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AC_AttitudeControl: only use rate shaping tc if tc is nonzero

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Bill Geyer 2022-04-16 23:47:14 -04:00 committed by Randy Mackay
parent 7594f7a558
commit a547916ebf
1 changed files with 58 additions and 14 deletions
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44
libraries/AC_AttitudeControl/AC_AttitudeControl.cpp
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@ -287,7 +287,11 @@ void AC_AttitudeControl::input_euler_angle_roll_pitch_euler_rate_yaw(float euler
// When yaw acceleration limiting is enabled, the yaw input shaper constrains angular acceleration about the yaw axis, slewing
// the output rate towards the input rate.
if (is_zero(_rate_y_tc)) {
_euler_rate_target.z = input_shaping_ang_vel(_euler_rate_target.z, euler_yaw_rate, euler_accel.z, _dt);
} else {
_euler_rate_target.z = input_shaping_rate((euler_yaw_rate - _euler_rate_target.z), _rate_y_tc, euler_accel.z, _euler_rate_target.z, _dt);
}
// Convert euler angle derivative of desired attitude into a body-frame angular velocity vector for feedforward
euler_rate_to_ang_vel(_euler_angle_target, _euler_rate_target, _ang_vel_target);
@ -388,9 +392,18 @@ void AC_AttitudeControl::input_euler_rate_roll_pitch_yaw(float euler_roll_rate_c
// When acceleration limiting is enabled, the input shaper constrains angular acceleration, slewing
// the output rate towards the input rate.
if (is_zero(_rate_rp_tc)) {
_euler_rate_target.x = input_shaping_ang_vel(_euler_rate_target.x, euler_roll_rate, euler_accel.x, _dt);
_euler_rate_target.y = input_shaping_ang_vel(_euler_rate_target.y, euler_pitch_rate, euler_accel.y, _dt);
} else {
_euler_rate_target.x = input_shaping_rate((euler_roll_rate - _euler_rate_target.x), _rate_rp_tc, euler_accel.x, _euler_rate_target.x, _dt);
_euler_rate_target.y = input_shaping_rate((euler_pitch_rate - _euler_rate_target.y), _rate_rp_tc, euler_accel.y, _euler_rate_target.y, _dt);
}
if (is_zero(_rate_y_tc)) {
_euler_rate_target.z = input_shaping_ang_vel(_euler_rate_target.z, euler_yaw_rate, euler_accel.z, _dt);
} else {
_euler_rate_target.z = input_shaping_rate((euler_yaw_rate - _euler_rate_target.z), _rate_y_tc, euler_accel.z, _euler_rate_target.z, _dt);
}
// Convert euler angle derivative of desired attitude into a body-frame angular velocity vector for feedforward
euler_rate_to_ang_vel(_euler_angle_target, _euler_rate_target, _ang_vel_target);
@ -428,9 +441,18 @@ void AC_AttitudeControl::input_rate_bf_roll_pitch_yaw(float roll_rate_bf_cds, fl
// Compute acceleration-limited body frame rates
// When acceleration limiting is enabled, the input shaper constrains angular acceleration about the axis, slewing
// the output rate towards the input rate.
if (is_zero(_rate_rp_tc)) {
_ang_vel_target.x = input_shaping_ang_vel(_ang_vel_target.x, roll_rate_rads, get_accel_roll_max_radss(), _dt);
_ang_vel_target.y = input_shaping_ang_vel(_ang_vel_target.y, pitch_rate_rads, get_accel_pitch_max_radss(), _dt);
} else {
_ang_vel_target.x = input_shaping_rate((roll_rate_rads - _ang_vel_target.x), _rate_rp_tc, get_accel_roll_max_radss(), _ang_vel_target.x, _dt);
_ang_vel_target.y = input_shaping_rate((pitch_rate_rads - _ang_vel_target.y), _rate_rp_tc, get_accel_pitch_max_radss(), _ang_vel_target.y, _dt);
}
if (is_zero(_rate_y_tc)) {
_ang_vel_target.z = input_shaping_ang_vel(_ang_vel_target.z, yaw_rate_rads, get_accel_yaw_max_radss(), _dt);
} else {
_ang_vel_target.z = input_shaping_rate((yaw_rate_rads - _ang_vel_target.z), _rate_y_tc, get_accel_yaw_max_radss(), _ang_vel_target.z, _dt);
}
// Convert body-frame angular velocity into euler angle derivative of desired attitude
ang_vel_to_euler_rate(_euler_angle_target, _ang_vel_target, _euler_rate_target);
@ -461,9 +483,18 @@ void AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_2(float roll_rate_bf_cds,
// Compute acceleration-limited body frame rates
// When acceleration limiting is enabled, the input shaper constrains angular acceleration about the axis, slewing
// the output rate towards the input rate.
if (is_zero(_rate_rp_tc)) {
_ang_vel_target.x = input_shaping_ang_vel(_ang_vel_target.x, roll_rate_rads, get_accel_roll_max_radss(), _dt);
_ang_vel_target.y = input_shaping_ang_vel(_ang_vel_target.y, pitch_rate_rads, get_accel_pitch_max_radss(), _dt);
} else {
_ang_vel_target.x = input_shaping_rate((roll_rate_rads - _ang_vel_target.x), _rate_rp_tc, get_accel_roll_max_radss(), _ang_vel_target.x, _dt);
_ang_vel_target.y = input_shaping_rate((pitch_rate_rads - _ang_vel_target.y), _rate_rp_tc, get_accel_pitch_max_radss(), _ang_vel_target.y, _dt);
}
if (is_zero(_rate_y_tc)) {
_ang_vel_target.z = input_shaping_ang_vel(_ang_vel_target.z, yaw_rate_rads, get_accel_yaw_max_radss(), _dt);
} else {
_ang_vel_target.z = input_shaping_rate((yaw_rate_rads - _ang_vel_target.z), _rate_y_tc, get_accel_yaw_max_radss(), _ang_vel_target.z, _dt);
}
// Update the unused targets attitude based on current attitude to condition mode change
_ahrs.get_quat_body_to_ned(_attitude_target);
@ -500,9 +531,18 @@ void AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_3(float roll_rate_bf_cds,
// Compute acceleration-limited body frame rates
// When acceleration limiting is enabled, the input shaper constrains angular acceleration about the axis, slewing
// the output rate towards the input rate.
if (is_zero(_rate_rp_tc)) {
_ang_vel_target.x = input_shaping_ang_vel(_ang_vel_target.x, roll_rate_rads, get_accel_roll_max_radss(), _dt);
_ang_vel_target.y = input_shaping_ang_vel(_ang_vel_target.y, pitch_rate_rads, get_accel_pitch_max_radss(), _dt);
} else {
_ang_vel_target.x = input_shaping_rate((roll_rate_rads - _ang_vel_target.x), _rate_rp_tc, get_accel_roll_max_radss(), _ang_vel_target.x, _dt);
_ang_vel_target.y = input_shaping_rate((pitch_rate_rads - _ang_vel_target.y), _rate_rp_tc, get_accel_pitch_max_radss(), _ang_vel_target.y, _dt);
}
if (is_zero(_rate_y_tc)) {
_ang_vel_target.z = input_shaping_ang_vel(_ang_vel_target.z, yaw_rate_rads, get_accel_yaw_max_radss(), _dt);
} else {
_ang_vel_target.z = input_shaping_rate((yaw_rate_rads - _ang_vel_target.z), _rate_y_tc, get_accel_yaw_max_radss(), _ang_vel_target.z, _dt);
}
// Retrieve quaternion body attitude
Quaternion attitude_body;
@ -584,7 +624,11 @@ void AC_AttitudeControl::input_thrust_vector_rate_heading(const Vector3f& thrust
// When yaw acceleration limiting is enabled, the yaw input shaper constrains angular acceleration about the yaw axis, slewing
// the output rate towards the input rate.
if (is_zero(_rate_y_tc)) {
_ang_vel_target.z = input_shaping_ang_vel(_ang_vel_target.z, heading_rate, get_accel_yaw_max_radss(), _dt);
} else {
_ang_vel_target.z = input_shaping_rate((heading_rate - _ang_vel_target.z), _rate_y_tc, get_accel_yaw_max_radss(), _ang_vel_target.z, _dt);
}
// Limit the angular velocity
ang_vel_limit(_ang_vel_target, radians(_ang_vel_roll_max), radians(_ang_vel_pitch_max), radians(_ang_vel_yaw_max));