eive/eive-obsw
13
4
Fork 0
Code Issues 4 Pull Requests 1 Releases 121 Wiki Activity

removed OutputValues

Browse Source 
amended sumbode list
inserted writes to output DataPools
This commit is contained in:
Marius Eggert
2022-11-03 10:43:27 +01:00
parent 44dda9455d
commit a13ccb43d2
24 changed files with 590 additions and 522 deletions
Download Patch File Download Diff File Expand all files Collapse all files

42
mission/controller/acs/Guidance.h
View File

@ -8,35 +8,37 @@
#ifndef GUIDANCE_H_
#define GUIDANCE_H_
#include "AcsParameters.h"
#include "SensorValues.h"
#include "OutputValues.h"
#include <time.h>
#include "../controllerdefinitions/AcsCtrlDefinitions.h"
#include "AcsParameters.h"
#include "SensorValues.h"
class Guidance {
public:
Guidance(AcsParameters *acsParameters_);
virtual ~Guidance();
public:
Guidance(AcsParameters *acsParameters_);
virtual ~Guidance();
void getTargetParamsSafe(double sunTargetSafe[3], double satRateRef[3]);
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 targetQuatPtg(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 and position
// of the ground station
void targetQuatPtg(ACS::SensorValues *sensorValues, acsctrl::MekfData *mekfData,
acsctrl::SusDataProcessed *susDataProcessed, timeval now, double targetQuat[4],
double refSatRate[3]);
// @note: compares target Quaternion and reference quaternion, also actual satellite rate and desired
void comparePtg( double targetQuat[4], ACS::OutputValues *outputValues, double refSatRate[3], double quatError[3], double deltaRate[3] );
// @note: compares target Quaternion and reference quaternion, also actual satellite rate and
// desired
void comparePtg(double targetQuat[4], acsctrl::MekfData *mekfData, double refSatRate[3],
double quatErrorComplete[4], double quatError[3], double deltaRate[3]);
// @note: will give back the pseudoinverse matrix for the reaction wheel depending on the valid reation wheel
// maybe can be done in "commanding.h"
void getDistributionMatrixRw(ACS::SensorValues* sensorValues, double *rwPseudoInv);
// @note: will give back the pseudoinverse matrix for the reaction wheel depending on the valid
// reation wheel maybe can be done in "commanding.h"
void getDistributionMatrixRw(ACS::SensorValues *sensorValues, double *rwPseudoInv);
private:
AcsParameters acsParameters;
bool strBlindAvoidFlag = false;
private:
AcsParameters acsParameters;
bool strBlindAvoidFlag = false;
};
#endif /* ACS_GUIDANCE_H_ */