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📄 modeledpr.hpp

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            useTGD = usetgd;        };        /** Explicit constructor, taking as input default ionospheric and tropospheric         * models, ephemeris to be used, default observable and whether TGD will be         * computed or not.         *         * This constructor is meant to be used when working with GNSS data structures         * in order to set the basic parameters from the beginning.         *         * @param dIonoModel    Ionospheric model to be used by default.         * @param dTropoModel   Tropospheric model to be used by default.         * @param dObservable   Observable type to be used by default.         * @param dEphemeris    EphemerisStore object to be used by default.         * @param usetgd        Whether TGD will be used by default or not.         *         * @sa DataStructures.hpp.         */        ModeledPR(IonoModelStore& dIonoModel, TropModel& dTropoModel, EphemerisStore& dEphemeris, const TypeID& dObservable, bool usetgd = true) throw(Exception) {             InitializeValues();            setDefaultIonoModel(dIonoModel);            setDefaultTropoModel(dTropoModel);            setDefaultObservable(dObservable);            setDefaultEphemeris(dEphemeris);            useTGD = usetgd;        };        /** Explicit constructor, taking as input default ionospheric model,          * ephemeris to be used, default observable and whether TGD will be         * computed or not.         *         * This constructor is meant to be used when working with GNSS data structures         * in order to set the basic parameters from the beginning.         *         * @param dIonoModel    Ionospheric model to be used by default.         * @param dObservable   Observable type to be used by default.         * @param dEphemeris    EphemerisStore object to be used by default.         * @param usetgd        Whether TGD will be used by default or not.         *         * @sa DataStructures.hpp.         */        ModeledPR(IonoModelStore& dIonoModel, EphemerisStore& dEphemeris, const TypeID& dObservable, bool usetgd = true) throw(Exception) {             InitializeValues();            setDefaultIonoModel(dIonoModel);            pDefaultTropoModel = NULL;            setDefaultObservable(dObservable);            setDefaultEphemeris(dEphemeris);            useTGD = usetgd;        };        /** Explicit constructor, taking as input default tropospheric model,          * ephemeris to be used, default observable and whether TGD will be         * computed or not.         *         * This constructor is meant to be used when working with GNSS data structures         * in order to set the basic parameters from the beginning.         *         * @param dTropoModel   Tropospheric model to be used by default.         * @param dObservable   Observable type to be used by default.         * @param dEphemeris    EphemerisStore object to be used by default.         * @param usetgd        Whether TGD will be used by default or not.         *         * @sa DataStructures.hpp.         */        ModeledPR(TropModel& dTropoModel, EphemerisStore& dEphemeris, const TypeID& dObservable, bool usetgd = true) throw(Exception) {             InitializeValues();            pDefaultIonoModel = NULL;            setDefaultTropoModel(dTropoModel);            setDefaultObservable(dObservable);            setDefaultEphemeris(dEphemeris);            useTGD = usetgd;        };        /** Method to set an a priori position of receiver using Bancroft method.         *         * @param Tr            Time of observation         * @param Satellite     Vector of satellites in view         * @param Pseudorange   Pseudoranges measured from mobile to satellites         * @param Eph           Satellites Ephemeris         *         * @return         *  0 if OK         *  -1 if problems arose         */        virtual int Prepare(const DayTime& Tr, std::vector<SatID>& Satellite, std::vector<double>& Pseudorange, const EphemerisStore& Eph);        /** Method to set an a priori position of receiver using Bancroft method.         *         * @param Tr            Time of observation         * @param Satellite     Vector of satellites in view         * @param Pseudorange   Pseudoranges measured from mobile to satellites         * @param Eph           Satellites Ephemeris         *         * @return         *  0 if OK         *  -1 if problems arose         */        virtual int Prepare(const DayTime& Tr, const Vector<SatID>& Satellite, const Vector<double>& Pseudorange, const EphemerisStore& Eph)         {            int i;            std::vector<SatID> vSat;            std::vector<double> vPR;            // Convert from gpstk::Vector to std::vector            for (i = 0; i < (int)Satellite.size(); i++)                vSat.push_back(Satellite[i]);            for (i = 0; i < (int)Pseudorange.size(); i++)                vPR.push_back(Pseudorange[i]);            return Prepare(Tr, vSat, vPR, Eph);        };        /** Method to set an a priori position of receiver using Bancroft method. Intended to be used         * with GNSS data structures.         *         * @param time      DayTime object for this epoch         * @param data      A satTypeValueMap data structure holding the data         *         * @return         *  0 if OK         *  -1 if problems arose         */        virtual inline int Prepare(const DayTime& time, const satTypeValueMap& data)        {            int i;            std::vector<SatID> vSat;            std::vector<double> vPR;            Vector<SatID> Satellite( data.getVectorOfSatID() );            Vector<double> Pseudorange( data.getVectorOfTypeID( (*this).getDefaultObservable() ) );            // Convert from gpstk::Vector to std::vector            for (i = 0; i < (int)Satellite.size(); i++)                vSat.push_back(Satellite[i]);            for (i = 0; i < (int)Pseudorange.size(); i++)                vPR.push_back(Pseudorange[i]);            return Prepare(time, vSat, vPR, (*( (*this).getDefaultEphemeris())) );        };        /** Method to set an a priori position of receiver using Bancroft method. Intended to be used         * with GNSS data structures.         *         * @param gData         GNSS data structure to be used         *         * @return         *  0 if OK         *  -1 if problems arose         */        virtual inline int Prepare(const gnssSatTypeValue& gData)        {            return ((*this).Prepare(gData.header.epoch, gData.body));        };        /** Method to set the initial (a priori) position of receiver before          * Compute() method.         * @return         *  0 if OK         *  -1 if problems arose         */        virtual int Prepare(const double& aRx, const double& bRx, const double& cRx,             Position::CoordinateSystem s=Position::Cartesian,            GeoidModel *geoid=NULL) throw(GeometryException);        /** Method to set the initial (a priori) position of receiver before          * Compute() method.         * @return         *  0 if OK         *  -1 if problems arose         */        virtual int Prepare(const Position& RxCoordinates) throw(GeometryException);        /** Returns a satTypeValueMap object, adding the new data generated when calling a modeling object.         *         * @param time      Epoch.         * @param gData     Data object holding the data.         */        virtual satTypeValueMap& processModel(const DayTime& time, satTypeValueMap& gData) throw(Exception);        /// Method to get if the model has been prepared.        inline bool getModelPrepared() const { return modelPrepared; };        /** Method to forcefully set whether the model has been prepared.         *         * @param prepare       Boolean indicating whether the model has been prepared.         */        inline void setModelPrepared(const bool& prepare) { modelPrepared = prepare; };        /// Destructor.        virtual ~ModeledPR() throw() {};    protected:        bool modelPrepared;   }; // class ModeledPR   //@}} // namespace#endif

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