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This commit is contained in:
Marius Eggert
2022-12-13 11:51:03 +01:00
parent d33ae9ede7
commit b49d37e15a
12 changed files with 577 additions and 575 deletions
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34
mission/controller/acs/Guidance.h
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@ -21,27 +21,31 @@ class Guidance {
void getTargetParamsSafe(double sunTargetSafe[3], double satRateRef[3]);
// Function to get the target quaternion and refence rotation rate from gps position and position of the ground station
void targetQuatPtgOldVersion(ACS::SensorValues *sensorValues, acsctrl::MekfData *mekfData,
acsctrl::SusDataProcessed *susDataProcessed, timeval now, double targetQuat[4],
double refSatRate[3]);
void targetQuatPtg(ACS::SensorValues *sensorValues, acsctrl::MekfData *mekfData,
// Function to get the target quaternion and refence rotation rate from gps position and position
// of the ground station
void targetQuatPtgOldVersion(ACS::SensorValues *sensorValues, acsctrl::MekfData *mekfData,
acsctrl::SusDataProcessed *susDataProcessed, timeval now,
double targetQuat[4], double refSatRate[3]);
void targetQuatPtg(ACS::SensorValues *sensorValues, acsctrl::MekfData *mekfData,
acsctrl::SusDataProcessed *susDataProcessed, timeval now, double targetQuat[4],
double refSatRate[3]);
// Function to get the target quaternion and refence rotation rate for sun pointing after ground station
void sunQuatPtg(ACS::SensorValues* sensorValues, ACS::OutputValues *outputValues, timeval now,
double targetQuat[4], double refSatRate[3]);
// Function to get the target quaternion and refence rotation rate for sun pointing after ground
// station
void sunQuatPtg(ACS::SensorValues *sensorValues, ACS::OutputValues *outputValues, timeval now,
double targetQuat[4], double refSatRate[3]);
// Function to get the target quaternion and refence rotation rate from gps position for Nadir pointing
void quatNadirPtgOldVersion(ACS::SensorValues* sensorValues, ACS::OutputValues *outputValues, timeval now,
double targetQuat[4], double refSatRate[3]);
// Function to get the target quaternion and refence rotation rate from gps position for Nadir
// pointing
void quatNadirPtgOldVersion(ACS::SensorValues *sensorValues, ACS::OutputValues *outputValues,
timeval now, double targetQuat[4], double refSatRate[3]);
void quatNadirPtg(ACS::SensorValues* sensorValues, ACS::OutputValues *outputValues, timeval now,
double targetQuat[4], double refSatRate[3]);
void quatNadirPtg(ACS::SensorValues *sensorValues, ACS::OutputValues *outputValues, timeval now,
double targetQuat[4], double refSatRate[3]);
// Function to get the target quaternion and refence rotation rate from parameters for inertial pointing
void inertialQuatPtg(double targetQuat[4], double refSatRate[3]);
// Function to get the target quaternion and refence rotation rate from parameters for inertial
// pointing
void inertialQuatPtg(double targetQuat[4], double refSatRate[3]);
// @note: compares target Quaternion and reference quaternion, also actual satellite rate and
// desired