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/*
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* MultiplicativeKalmanFilter.h
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*
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* Created on: 4 Feb 2022
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* Author: Robin Marquardt
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*
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* @brief: This class handles the calculation of an estimated quaternion and the gyro bias by
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* means of the spacecraft attitude sensors
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*
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* @note: A description of the used algorithms can be found in the bachelor thesis of Robin
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* Marquardt
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* https://eive-cloud.irs.uni-stuttgart.de/index.php/apps/files/?dir=/EIVE_Studenten/Marquardt_Robin&openfile=500811
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*/
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#ifndef MULTIPLICATIVEKALMANFILTER_H_
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#define MULTIPLICATIVEKALMANFILTER_H_
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#include "eive/resultClassIds.h"
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class MultiplicativeKalmanFilter {
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/* @brief: This class handles the calculation of an estimated quaternion and the gyro bias by
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* means of the spacecraft attitude sensors
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*
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* @note: A description of the used algorithms can be found in the bachelor thesis of Robin
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* Marquardt
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* https://eive-cloud.irs.uni-stuttgart.de/index.php/apps/files/?dir=/EIVE_Studenten/Marquardt_Robin&openfile=500811
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*/
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public:
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/* @brief: Constructor
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* @param: acsParameters_ Pointer to object which defines the ACS configuration parameters
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