#include "Sub.h" /* * Init and run calls for guided flight mode */ #ifndef GUIDED_LOOK_AT_TARGET_MIN_DISTANCE_CM # define GUIDED_LOOK_AT_TARGET_MIN_DISTANCE_CM 500 // point nose at target if it is more than 5m away #endif #define GUIDED_POSVEL_TIMEOUT_MS 3000 // guided mode's position-velocity controller times out after 3seconds with no new updates #define GUIDED_ATTITUDE_TIMEOUT_MS 1000 // guided mode's attitude controller times out after 1 second with no new updates static Vector3f posvel_pos_target_cm; static Vector3f posvel_vel_target_cms; static uint32_t posvel_update_time_ms; static uint32_t vel_update_time_ms; struct { uint32_t update_time_ms; float roll_cd; float pitch_cd; float yaw_cd; float climb_rate_cms; } static guided_angle_state = {0,0.0f, 0.0f, 0.0f, 0.0f}; struct Guided_Limit { uint32_t timeout_ms; // timeout (in seconds) from the time that guided is invoked float alt_min_cm; // lower altitude limit in cm above home (0 = no limit) float alt_max_cm; // upper altitude limit in cm above home (0 = no limit) float horiz_max_cm; // horizontal position limit in cm from where guided mode was initiated (0 = no limit) uint32_t start_time;// system time in milliseconds that control was handed to the external computer Vector3f start_pos; // start position as a distance from home in cm. used for checking horiz_max limit } guided_limit; // guided_init - initialise guided controller bool Sub::guided_init(bool ignore_checks) { if (!position_ok() && !ignore_checks) { return false; } // initialise yaw set_auto_yaw_mode(get_default_auto_yaw_mode(false)); // start in position control mode guided_pos_control_start(); return true; } // initialise guided mode's position controller void Sub::guided_pos_control_start() { // set to position control mode guided_mode = Guided_WP; // initialise waypoint and spline controller wp_nav.wp_and_spline_init(); // initialise wpnav to stopping point at current altitude // To-Do: set to current location if disarmed? // To-Do: set to stopping point altitude? Vector3f stopping_point; stopping_point.z = inertial_nav.get_altitude(); wp_nav.get_wp_stopping_point_xy(stopping_point); // no need to check return status because terrain data is not used wp_nav.set_wp_destination(stopping_point, false); // initialise yaw set_auto_yaw_mode(get_default_auto_yaw_mode(false)); } // initialise guided mode's velocity controller void Sub::guided_vel_control_start() { // set guided_mode to velocity controller guided_mode = Guided_Velocity; // initialize vertical speeds and leash lengths pos_control.set_max_speed_z(-get_pilot_speed_dn(), g.pilot_speed_up); pos_control.set_max_accel_z(g.pilot_accel_z); // initialise velocity controller pos_control.init_vel_controller_xyz(); } // initialise guided mode's posvel controller void Sub::guided_posvel_control_start() { // set guided_mode to velocity controller guided_mode = Guided_PosVel; pos_control.init_xy_controller(); // set speed and acceleration from wpnav's speed and acceleration pos_control.set_max_speed_xy(wp_nav.get_default_speed_xy()); pos_control.set_max_accel_xy(wp_nav.get_wp_acceleration()); const Vector3f& curr_pos = inertial_nav.get_position(); const Vector3f& curr_vel = inertial_nav.get_velocity(); // set target position and velocity to current position and velocity pos_control.set_xy_target(curr_pos.x, curr_pos.y); pos_control.set_desired_velocity_xy(curr_vel.x, curr_vel.y); // set vertical speed and acceleration pos_control.set_max_speed_z(wp_nav.get_default_speed_down(), wp_nav.get_default_speed_up()); pos_control.set_max_accel_z(wp_nav.get_accel_z()); // pilot always controls yaw set_auto_yaw_mode(AUTO_YAW_HOLD); } // initialise guided mode's angle controller void Sub::guided_angle_control_start() { // set guided_mode to velocity controller guided_mode = Guided_Angle; // set vertical speed and acceleration pos_control.set_max_speed_z(wp_nav.get_default_speed_down(), wp_nav.get_default_speed_up()); pos_control.set_max_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()); // initialise targets guided_angle_state.update_time_ms = AP_HAL::millis(); guided_angle_state.roll_cd = ahrs.roll_sensor; guided_angle_state.pitch_cd = ahrs.pitch_sensor; guided_angle_state.yaw_cd = ahrs.yaw_sensor; guided_angle_state.climb_rate_cms = 0.0f; // pilot always controls yaw set_auto_yaw_mode(AUTO_YAW_HOLD); } // guided_set_destination - sets guided mode's target destination // Returns true if the fence is enabled and guided waypoint is within the fence // else return false if the waypoint is outside the fence bool Sub::guided_set_destination(const Vector3f& destination) { // ensure we are in position control mode if (guided_mode != Guided_WP) { guided_pos_control_start(); } #if AC_FENCE == ENABLED // reject destination if outside the fence const Location dest_loc(destination); if (!fence.check_destination_within_fence(dest_loc)) { AP::logger().Write_Error(LogErrorSubsystem::NAVIGATION, LogErrorCode::DEST_OUTSIDE_FENCE); // failure is propagated to GCS with NAK return false; } #endif // no need to check return status because terrain data is not used wp_nav.set_wp_destination(destination, false); // log target Log_Write_GuidedTarget(guided_mode, destination, Vector3f()); return true; } // sets guided mode's target from a Location object // returns false if destination could not be set (probably caused by missing terrain data) // or if the fence is enabled and guided waypoint is outside the fence bool Sub::guided_set_destination(const Location& dest_loc) { // ensure we are in position control mode if (guided_mode != Guided_WP) { guided_pos_control_start(); } #if AC_FENCE == ENABLED // reject destination outside the fence. // Note: there is a danger that a target specified as a terrain altitude might not be checked if the conversion to alt-above-home fails if (!fence.check_destination_within_fence(dest_loc)) { AP::logger().Write_Error(LogErrorSubsystem::NAVIGATION, LogErrorCode::DEST_OUTSIDE_FENCE); // failure is propagated to GCS with NAK return false; } #endif if (!wp_nav.set_wp_destination(dest_loc)) { // failure to set destination can only be because of missing terrain data AP::logger().Write_Error(LogErrorSubsystem::NAVIGATION, LogErrorCode::FAILED_TO_SET_DESTINATION); // failure is propagated to GCS with NAK return false; } // log target Log_Write_GuidedTarget(guided_mode, Vector3f(dest_loc.lat, dest_loc.lng, dest_loc.alt),Vector3f()); return true; } // guided_set_velocity - sets guided mode's target velocity void Sub::guided_set_velocity(const Vector3f& velocity) { // check we are in velocity control mode if (guided_mode != Guided_Velocity) { guided_vel_control_start(); } vel_update_time_ms = AP_HAL::millis(); // set position controller velocity target pos_control.set_desired_velocity(velocity); } // set guided mode posvel target bool Sub::guided_set_destination_posvel(const Vector3f& destination, const Vector3f& velocity) { // check we are in velocity control mode if (guided_mode != Guided_PosVel) { guided_posvel_control_start(); } #if AC_FENCE == ENABLED // reject destination if outside the fence const Location dest_loc(destination); if (!fence.check_destination_within_fence(dest_loc)) { AP::logger().Write_Error(LogErrorSubsystem::NAVIGATION, LogErrorCode::DEST_OUTSIDE_FENCE); // failure is propagated to GCS with NAK return false; } #endif posvel_update_time_ms = AP_HAL::millis(); posvel_pos_target_cm = destination; posvel_vel_target_cms = velocity; pos_control.set_pos_target(posvel_pos_target_cm); // log target Log_Write_GuidedTarget(guided_mode, destination, velocity); return true; } // set guided mode angle target void Sub::guided_set_angle(const Quaternion &q, float climb_rate_cms) { // check we are in velocity control mode if (guided_mode != Guided_Angle) { guided_angle_control_start(); } // convert quaternion to euler angles q.to_euler(guided_angle_state.roll_cd, guided_angle_state.pitch_cd, guided_angle_state.yaw_cd); guided_angle_state.roll_cd = ToDeg(guided_angle_state.roll_cd) * 100.0f; guided_angle_state.pitch_cd = ToDeg(guided_angle_state.pitch_cd) * 100.0f; guided_angle_state.yaw_cd = wrap_180_cd(ToDeg(guided_angle_state.yaw_cd) * 100.0f); guided_angle_state.climb_rate_cms = climb_rate_cms; guided_angle_state.update_time_ms = AP_HAL::millis(); } // guided_run - runs the guided controller // should be called at 100hz or more void Sub::guided_run() { // call the correct auto controller switch (guided_mode) { case Guided_WP: // run position controller guided_pos_control_run(); break; case Guided_Velocity: // run velocity controller guided_vel_control_run(); break; case Guided_PosVel: // run position-velocity controller guided_posvel_control_run(); break; case Guided_Angle: // run angle controller guided_angle_control_run(); break; } } // guided_pos_control_run - runs the guided position controller // called from guided_run void Sub::guided_pos_control_run() { // if motors not enabled set throttle to zero and exit immediately if (!motors.armed()) { motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::GROUND_IDLE); // Sub vehicles do not stabilize roll/pitch/yaw when disarmed attitude_control.set_throttle_out(0,true,g.throttle_filt); attitude_control.relax_attitude_controllers(); return; } // process pilot's yaw input float target_yaw_rate = 0; if (!failsafe.pilot_input) { // get pilot's desired yaw rate target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in()); if (!is_zero(target_yaw_rate)) { set_auto_yaw_mode(AUTO_YAW_HOLD); } } // set motors to full range motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED); // run waypoint controller failsafe_terrain_set_status(wp_nav.update_wpnav()); float lateral_out, forward_out; translate_wpnav_rp(lateral_out, forward_out); // Send to forward/lateral outputs motors.set_lateral(lateral_out); motors.set_forward(forward_out); // call z-axis position controller (wpnav should have already updated it's alt target) pos_control.update_z_controller(); // call attitude controller if (auto_yaw_mode == AUTO_YAW_HOLD) { // roll & pitch from waypoint controller, yaw rate from pilot attitude_control.input_euler_angle_roll_pitch_euler_rate_yaw(channel_roll->get_control_in(), channel_pitch->get_control_in(), target_yaw_rate); } else { // roll, pitch from waypoint controller, yaw heading from auto_heading() attitude_control.input_euler_angle_roll_pitch_yaw(channel_roll->get_control_in(), channel_pitch->get_control_in(), get_auto_heading(), true); } } // guided_vel_control_run - runs the guided velocity controller // called from guided_run void Sub::guided_vel_control_run() { // ifmotors not enabled set throttle to zero and exit immediately if (!motors.armed()) { // initialise velocity controller pos_control.init_vel_controller_xyz(); motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::GROUND_IDLE); // Sub vehicles do not stabilize roll/pitch/yaw when disarmed attitude_control.set_throttle_out(0,true,g.throttle_filt); attitude_control.relax_attitude_controllers(); return; } // process pilot's yaw input float target_yaw_rate = 0; if (!failsafe.pilot_input) { // get pilot's desired yaw rate target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in()); if (!is_zero(target_yaw_rate)) { set_auto_yaw_mode(AUTO_YAW_HOLD); } } // set motors to full range motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED); // set velocity to zero if no updates received for 3 seconds uint32_t tnow = AP_HAL::millis(); if (tnow - vel_update_time_ms > GUIDED_POSVEL_TIMEOUT_MS && !pos_control.get_desired_velocity().is_zero()) { pos_control.set_desired_velocity(Vector3f(0,0,0)); } // call velocity controller which includes z axis controller pos_control.update_vel_controller_xyz(); float lateral_out, forward_out; translate_pos_control_rp(lateral_out, forward_out); // Send to forward/lateral outputs motors.set_lateral(lateral_out); motors.set_forward(forward_out); // call attitude controller if (auto_yaw_mode == AUTO_YAW_HOLD) { // roll & pitch from waypoint controller, yaw rate from pilot attitude_control.input_euler_angle_roll_pitch_euler_rate_yaw(channel_roll->get_control_in(), channel_pitch->get_control_in(), target_yaw_rate); } else { // roll, pitch from waypoint controller, yaw heading from auto_heading() attitude_control.input_euler_angle_roll_pitch_yaw(channel_roll->get_control_in(), channel_pitch->get_control_in(), get_auto_heading(), true); } } // guided_posvel_control_run - runs the guided spline controller // called from guided_run void Sub::guided_posvel_control_run() { // if motors not enabled set throttle to zero and exit immediately if (!motors.armed()) { // set target position and velocity to current position and velocity pos_control.set_pos_target(inertial_nav.get_position()); pos_control.set_desired_velocity(Vector3f(0,0,0)); motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::GROUND_IDLE); // Sub vehicles do not stabilize roll/pitch/yaw when disarmed attitude_control.set_throttle_out(0,true,g.throttle_filt); attitude_control.relax_attitude_controllers(); return; } // process pilot's yaw input float target_yaw_rate = 0; if (!failsafe.pilot_input) { // get pilot's desired yaw rate target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in()); if (!is_zero(target_yaw_rate)) { set_auto_yaw_mode(AUTO_YAW_HOLD); } } // set motors to full range motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED); // set velocity to zero if no updates received for 3 seconds uint32_t tnow = AP_HAL::millis(); if (tnow - posvel_update_time_ms > GUIDED_POSVEL_TIMEOUT_MS && !posvel_vel_target_cms.is_zero()) { posvel_vel_target_cms.zero(); } // calculate dt float dt = pos_control.time_since_last_xy_update(); // sanity check dt if (dt >= 0.2f) { dt = 0.0f; } // advance position target using velocity target posvel_pos_target_cm += posvel_vel_target_cms * dt; // send position and velocity targets to position controller pos_control.set_pos_target(posvel_pos_target_cm); pos_control.set_desired_velocity_xy(posvel_vel_target_cms.x, posvel_vel_target_cms.y); // run position controller pos_control.update_xy_controller(); float lateral_out, forward_out; translate_pos_control_rp(lateral_out, forward_out); // Send to forward/lateral outputs motors.set_lateral(lateral_out); motors.set_forward(forward_out); pos_control.update_z_controller(); // call attitude controller if (auto_yaw_mode == AUTO_YAW_HOLD) { // roll & pitch from waypoint controller, yaw rate from pilot attitude_control.input_euler_angle_roll_pitch_euler_rate_yaw(channel_roll->get_control_in(), channel_pitch->get_control_in(), target_yaw_rate); } else { // roll, pitch from waypoint controller, yaw heading from auto_heading() attitude_control.input_euler_angle_roll_pitch_yaw(channel_roll->get_control_in(), channel_pitch->get_control_in(), get_auto_heading(), true); } } // guided_angle_control_run - runs the guided angle controller // called from guided_run void Sub::guided_angle_control_run() { // if motors not enabled set throttle to zero and exit immediately if (!motors.armed()) { motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::GROUND_IDLE); // Sub vehicles do not stabilize roll/pitch/yaw when disarmed attitude_control.set_throttle_out(0.0f,true,g.throttle_filt); attitude_control.relax_attitude_controllers(); pos_control.relax_alt_hold_controllers(motors.get_throttle_hover()); return; } // constrain desired lean angles float roll_in = guided_angle_state.roll_cd; float pitch_in = guided_angle_state.pitch_cd; float total_in = norm(roll_in, pitch_in); float angle_max = MIN(attitude_control.get_althold_lean_angle_max(), aparm.angle_max); if (total_in > angle_max) { float ratio = angle_max / total_in; roll_in *= ratio; pitch_in *= ratio; } // wrap yaw request float yaw_in = wrap_180_cd(guided_angle_state.yaw_cd); // constrain climb rate float climb_rate_cms = constrain_float(guided_angle_state.climb_rate_cms, -fabsf(wp_nav.get_default_speed_down()), wp_nav.get_default_speed_up()); // check for timeout - set lean angles and climb rate to zero if no updates received for 3 seconds uint32_t tnow = AP_HAL::millis(); if (tnow - guided_angle_state.update_time_ms > GUIDED_ATTITUDE_TIMEOUT_MS) { roll_in = 0.0f; pitch_in = 0.0f; climb_rate_cms = 0.0f; } // set motors to full range motors.set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED); // call attitude controller attitude_control.input_euler_angle_roll_pitch_yaw(roll_in, pitch_in, yaw_in, true); // call position controller pos_control.set_alt_target_from_climb_rate_ff(climb_rate_cms, G_Dt, false); pos_control.update_z_controller(); } // Guided Limit code // guided_limit_clear - clear/turn off guided limits void Sub::guided_limit_clear() { guided_limit.timeout_ms = 0; guided_limit.alt_min_cm = 0.0f; guided_limit.alt_max_cm = 0.0f; guided_limit.horiz_max_cm = 0.0f; } // guided_limit_set - set guided timeout and movement limits void Sub::guided_limit_set(uint32_t timeout_ms, float alt_min_cm, float alt_max_cm, float horiz_max_cm) { guided_limit.timeout_ms = timeout_ms; guided_limit.alt_min_cm = alt_min_cm; guided_limit.alt_max_cm = alt_max_cm; guided_limit.horiz_max_cm = horiz_max_cm; } // guided_limit_init_time_and_pos - initialise guided start time and position as reference for limit checking // only called from AUTO mode's auto_nav_guided_start function void Sub::guided_limit_init_time_and_pos() { // initialise start time guided_limit.start_time = AP_HAL::millis(); // initialise start position from current position guided_limit.start_pos = inertial_nav.get_position(); } // guided_limit_check - returns true if guided mode has breached a limit // used when guided is invoked from the NAV_GUIDED_ENABLE mission command bool Sub::guided_limit_check() { // check if we have passed the timeout if ((guided_limit.timeout_ms > 0) && (AP_HAL::millis() - guided_limit.start_time >= guided_limit.timeout_ms)) { return true; } // get current location const Vector3f& curr_pos = inertial_nav.get_position(); // check if we have gone below min alt if (!is_zero(guided_limit.alt_min_cm) && (curr_pos.z < guided_limit.alt_min_cm)) { return true; } // check if we have gone above max alt if (!is_zero(guided_limit.alt_max_cm) && (curr_pos.z > guided_limit.alt_max_cm)) { return true; } // check if we have gone beyond horizontal limit if (guided_limit.horiz_max_cm > 0.0f) { float horiz_move = get_horizontal_distance_cm(guided_limit.start_pos, curr_pos); if (horiz_move > guided_limit.horiz_max_cm) { return true; } } // if we got this far we must be within limits return false; }