54 lines
1.4 KiB
C
54 lines
1.4 KiB
C
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#pragma once
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///
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/// <20><><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ǹ<EFBFBD><C7B9><EFBFBD>
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///
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//#define EIGEN_USE_MKL_ALL
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//#define EIGEN_VECTORIZE_SSE4_2
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//#include <mkl.h>
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// <20><><EFBFBD>ط<EFBFBD><D8B7><EFBFBD>
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#include "baseTool.h"
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#include <iostream>
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#include <Eigen/Core>
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#include <Eigen/Dense>
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#include <time.h>
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//#include <mkl.h>
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//#include <armadillo>
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using namespace std;
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using namespace Eigen;
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//using namespace arma;
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/// <summary>
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/// <20><><EFBFBD><EFBFBD>ʽ<EFBFBD><CABD><EFBFBD><EFBFBD>ģ<EFBFBD><C4A3>
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/// </summary>
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class OrbitPoly {
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public:
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//OrbitPoly(std::string orbitModelPath);
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OrbitPoly();
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OrbitPoly(int polynum, Eigen::MatrixX<double> polySatellitePara, double SatelliteModelStartTime);
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~OrbitPoly();
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Eigen::MatrixX<double> SatelliteSpacePoint(Eigen::MatrixX<double> satellitetime);
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Eigen::MatrixX<double> SatelliteSpacePoint(long double satellitetime);
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public:
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int polynum;
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Eigen::MatrixX<double> polySatellitePara;
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double SatelliteModelStartTime;
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};
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/// <summary>
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/// <20><>ȡָ<C8A1><D6B8>ʱ<EFBFBD>̵<EFBFBD><CCB5><EFBFBD><EFBFBD>ǹ<EFBFBD><C7B9><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
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/// </summary>
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/// <param name="satellitetime"><3E><><EFBFBD><EFBFBD>ʱ<EFBFBD><CAB1></param>
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/// <param name="SatelliteModelStartTime">ģ<><C4A3><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ʱ<EFBFBD><CAB1></param>
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/// <param name="polySatellitePara">ģ<>Ͳ<EFBFBD><CDB2><EFBFBD>[x1,y1,z1,vx1,vy1,vz1; x2,y2,z2,vx2,vy2,vz2; ..... ]</param>
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/// <param name="polynum">ģ<>Ͳ<EFBFBD><CDB2><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD></param>
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/// <returns><3E><><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD></returns>
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Eigen::MatrixX<double> SatelliteSpacePoints(Eigen::MatrixX<double> &satellitetime, double SatelliteModelStartTime, Eigen::MatrixX<double>& polySatellitePara, int polynum = 4);
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