mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-14 04:23:35 +08:00
EKF: Add support auxiliary velocity observation
This enables the EKF to use an additional NE velocity measurement. This can be used to improve position hold stability when landing using a beacon system for positioning by fusing the beacon velocity estimates.
This commit is contained in:
@@ -156,6 +156,12 @@ struct dragSample {
|
||||
uint64_t time_us; ///< timestamp of the measurement (uSec)
|
||||
};
|
||||
|
||||
struct auxVelSample {
|
||||
Vector2f velNE; ///< measured NE velocity relative to the local origin (m/sec)
|
||||
Vector2f velVarNE; ///< estimated error variance of the NE velocity (m/sec)**2
|
||||
uint64_t time_us; ///< timestamp of the measurement (uSec)
|
||||
};
|
||||
|
||||
// Integer definitions for vdist_sensor_type
|
||||
#define VDIST_SENSOR_BARO 0 ///< Use baro height
|
||||
#define VDIST_SENSOR_GPS 1 ///< Use GPS height
|
||||
@@ -210,6 +216,7 @@ struct parameters {
|
||||
float flow_delay_ms{5.0f}; ///< optical flow measurement delay relative to the IMU (mSec) - this is to the middle of the optical flow integration interval
|
||||
float range_delay_ms{5.0f}; ///< range finder measurement delay relative to the IMU (mSec)
|
||||
float ev_delay_ms{100.0f}; ///< off-board vision measurement delay relative to the IMU (mSec)
|
||||
float auxvel_delay_ms{0.0f}; ///< auxiliary velocity measurement delay relative to the IMU (mSec)
|
||||
|
||||
// input noise
|
||||
float gyro_noise{1.5e-2f}; ///< IMU angular rate noise used for covariance prediction (rad/sec)
|
||||
@@ -326,6 +333,9 @@ struct parameters {
|
||||
float vert_innov_test_lim{4.5f}; ///< Number of standard deviations allowed before the combined vertical velocity and position test is declared as failed
|
||||
int bad_acc_reset_delay_us{500000}; ///< Continuous time that the vertical position and velocity innovation test must fail before the states are reset (uSec)
|
||||
|
||||
// auxilliary velocity fusion
|
||||
float auxvel_noise{0.5f}; ///< minimum observation noise, uses reported noise if greater (m/s)
|
||||
float auxvel_gate{5.0f}; ///< velocity fusion innovation consistency gate size (STD)
|
||||
};
|
||||
|
||||
struct stateSample {
|
||||
|
||||
+25
-1
@@ -130,9 +130,12 @@ void Ekf::controlFusionModes()
|
||||
// in a single function using sensor data from multiple sources (GPS, baro, range finder, etc)
|
||||
controlVelPosFusion();
|
||||
|
||||
// Additional data from an external vision sensor can also be fused.
|
||||
// Additional data from an external vision pose estimator can be fused.
|
||||
controlExternalVisionFusion();
|
||||
|
||||
// Additional NE velocity data from an auxiliary sensor can be fused
|
||||
controlAuxVelFusion();
|
||||
|
||||
// report dead reckoning if we are no longer fusing measurements that directly constrain velocity drift
|
||||
_is_dead_reckoning = (_time_last_imu - _time_last_pos_fuse > _params.no_aid_timeout_max)
|
||||
&& (_time_last_imu - _time_last_delpos_fuse > _params.no_aid_timeout_max)
|
||||
@@ -522,13 +525,17 @@ void Ekf::controlGpsFusion()
|
||||
float lower_limit = fmaxf(_params.gps_pos_noise, 0.01f);
|
||||
float upper_limit = fmaxf(_params.pos_noaid_noise, lower_limit);
|
||||
_posObsNoiseNE = math::constrain(_gps_sample_delayed.hacc, lower_limit, upper_limit);
|
||||
_velObsVarNE(1) = _velObsVarNE(0) = sq(fmaxf(_params.gps_vel_noise, 0.01f));
|
||||
|
||||
// calculate innovations
|
||||
_vel_pos_innov[0] = _state.vel(0) - _gps_sample_delayed.vel(0);
|
||||
_vel_pos_innov[1] = _state.vel(1) - _gps_sample_delayed.vel(1);
|
||||
_vel_pos_innov[3] = _state.pos(0) - _gps_sample_delayed.pos(0);
|
||||
_vel_pos_innov[4] = _state.pos(1) - _gps_sample_delayed.pos(1);
|
||||
|
||||
// set innovation gate size
|
||||
_posInnovGateNE = fmaxf(_params.posNE_innov_gate, 1.0f);
|
||||
_hvelInnovGate = fmaxf(_params.vel_innov_gate, 1.0f);
|
||||
}
|
||||
|
||||
} else if (_control_status.flags.gps && (_time_last_imu - _time_last_gps > (uint64_t)10e6)) {
|
||||
@@ -1355,3 +1362,20 @@ void Ekf::controlVelPosFusion()
|
||||
|
||||
}
|
||||
}
|
||||
|
||||
void Ekf::controlAuxVelFusion()
|
||||
{
|
||||
bool data_ready = _auxvel_buffer.pop_first_older_than(_imu_sample_delayed.time_us, &_auxvel_sample_delayed);
|
||||
bool primary_aiding = _control_status.flags.gps || _control_status.flags.ev_pos || _control_status.flags.opt_flow;
|
||||
|
||||
if (data_ready && primary_aiding) {
|
||||
_fuse_vert_vel = _fuse_pos = _fuse_height = false;
|
||||
_fuse_hor_vel = true;
|
||||
_vel_pos_innov[0] = _state.vel(0) - _auxvel_sample_delayed.velNE(0);
|
||||
_vel_pos_innov[1] = _state.vel(1) - _auxvel_sample_delayed.velNE(1);
|
||||
_velObsVarNE = _auxvel_sample_delayed.velVarNE;
|
||||
_hvelInnovGate = _params.auxvel_gate;
|
||||
fuseVelPosHeight();
|
||||
_fuse_hor_vel = _fuse_vert_vel = _fuse_pos = _fuse_height = false;
|
||||
}
|
||||
}
|
||||
|
||||
@@ -264,6 +264,9 @@ private:
|
||||
float _posObsNoiseNE; ///< 1-STD observtion noise used for the fusion of NE position data (m)
|
||||
float _posInnovGateNE; ///< Number of standard deviations used for the NE position fusion innovation consistency check
|
||||
|
||||
Vector2f _velObsVarNE; ///< 1-STD observation noise variance used for the fusion of NE velocity data (m/sec)**2
|
||||
float _hvelInnovGate; ///< Number of standard deviations used for the horizontal velocity fusion innovation consistency check
|
||||
|
||||
// variables used when position data is being fused using a relative position odometry model
|
||||
bool _fuse_hpos_as_odom{false}; ///< true when the NE position data is being fused using an odometry assumption
|
||||
Vector3f _pos_meas_prev; ///< previous value of NED position measurement fused using odometry assumption (m)
|
||||
@@ -561,6 +564,9 @@ private:
|
||||
// control fusion of velocity and position observations
|
||||
void controlVelPosFusion();
|
||||
|
||||
// control fusion of auxiliary velocity observations
|
||||
void controlAuxVelFusion();
|
||||
|
||||
// control for height sensor timeouts, sensor changes and state resets
|
||||
void controlHeightSensorTimeouts();
|
||||
|
||||
|
||||
@@ -442,6 +442,38 @@ void EstimatorInterface::setExtVisionData(uint64_t time_usec, ext_vision_message
|
||||
}
|
||||
}
|
||||
|
||||
void EstimatorInterface::setAuxVelData(uint64_t time_usec, float (&data)[2], float (&variance)[2])
|
||||
{
|
||||
if (!_initialised || _auxvel_buffer_fail) {
|
||||
return;
|
||||
}
|
||||
|
||||
// Allocate the required buffer size if not previously done
|
||||
// Do not retry if allocation has failed previously
|
||||
if (_auxvel_buffer.get_length() < _obs_buffer_length) {
|
||||
_auxvel_buffer_fail = !_auxvel_buffer.allocate(_obs_buffer_length);
|
||||
if (_auxvel_buffer_fail) {
|
||||
ECL_ERR("EKF aux vel buffer allocation failed");
|
||||
return;
|
||||
}
|
||||
}
|
||||
|
||||
// limit data rate to prevent data being lost
|
||||
if (time_usec - _time_last_auxvel > _min_obs_interval_us) {
|
||||
|
||||
auxVelSample auxvel_sample_new;
|
||||
auxvel_sample_new.time_us = time_usec - _params.auxvel_delay_ms * 1000;
|
||||
|
||||
auxvel_sample_new.time_us -= FILTER_UPDATE_PERIOD_MS * 1000 / 2;
|
||||
_time_last_auxvel = time_usec;
|
||||
|
||||
auxvel_sample_new.velNE = Vector2f(data);
|
||||
auxvel_sample_new.velVarNE = Vector2f(variance);
|
||||
|
||||
_auxvel_buffer.push(auxvel_sample_new);
|
||||
}
|
||||
}
|
||||
|
||||
bool EstimatorInterface::initialise_interface(uint64_t timestamp)
|
||||
{
|
||||
// find the maximum time delay the buffers are required to handle
|
||||
@@ -450,8 +482,9 @@ bool EstimatorInterface::initialise_interface(uint64_t timestamp)
|
||||
math::max(_params.gps_delay_ms,
|
||||
math::max(_params.flow_delay_ms,
|
||||
math::max(_params.ev_delay_ms,
|
||||
math::max(_params.min_delay_ms,
|
||||
math::max(_params.airspeed_delay_ms, _params.baro_delay_ms)))))));
|
||||
math::max(_params.auxvel_delay_ms,
|
||||
math::max(_params.min_delay_ms,
|
||||
math::max(_params.airspeed_delay_ms, _params.baro_delay_ms))))))));
|
||||
|
||||
// calculate the IMU buffer length required to accomodate the maximum delay with some allowance for jitter
|
||||
_imu_buffer_length = (max_time_delay_ms / FILTER_UPDATE_PERIOD_MS) + 1;
|
||||
@@ -511,6 +544,7 @@ void EstimatorInterface::unallocate_buffers()
|
||||
_output_buffer.unallocate();
|
||||
_output_vert_buffer.unallocate();
|
||||
_drag_buffer.unallocate();
|
||||
_auxvel_buffer.unallocate();
|
||||
|
||||
}
|
||||
|
||||
|
||||
@@ -185,6 +185,9 @@ public:
|
||||
// set external vision position and attitude data
|
||||
void setExtVisionData(uint64_t time_usec, ext_vision_message *evdata);
|
||||
|
||||
// set auxiliary velocity data
|
||||
void setAuxVelData(uint64_t time_usec, float (&data)[2], float (&variance)[2]);
|
||||
|
||||
// return a address to the parameters struct
|
||||
// in order to give access to the application
|
||||
parameters *getParamHandle() {return &_params;}
|
||||
@@ -402,6 +405,7 @@ protected:
|
||||
extVisionSample _ev_sample_delayed{};
|
||||
dragSample _drag_sample_delayed{};
|
||||
dragSample _drag_down_sampled{}; // down sampled drag specific force data (filter prediction rate -> observation rate)
|
||||
auxVelSample _auxvel_sample_delayed{};
|
||||
|
||||
// Used by the multi-rotor specific drag force fusion
|
||||
uint8_t _drag_sample_count{0}; // number of drag specific force samples assumulated at the filter prediction rate
|
||||
@@ -463,6 +467,7 @@ protected:
|
||||
RingBuffer<outputSample> _output_buffer;
|
||||
RingBuffer<outputVert> _output_vert_buffer;
|
||||
RingBuffer<dragSample> _drag_buffer;
|
||||
RingBuffer<auxVelSample> _auxvel_buffer;
|
||||
|
||||
// observation buffer final allocation failed
|
||||
bool _gps_buffer_fail{false};
|
||||
@@ -473,6 +478,7 @@ protected:
|
||||
bool _flow_buffer_fail{false};
|
||||
bool _ev_buffer_fail{false};
|
||||
bool _drag_buffer_fail{false};
|
||||
bool _auxvel_buffer_fail{false};
|
||||
|
||||
uint64_t _time_last_imu{0}; // timestamp of last imu sample in microseconds
|
||||
uint64_t _time_last_gps{0}; // timestamp of last gps measurement in microseconds
|
||||
@@ -483,6 +489,7 @@ protected:
|
||||
uint64_t _time_last_ext_vision{0}; // timestamp of last external vision measurement in microseconds
|
||||
uint64_t _time_last_optflow{0};
|
||||
uint64_t _time_last_gnd_effect_on{0}; //last time the baro ground effect compensation was turned on externally (uSec)
|
||||
uint64_t _time_last_auxvel{0};
|
||||
|
||||
fault_status_u _fault_status{};
|
||||
|
||||
|
||||
+6
-11
@@ -54,18 +54,13 @@ void Ekf::fuseVelPosHeight()
|
||||
|
||||
// calculate innovations, innovations gate sizes and observation variances
|
||||
if (_fuse_hor_vel) {
|
||||
// enable fusion for NE velocity axes
|
||||
fuse_map[0] = fuse_map[1] = true;
|
||||
// horizontal velocity innovations
|
||||
_vel_pos_innov[0] = _state.vel(0) - _gps_sample_delayed.vel(0);
|
||||
_vel_pos_innov[1] = _state.vel(1) - _gps_sample_delayed.vel(1);
|
||||
// observation variance - use receiver reported accuracy with parameter setting the minimum value
|
||||
R[0] = fmaxf(_params.gps_vel_noise, 0.01f);
|
||||
R[0] = fmaxf(R[0], _gps_sample_delayed.sacc);
|
||||
R[0] = R[0] * R[0];
|
||||
R[1] = R[0];
|
||||
// innovation gate sizes
|
||||
gate_size[0] = fmaxf(_params.vel_innov_gate, 1.0f);
|
||||
gate_size[1] = gate_size[0];
|
||||
|
||||
// Set observation noise variance and innovation consistency check gate size for the NE position observations
|
||||
R[0] = _velObsVarNE(0);
|
||||
R[1] = _velObsVarNE(1);
|
||||
gate_size[1] = gate_size[0] = _hvelInnovGate;
|
||||
}
|
||||
|
||||
if (_fuse_vert_vel) {
|
||||
|
||||
Reference in New Issue
Block a user