GLONASSEphemeris.hpp

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// This file is part of INSTINCT, the INS Toolkit for Integrated
// Navigation Concepts and Training by the Institute of Navigation of
// the University of Stuttgart, Germany.
//
// This Source Code Form is subject to the terms of the Mozilla Public
// License, v. 2.0. If a copy of the MPL was not distributed with this
// file, You can obtain one at https://mozilla.org/MPL/2.0/.
 
 
#pragma once
 
#include <bitset>
 
#include "Navigation/GNSS/Satellite/internal/SatNavData.hpp"
 
namespace NAV
{
 
class GLONASSEphemeris final : public SatNavData
{
  public:
    // #######################################################################################################
    //                                                Members
    // #######################################################################################################
 
    const double tau_c;
 
    const InsTime toc;
    const double tau_n;
    const double gamma_n;
    const bool health;
    const Eigen::Vector3d PZ90_pos;
    const Eigen::Vector3d PZ90_vel;
    const Eigen::Vector3d PZ90_accelLuniSolar;
    const int8_t frequencyNumber;
 
    // #######################################################################################################
    //                                               Functions
    // #######################################################################################################
 
    GLONASSEphemeris(const InsTime& toc, double tau_c,
                     double tau_n, double gamma_n, bool health,
                     Eigen::Vector3d pos, Eigen::Vector3d vel, Eigen::Vector3d accelLuniSolar,
                     int8_t frequencyNumber);
 
#ifdef TESTING
    GLONASSEphemeris(int32_t year, int32_t month, int32_t day, int32_t hour, int32_t minute, double second,
                     double m_tau_n, double gamma_n, double messageFrameTime,
                     double satPos_x, double satVel_x, double satAccel_x, double health,
                     double satPos_y, double satVel_y, double satAccel_y, double frequencyNumber,
                     double satPos_z, double satVel_z, double satAccel_z, double ageOfOperationInfo,
                     double statusFlags = 0.0, double L1L2groupDelayDifference = 0.0, double URAI = 0.0, double healthFlags = 0.0,
                     double tau_c = 0.0);
#endif
 
    ~GLONASSEphemeris() final = default;
    GLONASSEphemeris(const GLONASSEphemeris&) = default;
    GLONASSEphemeris(GLONASSEphemeris&&) = default;
    GLONASSEphemeris& operator=(const GLONASSEphemeris&) = delete;
    GLONASSEphemeris& operator=(GLONASSEphemeris&&) = delete;
 
    [[nodiscard]] double calcSatellitePositionVariance() const final;
 
    [[nodiscard]] Corrections calcClockCorrections(const InsTime& recvTime, double dist, const Frequency& freq) const final;
 
    [[nodiscard]] bool isHealthy() const final;
 
  private:
    static constexpr double _h = 60.0;
 
    [[nodiscard]] PosVelAccel calcSatelliteData(const InsTime& transTime, Orbit::Calc calc) const final;
};
 
} // namespace NAV