mirror of
https://github.com/sunnypilot/sunnypilot.git
synced 2026-02-18 23:33:58 +08:00
locationd : Acceleration Bias in locationd (#22879)
* add accel bias to filter for offline calculation
* bugfix acc bias in live_kf
* add no_accel obsertvation
* increase initial certainty of acc-bias and reduce PN
* increase initial certainty of acc-bias and reduce PN
* increase accel bias PN
* increase obs noise for no_accel observation
* style fixes
* update refs
old-commit-hash: 534bf697ee
This commit is contained in:
@@ -305,6 +305,7 @@ void Localizer::handle_car_state(double current_time, const cereal::CarState::Re
|
||||
this->car_speed = std::abs(log.getVEgo());
|
||||
if (log.getStandstill()) {
|
||||
this->kf->predict_and_observe(current_time, OBSERVATION_NO_ROT, { Vector3d(0.0, 0.0, 0.0) });
|
||||
this->kf->predict_and_observe(current_time, OBSERVATION_NO_ACCEL, { Vector3d(0.0, 0.0, 0.0) });
|
||||
}
|
||||
}
|
||||
|
||||
|
||||
@@ -29,6 +29,7 @@ class ObservationKind:
|
||||
PSEUDORANGE_RATE = 23
|
||||
ECEF_VEL = 31
|
||||
ECEF_ORIENTATION_FROM_GPS = 32
|
||||
NO_ACCEL = 33
|
||||
|
||||
ROAD_FRAME_XY_SPEED = 24 # (x, y) [m/s]
|
||||
ROAD_FRAME_YAW_RATE = 25 # [rad/s]
|
||||
|
||||
@@ -28,8 +28,8 @@ std::vector<Eigen::Map<MatrixXdr>> get_vec_mapmat(std::vector<MatrixXdr>& mat_ve
|
||||
}
|
||||
|
||||
LiveKalman::LiveKalman() {
|
||||
this->dim_state = 23;
|
||||
this->dim_state_err = 22;
|
||||
this->dim_state = 26;
|
||||
this->dim_state_err = 25;
|
||||
|
||||
this->initial_x = live_initial_x;
|
||||
this->initial_P = live_initial_P_diag.asDiagonal();
|
||||
|
||||
@@ -29,6 +29,7 @@ class States():
|
||||
ODO_SCALE = slice(16, 17) # odometer scale
|
||||
ACCELERATION = slice(17, 20) # Acceleration in device frame in m/s**2
|
||||
IMU_OFFSET = slice(20, 23) # imu offset angles in radians
|
||||
ACC_BIAS = slice(23, 26)
|
||||
|
||||
# Error-state has different slices because it is an ESKF
|
||||
ECEF_POS_ERR = slice(0, 3)
|
||||
@@ -39,6 +40,7 @@ class States():
|
||||
ODO_SCALE_ERR = slice(15, 16)
|
||||
ACCELERATION_ERR = slice(16, 19)
|
||||
IMU_OFFSET_ERR = slice(19, 22)
|
||||
ACC_BIAS_ERR = slice(22, 25)
|
||||
|
||||
|
||||
class LiveKalman():
|
||||
@@ -51,6 +53,7 @@ class LiveKalman():
|
||||
0, 0, 0,
|
||||
1,
|
||||
0, 0, 0,
|
||||
0, 0, 0,
|
||||
0, 0, 0])
|
||||
|
||||
# state covariance
|
||||
@@ -60,8 +63,9 @@ class LiveKalman():
|
||||
1**2, 1**2, 1**2,
|
||||
1**2, 1**2, 1**2,
|
||||
0.02**2,
|
||||
1**2, 1**2, 1**2,
|
||||
(0.01)**2, (0.01)**2, (0.01)**2])
|
||||
100**2, 100**2, 100**2,
|
||||
0.01**2, 0.01**2, 0.01**2,
|
||||
0.01**2, 0.01**2, 0.01**2])
|
||||
|
||||
# process noise
|
||||
Q_diag = np.array([0.03**2, 0.03**2, 0.03**2,
|
||||
@@ -71,7 +75,8 @@ class LiveKalman():
|
||||
(0.005 / 100)**2, (0.005 / 100)**2, (0.005 / 100)**2,
|
||||
(0.02 / 100)**2,
|
||||
3**2, 3**2, 3**2,
|
||||
(0.05 / 60)**2, (0.05 / 60)**2, (0.05 / 60)**2])
|
||||
(0.05 / 60)**2, (0.05 / 60)**2, (0.05 / 60)**2,
|
||||
0.005**2, 0.005**2, 0.005**2])
|
||||
|
||||
obs_noise_diag = {ObservationKind.ODOMETRIC_SPEED: np.array([0.2**2]),
|
||||
ObservationKind.PHONE_GYRO: np.array([0.025**2, 0.025**2, 0.025**2]),
|
||||
@@ -79,6 +84,7 @@ class LiveKalman():
|
||||
ObservationKind.CAMERA_ODO_ROTATION: np.array([0.05**2, 0.05**2, 0.05**2]),
|
||||
ObservationKind.IMU_FRAME: np.array([0.05**2, 0.05**2, 0.05**2]),
|
||||
ObservationKind.NO_ROT: np.array([0.005**2, 0.005**2, 0.005**2]),
|
||||
ObservationKind.NO_ACCEL: np.array([0.05**2, 0.05**2, 0.05**2]),
|
||||
ObservationKind.ECEF_POS: np.array([5**2, 5**2, 5**2]),
|
||||
ObservationKind.ECEF_VEL: np.array([.5**2, .5**2, .5**2]),
|
||||
ObservationKind.ECEF_ORIENTATION_FROM_GPS: np.array([.2**2, .2**2, .2**2, .2**2])}
|
||||
@@ -100,6 +106,7 @@ class LiveKalman():
|
||||
roll_bias, pitch_bias, yaw_bias = state[States.GYRO_BIAS, :]
|
||||
acceleration = state[States.ACCELERATION, :]
|
||||
imu_angles = state[States.IMU_OFFSET, :]
|
||||
acc_bias = state[States.ACC_BIAS, :]
|
||||
|
||||
dt = sp.Symbol('dt')
|
||||
|
||||
@@ -133,6 +140,7 @@ class LiveKalman():
|
||||
omega_err = state_err[States.ANGULAR_VELOCITY_ERR, :]
|
||||
acceleration_err = state_err[States.ACCELERATION_ERR, :]
|
||||
|
||||
|
||||
# Time derivative of the state error as a function of state error and state
|
||||
quat_err_matrix = euler_rotate(quat_err[0], quat_err[1], quat_err[2])
|
||||
q_err_dot = quat_err_matrix * quat_rot * (omega + omega_err)
|
||||
@@ -183,7 +191,8 @@ class LiveKalman():
|
||||
|
||||
pos = sp.Matrix([x, y, z])
|
||||
gravity = quat_rot.T * ((EARTH_GM / ((x**2 + y**2 + z**2)**(3.0 / 2.0))) * pos)
|
||||
h_acc_sym = (gravity + acceleration)
|
||||
h_acc_sym = (gravity + acceleration + acc_bias)
|
||||
h_acc_stationary_sym = acceleration
|
||||
h_phone_rot_sym = sp.Matrix([vroll, vpitch, vyaw])
|
||||
|
||||
speed = sp.sqrt(vx**2 + vy**2 + vz**2 + 1e-6)
|
||||
@@ -205,7 +214,8 @@ class LiveKalman():
|
||||
[h_orientation_sym, ObservationKind.ECEF_ORIENTATION_FROM_GPS, None],
|
||||
[h_relative_motion, ObservationKind.CAMERA_ODO_TRANSLATION, None],
|
||||
[h_phone_rot_sym, ObservationKind.CAMERA_ODO_ROTATION, None],
|
||||
[h_imu_frame_sym, ObservationKind.IMU_FRAME, None]]
|
||||
[h_imu_frame_sym, ObservationKind.IMU_FRAME, None],
|
||||
[h_acc_stationary_sym, ObservationKind.NO_ACCEL, None]]
|
||||
|
||||
# this returns a sympy routine for the jacobian of the observation function of the local vel
|
||||
in_vec = sp.MatrixSymbol('in_vec', 6, 1) # roll, pitch, yaw, vx, vy, vz
|
||||
|
||||
@@ -1 +1 @@
|
||||
5703f591ce18bb3aebf67c0594220485f8cb3f79
|
||||
b3c61dc5f6777497fdd82fb7421a469a43efcbf1
|
||||
Reference in New Issue
Block a user