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AP_NavEKF2: remove instance id from EK2 external interface 

Removes passing of instance id in interfaces where -1 was the only value
ever passed in
apm_2208
Peter Barker 3 years ago committed by Andrew Tridgell
parent
c1c18331f9
commit
04a64a20fa
2 changed files with 61 additions and 99 deletions
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  1. 102
      libraries/AP_NavEKF2/AP_NavEKF2.cpp
  2. 58
      libraries/AP_NavEKF2/AP_NavEKF2.h

102
libraries/AP_NavEKF2/AP_NavEKF2.cpp
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@ -913,74 +913,59 @@ int8_t NavEKF2::getPrimaryCoreIMUIndex(void) const @@ -913,74 +913,59 @@ int8_t NavEKF2::getPrimaryCoreIMUIndex(void) const
// Write the last calculated NE position relative to the reference point (m).
// If a calculated solution is not available, use the best available data and return false
// If false returned, do not use for flight control
bool NavEKF2::getPosNE(int8_t instance, Vector2f &posNE) const
bool NavEKF2::getPosNE(Vector2f &posNE) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (!core) {
return false;
}
return core[instance].getPosNE(posNE);
return core[primary].getPosNE(posNE);
}
// Write the last calculated D position relative to the reference point (m).
// If a calculated solution is not available, use the best available data and return false
// If false returned, do not use for flight control
bool NavEKF2::getPosD(int8_t instance, float &posD) const
bool NavEKF2::getPosD(float &posD) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (!core) {
return false;
}
return core[instance].getPosD(posD);
return core[primary].getPosD(posD);
}
// return NED velocity in m/s
void NavEKF2::getVelNED(int8_t instance, Vector3f &vel) const
void NavEKF2::getVelNED(Vector3f &vel) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getVelNED(vel);
core[primary].getVelNED(vel);
}
}
// return estimate of true airspeed vector in body frame in m/s for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
// returns false if estimate is unavailable
bool NavEKF2::getAirSpdVec(int8_t instance, Vector3f &vel) const
bool NavEKF2::getAirSpdVec(Vector3f &vel) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
return core[instance].getAirSpdVec(vel);
return core[primary].getAirSpdVec(vel);
}
return false;
}
// Return the rate of change of vertical position in the down direction (dPosD/dt) in m/s
float NavEKF2::getPosDownDerivative(int8_t instance) const
float NavEKF2::getPosDownDerivative() const
{
if (instance < 0 || instance >= num_cores) instance = primary;
// return the value calculated from a complementary filter applied to the EKF height and vertical acceleration
if (core) {
return core[instance].getPosDownDerivative();
return core[primary].getPosDownDerivative();
}
return 0.0f;
}
// return body axis gyro bias estimates in rad/sec
void NavEKF2::getGyroBias(int8_t instance, Vector3f &gyroBias) const
void NavEKF2::getGyroBias(Vector3f &gyroBias) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getGyroBias(gyroBias);
}
}
// return body axis gyro scale factor error as a percentage
void NavEKF2::getGyroScaleErrorPercentage(int8_t instance, Vector3f &gyroScale) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getGyroScaleErrorPercentage(gyroScale);
core[primary].getGyroBias(gyroBias);
}
}
@ -1031,38 +1016,34 @@ void NavEKF2::getEkfControlLimits(float &ekfGndSpdLimit, float &ekfNavVelGainSca @@ -1031,38 +1016,34 @@ void NavEKF2::getEkfControlLimits(float &ekfGndSpdLimit, float &ekfNavVelGainSca
}
// return the individual Z-accel bias estimates in m/s^2
void NavEKF2::getAccelZBias(int8_t instance, float &zbias) const
void NavEKF2::getAccelZBias(float &zbias) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getAccelZBias(zbias);
core[primary].getAccelZBias(zbias);
}
}
// return the NED wind speed estimates in m/s (positive is air moving in the direction of the axis)
void NavEKF2::getWind(int8_t instance, Vector3f &wind) const
void NavEKF2::getWind(Vector3f &wind) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getWind(wind);
core[primary].getWind(wind);
}
}
// return earth magnetic field estimates in measurement units / 1000
void NavEKF2::getMagNED(int8_t instance, Vector3f &magNED) const
void NavEKF2::getMagNED(Vector3f &magNED) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getMagNED(magNED);
core[primary].getMagNED(magNED);
}
}
// return body magnetic field estimates in measurement units / 1000
void NavEKF2::getMagXYZ(int8_t instance, Vector3f &magXYZ) const
void NavEKF2::getMagXYZ(Vector3f &magXYZ) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getMagXYZ(magXYZ);
core[primary].getMagXYZ(magXYZ);
}
}
@ -1101,13 +1082,12 @@ bool NavEKF2::getLLH(struct Location &loc) const @@ -1101,13 +1082,12 @@ bool NavEKF2::getLLH(struct Location &loc) const
// An out of range instance (eg -1) returns data for the primary instance
// All NED positions calculated by the filter are relative to this location
// Returns false if the origin has not been set
bool NavEKF2::getOriginLLH(int8_t instance, struct Location &loc) const
bool NavEKF2::getOriginLLH(struct Location &loc) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (!core) {
return false;
}
return core[instance].getOriginLLH(loc);
return core[primary].getOriginLLH(loc);
}
// set the latitude and longitude and height used to set the NED origin
@ -1148,11 +1128,10 @@ bool NavEKF2::getHAGL(float &HAGL) const @@ -1148,11 +1128,10 @@ bool NavEKF2::getHAGL(float &HAGL) const
}
// return the Euler roll, pitch and yaw angle in radians for the specified instance
void NavEKF2::getEulerAngles(int8_t instance, Vector3f &eulers) const
void NavEKF2::getEulerAngles(Vector3f &eulers) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getEulerAngles(eulers);
core[primary].getEulerAngles(eulers);
}
}
@ -1176,35 +1155,31 @@ void NavEKF2::getQuaternionBodyToNED(int8_t instance, Quaternion &quat) const @@ -1176,35 +1155,31 @@ void NavEKF2::getQuaternionBodyToNED(int8_t instance, Quaternion &quat) const
}
// return the quaternions defining the rotation from NED to XYZ (autopilot) axes
void NavEKF2::getQuaternion(int8_t instance, Quaternion &quat) const
void NavEKF2::getQuaternion(Quaternion &quat) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getQuaternion(quat);
core[primary].getQuaternion(quat);
}
}
// return the innovations for the specified instance
bool NavEKF2::getInnovations(int8_t instance, Vector3f &velInnov, Vector3f &posInnov, Vector3f &magInnov, float &tasInnov, float &yawInnov) const
bool NavEKF2::getInnovations(Vector3f &velInnov, Vector3f &posInnov, Vector3f &magInnov, float &tasInnov, float &yawInnov) const
{
if (core == nullptr) {
return false;
}
if (instance < 0 || instance >= num_cores) instance = primary;
return core[instance].getInnovations(velInnov, posInnov, magInnov, tasInnov, yawInnov);
return core[primary].getInnovations(velInnov, posInnov, magInnov, tasInnov, yawInnov);
}
// return the innovation consistency test ratios for the velocity, position, magnetometer and true airspeed measurements
bool NavEKF2::getVariances(int8_t instance, float &velVar, float &posVar, float &hgtVar, Vector3f &magVar, float &tasVar, Vector2f &offset) const
bool NavEKF2::getVariances(float &velVar, float &posVar, float &hgtVar, Vector3f &magVar, float &tasVar, Vector2f &offset) const
{
if (core == nullptr) {
return false;
}
if (instance < 0 || instance >= num_cores) instance = primary;
return core[instance].getVariances(velVar, posVar, hgtVar, magVar, tasVar, offset);
return core[primary].getVariances(velVar, posVar, hgtVar, magVar, tasVar, offset);
}
// should we use the compass? This is public so it can be used for
@ -1265,11 +1240,10 @@ void NavEKF2::setTerrainHgtStable(bool val) @@ -1265,11 +1240,10 @@ void NavEKF2::setTerrainHgtStable(bool val)
6 = badly conditioned synthetic sideslip fusion
7 = filter is not initialised
*/
void NavEKF2::getFilterFaults(int8_t instance, uint16_t &faults) const
void NavEKF2::getFilterFaults(uint16_t &faults) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getFilterFaults(faults);
core[primary].getFilterFaults(faults);
} else {
faults = 0;
}
@ -1278,11 +1252,10 @@ void NavEKF2::getFilterFaults(int8_t instance, uint16_t &faults) const @@ -1278,11 +1252,10 @@ void NavEKF2::getFilterFaults(int8_t instance, uint16_t &faults) const
/*
return filter status flags
*/
void NavEKF2::getFilterStatus(int8_t instance, nav_filter_status &status) const
void NavEKF2::getFilterStatus(nav_filter_status &status) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getFilterStatus(status);
core[primary].getFilterStatus(status);
} else {
memset(&status, 0, sizeof(status));
}
@ -1291,11 +1264,10 @@ void NavEKF2::getFilterStatus(int8_t instance, nav_filter_status &status) const @@ -1291,11 +1264,10 @@ void NavEKF2::getFilterStatus(int8_t instance, nav_filter_status &status) const
/*
return filter gps quality check status
*/
void NavEKF2::getFilterGpsStatus(int8_t instance, nav_gps_status &status) const
void NavEKF2::getFilterGpsStatus(nav_gps_status &status) const
{
if (instance < 0 || instance >= num_cores) instance = primary;
if (core) {
core[instance].getFilterGpsStatus(status);
core[primary].getFilterGpsStatus(status);
} else {
memset(&status, 0, sizeof(status));
}
@ -1601,7 +1573,7 @@ void NavEKF2::writeExtNavVelData(const Vector3f &vel, float err, uint32_t timeSt @@ -1601,7 +1573,7 @@ void NavEKF2::writeExtNavVelData(const Vector3f &vel, float err, uint32_t timeSt
}
}
// get a yaw estimator instance
// get yaw estimator instance
const EKFGSF_yaw *NavEKF2::get_yawEstimator(void) const
{
if (core) {

58
libraries/AP_NavEKF2/AP_NavEKF2.h
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@ -68,40 +68,30 @@ public: @@ -68,40 +68,30 @@ public:
// return -1 if no primary core selected
int8_t getPrimaryCoreIMUIndex(void) const;
// Write the last calculated NE position relative to the reference point (m) for the specified instance.
// An out of range instance (eg -1) returns data for the primary instance
// Write the last calculated NE position relative to the reference point (m)
// If a calculated solution is not available, use the best available data and return false
// If false returned, do not use for flight control
bool getPosNE(int8_t instance, Vector2f &posNE) const;
bool getPosNE(Vector2f &posNE) const;
// Write the last calculated D position relative to the reference point (m) for the specified instance.
// An out of range instance (eg -1) returns data for the primary instance
// Write the last calculated D position relative to the reference point (m)
// If a calculated solution is not available, use the best available data and return false
// If false returned, do not use for flight control
bool getPosD(int8_t instance, float &posD) const;
bool getPosD(float &posD) const;
// return NED velocity in m/s for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
void getVelNED(int8_t instance, Vector3f &vel) const;
// return NED velocity in m/s
void getVelNED(Vector3f &vel) const;
// return estimate of true airspeed vector in body frame in m/s for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
// return estimate of true airspeed vector in body frame in m/s
// returns false if estimate is unavailable
bool getAirSpdVec(int8_t instance, Vector3f &vel) const;
bool getAirSpdVec(Vector3f &vel) const;
// Return the rate of change of vertical position in the down direction (dPosD/dt) in m/s for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
// Return the rate of change of vertical position in the down direction (dPosD/dt) in m/s
// This can be different to the z component of the EKF velocity state because it will fluctuate with height errors and corrections in the EKF
// but will always be kinematically consistent with the z component of the EKF position state
float getPosDownDerivative(int8_t instance) const;
// return body axis gyro bias estimates in rad/sec for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
void getGyroBias(int8_t instance, Vector3f &gyroBias) const;
float getPosDownDerivative() const;
// return body axis gyro scale factor error as a percentage for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
void getGyroScaleErrorPercentage(int8_t instance, Vector3f &gyroScale) const;
// return body axis gyro bias estimates in rad/sec
void getGyroBias(Vector3f &gyroBias) const;
// reset body axis gyro bias estimates
void resetGyroBias(void);
@ -119,19 +109,19 @@ public: @@ -119,19 +109,19 @@ public:
// return the Z-accel bias estimate in m/s^2 for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
void getAccelZBias(int8_t instance, float &zbias) const;
void getAccelZBias(float &zbias) const;
// return the NED wind speed estimates in m/s (positive is air moving in the direction of the axis)
// An out of range instance (eg -1) returns data for the primary instance
void getWind(int8_t instance, Vector3f &wind) const;
void getWind(Vector3f &wind) const;
// return earth magnetic field estimates in measurement units / 1000 for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
void getMagNED(int8_t instance, Vector3f &magNED) const;
void getMagNED(Vector3f &magNED) const;
// return body magnetic field estimates in measurement units / 1000 for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
void getMagXYZ(int8_t instance, Vector3f &magXYZ) const;
void getMagXYZ(Vector3f &magXYZ) const;
// Return estimated magnetometer offsets
// Return true if magnetometer offsets are valid
@ -147,7 +137,7 @@ public: @@ -147,7 +137,7 @@ public:
// An out of range instance (eg -1) returns data for the primary instance
// All NED positions calculated by the filter are relative to this location
// Returns false if the origin has not been set
bool getOriginLLH(int8_t instance, struct Location &loc) const;
bool getOriginLLH(struct Location &loc) const;
// set the latitude and longitude and height used to set the NED origin
// All NED positions calculated by the filter will be relative to this location
@ -161,7 +151,7 @@ public: @@ -161,7 +151,7 @@ public:
// return the Euler roll, pitch and yaw angle in radians for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
void getEulerAngles(int8_t instance, Vector3f &eulers) const;
void getEulerAngles(Vector3f &eulers) const;
// return the transformation matrix from XYZ (body) to NED axes
void getRotationBodyToNED(Matrix3f &mat) const;
@ -170,15 +160,15 @@ public: @@ -170,15 +160,15 @@ public:
void getQuaternionBodyToNED(int8_t instance, Quaternion &quat) const;
// return the quaternions defining the rotation from NED to autopilot axes
void getQuaternion(int8_t instance, Quaternion &quat) const;
void getQuaternion(Quaternion &quat) const;
// return the innovations for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
bool getInnovations(int8_t index, Vector3f &velInnov, Vector3f &posInnov, Vector3f &magInnov, float &tasInnov, float &yawInnov) const;
bool getInnovations(Vector3f &velInnov, Vector3f &posInnov, Vector3f &magInnov, float &tasInnov, float &yawInnov) const;
// return the innovation consistency test ratios for the specified instance
// An out of range instance (eg -1) returns data for the primary instance
bool getVariances(int8_t instance, float &velVar, float &posVar, float &hgtVar, Vector3f &magVar, float &tasVar, Vector2f &offset) const;
bool getVariances(float &velVar, float &posVar, float &hgtVar, Vector3f &magVar, float &tasVar, Vector2f &offset) const;
// should we use the compass? This is public so it can be used for
// reporting via ahrs.use_compass()
@ -211,19 +201,19 @@ public: @@ -211,19 +201,19 @@ public:
6 = badly conditioned synthetic sideslip fusion
7 = filter is not initialised
*/
void getFilterFaults(int8_t instance, uint16_t &faults) const;
void getFilterFaults(uint16_t &faults) const;
/*
return filter gps quality check status for the specified instance
An out of range instance (eg -1) returns data for the primary instance
*/
void getFilterGpsStatus(int8_t instance, nav_gps_status &faults) const;
void getFilterGpsStatus(nav_gps_status &faults) const;
/*
return filter status flags for the specified instance
An out of range instance (eg -1) returns data for the primary instance
*/
void getFilterStatus(int8_t instance, nav_filter_status &status) const;
void getFilterStatus(nav_filter_status &status) const;
// send an EKF_STATUS_REPORT message to GCS
void send_status_report(mavlink_channel_t chan) const;

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