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