roll_out; nav_pitch = (float)nav_angle * roll_out; } // distribute the roll angle based on our orientation // -------------------------------------------------- void calc_nav_roll() { long b_err = bearing_error; bool rev = false; float roll_out; if(b_err > 18000){ b_err -= 18000; rev = true; } roll_out = abs(b_err - 9000); roll_out = (9000.0 - roll_out) / 9000.0; roll_out = (rev) ? -roll_out : roll_out; nav_roll = (float)nav_angle * roll_out; }