#include "Sub.h" bool Sub::surface_init() { #if CONFIG_HAL_BOARD != HAL_BOARD_SITL if(!control_check_barometer()) { return false; } #endif // initialize vertical speeds and leash lengths pos_control.set_speed_z(wp_nav.get_speed_down(), wp_nav.get_speed_up()); pos_control.set_accel_z(wp_nav.get_accel_z()); // initialise position and desired velocity pos_control.set_alt_target(inertial_nav.get_altitude()); pos_control.set_desired_velocity_z(inertial_nav.get_velocity_z()); return true; } void Sub::surface_run() { float target_roll, target_pitch; float target_yaw_rate; // if not armed set throttle to zero and exit immediately if (!motors.armed()) { motors.output_min(); motors.set_desired_spool_state(AP_Motors::DESIRED_SPIN_WHEN_ARMED); attitude_control.set_throttle_out_unstabilized(0,true,g.throttle_filt); return; } // Already at surface, hold depth at surface if (ap.at_surface) { set_mode(ALT_HOLD, MODE_REASON_SURFACE_COMPLETE); } // convert pilot input to lean angles // To-Do: convert get_pilot_desired_lean_angles to return angles as floats get_pilot_desired_lean_angles(channel_roll->get_control_in(), channel_pitch->get_control_in(), target_roll, target_pitch, aparm.angle_max); // get pilot's desired yaw rate target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in()); // call attitude controller attitude_control.input_euler_angle_roll_pitch_euler_rate_yaw(target_roll, target_pitch, target_yaw_rate); // set target climb rate float cmb_rate = constrain_float(abs(wp_nav.get_speed_up()), 1, pos_control.get_speed_up()); // record desired climb rate for logging desired_climb_rate = cmb_rate; // update altitude target and call position controller pos_control.set_alt_target_from_climb_rate_ff(cmb_rate, G_Dt, true); pos_control.update_z_controller(); // pilot has control for repositioning motors.set_forward(channel_forward->norm_input()); motors.set_lateral(channel_lateral->norm_input()); }