Marius Eggert
5f17f365e3
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126 lines
4.0 KiB
C++
126 lines
4.0 KiB
C++
/*
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* Igrf13Model.cpp
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*
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* Created on: 10 Mar 2022
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* Author: Robin Marquardt
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*/
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#include "Igrf13Model.h"
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#include "util/MathOperations.h"
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#include <math.h>
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#include <stdint.h>
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#include <string.h>
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//#include <time.h>
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#include <fsfw/globalfunctions/constants.h>
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#include <fsfw/globalfunctions/math/MatrixOperations.h>
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#include <fsfw/globalfunctions/math/QuaternionOperations.h>
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#include <fsfw/globalfunctions/math/VectorOperations.h>
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Igrf13Model::Igrf13Model(){
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}
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Igrf13Model::~Igrf13Model(){
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}
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void Igrf13Model::magFieldComp(const double longitude, const double gcLatitude,
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const double altitude, timeval timeOfMagMeasurement, double* magFieldModelInertial) {
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double phi = longitude, theta = gcLatitude; //geocentric
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/* Here is the co-latitude needed*/
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theta -= 90*Math::PI/180;
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theta *= (-1);
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double rE = 6371200.0; // radius earth [m]
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/* Predefine recursive associated Legendre polynomials */
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double P11 = 1;
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double P10 = P11; //P10 = P(n-1,m-0)
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double dP11 = 0; //derivative
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double dP10 = dP11; //derivative
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double P2 = 0, dP2 = 0, P20 = 0, dP20 = 0, K = 0;
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for (int m = 0; m <= igrfOrder; m++) {
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for (int n = 1; n <= igrfOrder; n++) {
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if (m <= n) {
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/* Calculation of Legendre Polynoms (normalised) */
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if (n == m) {
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P2 = sin(theta) * P11;
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dP2 = sin(theta) * dP11 - cos(theta) * P11;
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P11 = P2;
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P10 = P11;
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P20 = 0;
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dP11 = dP2;
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dP10 = dP11;
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dP20 = 0;
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} else if (n == 1) {
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P2 = cos(theta) * P10;
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dP2 = cos(theta) * dP10 - sin(theta) * P10;
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P20 = P10;
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P10 = P2;
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dP20 = dP10;
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dP10 = dP2;
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} else {
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K = (pow((n - 1), 2) - pow(m, 2))
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/ ((2 * n - 1) * (2 * n - 3));
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P2 = cos(theta) * P10 - K * P20;
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dP2 = cos(theta) * dP10 - sin(theta) * P10 - K * dP20;
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P20 = P10;
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P10 = P2;
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dP20 = dP10;
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dP10 = dP2;
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}
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/* gradient of scalar potential towards radius */
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magFieldModel[0]+=pow(rE/(altitude+rE),(n+2))*(n+1)*
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((updatedG[m][n-1]*cos(m*phi) + updatedH[m][n-1]*sin(m*phi))*P2);
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/* gradient of scalar potential towards phi */
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magFieldModel[1]+=pow(rE/(altitude+rE),(n+2))*
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((updatedG[m][n-1]*cos(m*phi) + updatedH[m][n-1]*sin(m*phi))*dP2);
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/* gradient of scalar potential towards theta */
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magFieldModel[2]+=pow(rE/(altitude+rE),(n+2))*
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((-updatedG[m][n-1]*sin(m*phi) + updatedH[m][n-1]*cos(m*phi))*P2*m);
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}
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}
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}
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magFieldModel[1] *= -1;
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magFieldModel[2] *= (-1 / sin(theta));
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/* Next step: transform into inertial KOS (IJK)*/
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//Julean Centuries
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double JD2000Floor = 0;
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double JD2000 = MathOperations<double>::convertUnixToJD2000(timeOfMagMeasurement);
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JD2000Floor = floor(JD2000);
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double JC2000 = JD2000Floor / 36525;
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double gst = 100.4606184 + 36000.77005361 * JC2000 + 0.00038793 * pow(JC2000,2)
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- 0.000000026 * pow(JC2000,3); //greenwich sidereal time
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gst *= PI/180; //convert to radians
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double sec = (JD2000 - JD2000Floor) * 86400; // Seconds on this day (Universal time) // FROM GPS ?
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double omega0 = 0.00007292115; // mean angular velocity earth [rad/s]
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gst +=omega0 * sec;
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double lst = gst + longitude; //local sidereal time [rad]
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magFieldModelInertial[0] = magFieldModel[0] * cos(theta) + magFieldModel[1] * sin(theta)*cos(lst) - magFieldModel[1] * sin(lst);
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magFieldModelInertial[1] = magFieldModel[0] * cos(theta) + magFieldModel[1] * sin(theta)*sin(lst) + magFieldModel[1] * cos(lst);
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magFieldModelInertial[2] = magFieldModel[0] * sin(theta) + magFieldModel[1] * cos(lst);
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double normVecMagFieldInert[3] = {0,0,0};
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VectorOperations<double>::normalize(magFieldModelInertial, normVecMagFieldInert, 3);
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}
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void Igrf13Model::updateCoeffGH(timeval timeOfMagMeasurement){
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double JD2000Igrf = (2458850.0-2451545); //Begin of IGRF-13 (2020-01-01,00:00:00) in JD2000
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double JD2000 = MathOperations<double>::convertUnixToJD2000(timeOfMagMeasurement);
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double days = ceil(JD2000-JD2000Igrf);
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for(int i = 0;i <= igrfOrder; i++){
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for(int j = 0;j <= (igrfOrder-1); j++){
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updatedG[i][j] = coeffG[i][j] + svG[i][j] * (days/365);
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updatedH[i][j] = coeffH[i][j] + svH[i][j] * (days/365);
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}
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}
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}
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