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203 lines
8.4 KiB
203 lines
8.4 KiB
#include "AP_Mount_Servo.h" |
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#include <AP_GPS/AP_GPS.h> |
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extern const AP_HAL::HAL& hal; |
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// init - performs any required initialisation for this instance |
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void AP_Mount_Servo::init(const AP_SerialManager& serial_manager) |
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{ |
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if (_instance == 0) { |
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_roll_idx = SRV_Channel::k_mount_roll; |
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_tilt_idx = SRV_Channel::k_mount_tilt; |
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_pan_idx = SRV_Channel::k_mount_pan; |
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_open_idx = SRV_Channel::k_mount_open; |
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} else { |
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// this must be the 2nd mount |
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_roll_idx = SRV_Channel::k_mount2_roll; |
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_tilt_idx = SRV_Channel::k_mount2_tilt; |
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_pan_idx = SRV_Channel::k_mount2_pan; |
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_open_idx = SRV_Channel::k_mount2_open; |
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} |
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// check which servos have been assigned |
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check_servo_map(); |
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} |
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// update mount position - should be called periodically |
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void AP_Mount_Servo::update() |
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{ |
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static bool mount_open = 0; // 0 is closed |
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// check servo map every three seconds to allow users to modify parameters |
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uint32_t now = AP_HAL::millis(); |
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if (now - _last_check_servo_map_ms > 3000) { |
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check_servo_map(); |
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_last_check_servo_map_ms = now; |
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} |
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switch(get_mode()) { |
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// move mount to a "retracted position" or to a position where a fourth servo can retract the entire mount into the fuselage |
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case MAV_MOUNT_MODE_RETRACT: |
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{ |
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_angle_bf_output_deg = _state._retract_angles.get(); |
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break; |
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} |
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// move mount to a neutral position, typically pointing forward |
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case MAV_MOUNT_MODE_NEUTRAL: |
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{ |
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_angle_bf_output_deg = _state._neutral_angles.get(); |
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break; |
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} |
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// point to the angles given by a mavlink message |
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case MAV_MOUNT_MODE_MAVLINK_TARGETING: |
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{ |
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// earth-frame angle targets (i.e. _angle_ef_target_rad) should have already been set by a MOUNT_CONTROL message from GCS |
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stabilize(); |
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break; |
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} |
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// RC radio manual angle control, but with stabilization from the AHRS |
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case MAV_MOUNT_MODE_RC_TARGETING: |
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{ |
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// update targets using pilot's rc inputs |
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update_targets_from_rc(); |
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stabilize(); |
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break; |
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} |
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// point mount to a GPS point given by the mission planner |
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case MAV_MOUNT_MODE_GPS_POINT: |
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{ |
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if(AP::gps().status() >= AP_GPS::GPS_OK_FIX_2D) { |
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calc_angle_to_location(_state._roi_target, _angle_ef_target_rad, _flags.tilt_control, _flags.pan_control, false); |
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stabilize(); |
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} |
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break; |
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} |
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default: |
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//do nothing |
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break; |
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} |
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// move mount to a "retracted position" into the fuselage with a fourth servo |
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bool mount_open_new = (get_mode() == MAV_MOUNT_MODE_RETRACT) ? 0 : 1; |
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if (mount_open != mount_open_new) { |
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mount_open = mount_open_new; |
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move_servo(_open_idx, mount_open_new, 0, 1); |
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} |
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// write the results to the servos |
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move_servo(_roll_idx, _angle_bf_output_deg.x*10, _state._roll_angle_min*0.1f, _state._roll_angle_max*0.1f); |
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move_servo(_tilt_idx, _angle_bf_output_deg.y*10, _state._tilt_angle_min*0.1f, _state._tilt_angle_max*0.1f); |
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move_servo(_pan_idx, _angle_bf_output_deg.z*10, _state._pan_angle_min*0.1f, _state._pan_angle_max*0.1f); |
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} |
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// set_mode - sets mount's mode |
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void AP_Mount_Servo::set_mode(enum MAV_MOUNT_MODE mode) |
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{ |
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// record the mode change and return success |
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_state._mode = mode; |
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} |
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// private methods |
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// check_servo_map - detects which axis we control using the functions assigned to the servos in the RC_Channel_aux |
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// should be called periodically (i.e. 1hz or less) |
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void AP_Mount_Servo::check_servo_map() |
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{ |
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_flags.roll_control = SRV_Channels::function_assigned(_roll_idx); |
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_flags.tilt_control = SRV_Channels::function_assigned(_tilt_idx); |
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_flags.pan_control = SRV_Channels::function_assigned(_pan_idx); |
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} |
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// send_mount_status - called to allow mounts to send their status to GCS using the MOUNT_STATUS message |
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void AP_Mount_Servo::send_mount_status(mavlink_channel_t chan) |
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{ |
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mavlink_msg_mount_status_send(chan, 0, 0, _angle_bf_output_deg.y*100, _angle_bf_output_deg.x*100, _angle_bf_output_deg.z*100); |
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} |
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// stabilize - stabilizes the mount relative to the Earth's frame |
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// input: _angle_ef_target_rad (earth frame targets in radians) |
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// output: _angle_bf_output_deg (body frame angles in degrees) |
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void AP_Mount_Servo::stabilize() |
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{ |
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AP_AHRS &ahrs = AP::ahrs(); |
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// only do the full 3D frame transform if we are doing pan control |
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if (_state._stab_pan) { |
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Matrix3f m; ///< holds 3 x 3 matrix, var is used as temp in calcs |
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Matrix3f cam; ///< Rotation matrix earth to camera. Desired camera from input. |
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Matrix3f gimbal_target; ///< Rotation matrix from plane to camera. Then Euler angles to the servos. |
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m = ahrs.get_rotation_body_to_ned(); |
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m.transpose(); |
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cam.from_euler(_angle_ef_target_rad.x, _angle_ef_target_rad.y, _angle_ef_target_rad.z); |
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gimbal_target = m * cam; |
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gimbal_target.to_euler(&_angle_bf_output_deg.x, &_angle_bf_output_deg.y, &_angle_bf_output_deg.z); |
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_angle_bf_output_deg.x = _state._stab_roll ? degrees(_angle_bf_output_deg.x) : degrees(_angle_ef_target_rad.x); |
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_angle_bf_output_deg.y = _state._stab_tilt ? degrees(_angle_bf_output_deg.y) : degrees(_angle_ef_target_rad.y); |
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_angle_bf_output_deg.z = degrees(_angle_bf_output_deg.z); |
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} else { |
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// otherwise base mount roll and tilt on the ahrs |
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// roll/tilt attitude, plus any requested angle |
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_angle_bf_output_deg.x = degrees(_angle_ef_target_rad.x); |
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_angle_bf_output_deg.y = degrees(_angle_ef_target_rad.y); |
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_angle_bf_output_deg.z = degrees(_angle_ef_target_rad.z); |
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if (_state._stab_roll) { |
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_angle_bf_output_deg.x -= degrees(ahrs.roll); |
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} |
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if (_state._stab_tilt) { |
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_angle_bf_output_deg.y -= degrees(ahrs.pitch); |
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} |
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// lead filter |
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const Vector3f &gyro = ahrs.get_gyro(); |
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if (_state._stab_roll && !is_zero(_state._roll_stb_lead) && fabsf(ahrs.pitch) < M_PI/3.0f) { |
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// Compute rate of change of euler roll angle |
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float roll_rate = gyro.x + (ahrs.sin_pitch() / ahrs.cos_pitch()) * (gyro.y * ahrs.sin_roll() + gyro.z * ahrs.cos_roll()); |
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_angle_bf_output_deg.x -= degrees(roll_rate) * _state._roll_stb_lead; |
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} |
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if (_state._stab_tilt && !is_zero(_state._pitch_stb_lead)) { |
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// Compute rate of change of euler pitch angle |
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float pitch_rate = ahrs.cos_pitch() * gyro.y - ahrs.sin_roll() * gyro.z; |
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_angle_bf_output_deg.y -= degrees(pitch_rate) * _state._pitch_stb_lead; |
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} |
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} |
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} |
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// closest_limit - returns closest angle to 'angle' taking into account limits. all angles are in degrees * 10 |
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int16_t AP_Mount_Servo::closest_limit(int16_t angle, int16_t angle_min, int16_t angle_max) |
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{ |
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// Make sure the angle lies in the interval [-180 .. 180[ degrees |
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while (angle < -1800) angle += 3600; |
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while (angle >= 1800) angle -= 3600; |
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// Make sure the angle limits lie in the interval [-180 .. 180[ degrees |
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while (angle_min < -1800) angle_min += 3600; |
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while (angle_min >= 1800) angle_min -= 3600; |
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while (angle_max < -1800) angle_max += 3600; |
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while (angle_max >= 1800) angle_max -= 3600; |
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// If the angle is outside servo limits, saturate the angle to the closest limit |
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// On a circle the closest angular position must be carefully calculated to account for wrap-around |
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if ((angle < angle_min) && (angle > angle_max)) { |
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// angle error if min limit is used |
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int16_t err_min = angle_min - angle + (angle<angle_min ? 0 : 3600); // add 360 degrees if on the "wrong side" |
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// angle error if max limit is used |
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int16_t err_max = angle - angle_max + (angle>angle_max ? 0 : 3600); // add 360 degrees if on the "wrong side" |
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angle = err_min<err_max ? angle_min : angle_max; |
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} |
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return angle; |
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} |
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// move_servo - moves servo with the given id to the specified angle. all angles are in degrees * 10 |
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void AP_Mount_Servo::move_servo(uint8_t function_idx, int16_t angle, int16_t angle_min, int16_t angle_max) |
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{ |
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// saturate to the closest angle limit if outside of [min max] angle interval |
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int16_t servo_out = closest_limit(angle, angle_min, angle_max); |
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SRV_Channels::move_servo((SRV_Channel::Aux_servo_function_t)function_idx, servo_out, angle_min, angle_max); |
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}
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