ardupilot/libraries/AP_Mount/AP_Mount_Servo.cpp

187 lines
6.9 KiB
C++

#include "AP_Mount_Servo.h"
#if HAL_MOUNT_SERVO_ENABLED
#include <AP_AHRS/AP_AHRS.h>
#include <GCS_MAVLink/GCS_MAVLink.h>
extern const AP_HAL::HAL& hal;
// init - performs any required initialisation for this instance
void AP_Mount_Servo::init()
{
if (_instance == 0) {
_roll_idx = SRV_Channel::k_mount_roll;
_tilt_idx = SRV_Channel::k_mount_tilt;
_pan_idx = SRV_Channel::k_mount_pan;
_open_idx = SRV_Channel::k_mount_open;
} else {
// this must be the 2nd mount
_roll_idx = SRV_Channel::k_mount2_roll;
_tilt_idx = SRV_Channel::k_mount2_tilt;
_pan_idx = SRV_Channel::k_mount2_pan;
_open_idx = SRV_Channel::k_mount2_open;
}
}
// update mount position - should be called periodically
void AP_Mount_Servo::update()
{
switch (get_mode()) {
// move mount to a "retracted position" or to a position where a fourth servo can retract the entire mount into the fuselage
case MAV_MOUNT_MODE_RETRACT: {
_angle_bf_output_deg = _params.retract_angles.get();
// initialise _angle_rad to smooth transition if user changes to RC_TARGETTING
_angle_rad.roll = radians(_angle_bf_output_deg.x);
_angle_rad.pitch = radians(_angle_bf_output_deg.y);
_angle_rad.yaw = radians(_angle_bf_output_deg.z);
_angle_rad.yaw_is_ef = false;
break;
}
// move mount to a neutral position, typically pointing forward
case MAV_MOUNT_MODE_NEUTRAL: {
_angle_bf_output_deg = _params.neutral_angles.get();
// initialise _angle_rad to smooth transition if user changes to RC_TARGETTING
_angle_rad.roll = radians(_angle_bf_output_deg.x);
_angle_rad.pitch = radians(_angle_bf_output_deg.y);
_angle_rad.yaw = radians(_angle_bf_output_deg.z);
_angle_rad.yaw_is_ef = false;
break;
}
// point to the angles given by a mavlink message
case MAV_MOUNT_MODE_MAVLINK_TARGETING: {
switch (mavt_target.target_type) {
case MountTargetType::ANGLE:
_angle_rad = mavt_target.angle_rad;
break;
case MountTargetType::RATE:
update_angle_target_from_rate(mavt_target.rate_rads, _angle_rad);
break;
}
// update _angle_bf_output_deg based on angle target
update_angle_outputs(_angle_rad);
break;
}
// RC radio manual angle control, but with stabilization from the AHRS
case MAV_MOUNT_MODE_RC_TARGETING: {
// update targets using pilot's RC inputs
MountTarget rc_target {};
if (get_rc_rate_target(rc_target)) {
update_angle_target_from_rate(rc_target, _angle_rad);
} else if (get_rc_angle_target(rc_target)) {
_angle_rad = rc_target;
}
// update _angle_bf_output_deg based on angle target
update_angle_outputs(_angle_rad);
break;
}
// point mount to a GPS location
case MAV_MOUNT_MODE_GPS_POINT: {
if (get_angle_target_to_roi(_angle_rad)) {
update_angle_outputs(_angle_rad);
}
break;
}
case MAV_MOUNT_MODE_HOME_LOCATION: {
if (get_angle_target_to_home(_angle_rad)) {
update_angle_outputs(_angle_rad);
}
break;
}
case MAV_MOUNT_MODE_SYSID_TARGET: {
if (get_angle_target_to_sysid(_angle_rad)) {
update_angle_outputs(_angle_rad);
}
break;
}
default:
//do nothing
break;
}
// move mount to a "retracted position" into the fuselage with a fourth servo
const bool mount_open = (get_mode() == MAV_MOUNT_MODE_RETRACT) ? 0 : 1;
move_servo(_open_idx, mount_open, 0, 1);
// write the results to the servos
move_servo(_roll_idx, _angle_bf_output_deg.x*10, _params.roll_angle_min*10, _params.roll_angle_max*10);
move_servo(_tilt_idx, _angle_bf_output_deg.y*10, _params.pitch_angle_min*10, _params.pitch_angle_max*10);
move_servo(_pan_idx, _angle_bf_output_deg.z*10, _params.yaw_angle_min*10, _params.yaw_angle_max*10);
}
// returns true if this mount can control its pan (required for multicopters)
bool AP_Mount_Servo::has_pan_control() const
{
return SRV_Channels::function_assigned(_pan_idx) && yaw_range_valid();
}
// get attitude as a quaternion. returns true on success
bool AP_Mount_Servo::get_attitude_quaternion(Quaternion& att_quat)
{
att_quat.from_euler(radians(_angle_bf_output_deg.x), radians(_angle_bf_output_deg.y), radians(_angle_bf_output_deg.z));
return true;
}
// private methods
// update body-frame angle outputs from earth-frame angle targets
void AP_Mount_Servo::update_angle_outputs(const MountTarget& angle_rad)
{
const AP_AHRS &ahrs = AP::ahrs();
// get target yaw in body-frame with limits applied
const float yaw_bf_rad = constrain_float(get_bf_yaw_angle(angle_rad), radians(_params.yaw_angle_min), radians(_params.yaw_angle_max));
// default output to target earth-frame roll and pitch angles, body-frame yaw
_angle_bf_output_deg.x = degrees(angle_rad.roll);
_angle_bf_output_deg.y = degrees(angle_rad.pitch);
_angle_bf_output_deg.z = degrees(yaw_bf_rad);
// this is sufficient for self-stabilising brushless gimbals
if (!requires_stabilization) {
return;
}
// retrieve lean angles from ahrs
Vector2f ahrs_angle_rad = {ahrs.roll, ahrs.pitch};
// rotate ahrs roll and pitch angles to gimbal yaw
if (has_pan_control()) {
ahrs_angle_rad.rotate(-yaw_bf_rad);
}
// add roll and pitch lean angle correction
_angle_bf_output_deg.x -= degrees(ahrs_angle_rad.x);
_angle_bf_output_deg.y -= degrees(ahrs_angle_rad.y);
// lead filter
const Vector3f &gyro = ahrs.get_gyro();
if (!is_zero(_params.roll_stb_lead) && fabsf(ahrs.pitch) < M_PI/3.0f) {
// Compute rate of change of euler roll angle
float roll_rate = gyro.x + (ahrs.sin_pitch() / ahrs.cos_pitch()) * (gyro.y * ahrs.sin_roll() + gyro.z * ahrs.cos_roll());
_angle_bf_output_deg.x -= degrees(roll_rate) * _params.roll_stb_lead;
}
if (!is_zero(_params.pitch_stb_lead)) {
// Compute rate of change of euler pitch angle
float pitch_rate = ahrs.cos_pitch() * gyro.y - ahrs.sin_roll() * gyro.z;
_angle_bf_output_deg.y -= degrees(pitch_rate) * _params.pitch_stb_lead;
}
}
// move_servo - moves servo with the given id to the specified angle. all angles are in degrees * 10
void AP_Mount_Servo::move_servo(uint8_t function_idx, int16_t angle, int16_t angle_min, int16_t angle_max)
{
SRV_Channels::move_servo((SRV_Channel::Aux_servo_function_t)function_idx, angle, angle_min, angle_max);
}
#endif // HAL_MOUNT_SERVO_ENABLED