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RasterProcessTool/Toolbox/SimulationSARTool/SimulationSAR/SatelliteOribtModel.h

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合并仿真、成像、影像合并的代码
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#pragma once
/*****************************************************************//**
* \file SatelliteOribtModel.h
* \brief <EFBFBD><EFBFBD><EFBFBD><EFBFBD>ģ<EFBFBD><EFBFBD>
*
* \author <EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
* \date October 2024
*********************************************************************/
#include "LogInfoCls.h"
#include "BaseConstVariable.h"
#include "SARSatelliteSimulationAbstractCls.h"
#include <vector>
#include <memory>
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#include <QFile>
#include <QXmlStreamWriter>
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/// <summary>
/// <20><><EFBFBD><EFBFBD>ʽ<EFBFBD><CABD><EFBFBD><EFBFBD>ģ<EFBFBD><C4A3>
/// </summary>
class PolyfitSatelliteOribtModel:public AbstractSatelliteOribtModel
{
public:
PolyfitSatelliteOribtModel();
~PolyfitSatelliteOribtModel() override;
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void saveToXml(const QString& filePath) ;
bool loadFromXml(const QString& filePath);
void readVector(QXmlStreamReader& xmlReader, const QString& name, std::vector<double>& vec);
void writeVector(QXmlStreamWriter& xmlWriter, const QString& name, const std::vector<double>& vec);
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public:
QString getSatelliteOribtModelParamsString();
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public: // <20><><EFBFBD>ǹ<EFBFBD><C7B9><EFBFBD><EFBFBD>ڵ<EFBFBD>
virtual SatelliteOribtNode getSatelliteOribtNode(double& timeFromStartTime, bool& antAzAngleFlag) override; // <20><>ȡ<EFBFBD><C8A1><EFBFBD><EFBFBD><EFBFBD>ڵ<EFBFBD>
virtual ErrorCode getSatelliteOribtNode(double& timeFromStartTime, SatelliteOribtNode& node, bool& antAzAngleFlag) override; // <20><>ȡ<EFBFBD><C8A1><EFBFBD><EFBFBD><EFBFBD>ڵ<EFBFBD>
virtual ErrorCode getSatelliteAntDirectNormal(SatelliteOribtNode& Rs, Vector3D& Rt, SatelliteAntDirect& antNode); // <20><><EFBFBD><EFBFBD>Ŀ<EFBFBD><C4BF><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>߷<EFBFBD><DFB7><EFBFBD>ͼ<EFBFBD>е<EFBFBD>λ<EFBFBD><CEBB>
public: // <20><><EFBFBD>ǹ<EFBFBD><C7B9><EFBFBD>ģ<EFBFBD>͵IJο<C4B2>ʱ<EFBFBD><CAB1><EFBFBD>ڵ<EFBFBD>
virtual void setSatelliteOribtStartTime(long double oribtStartTime) override;// <20><><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ģ<EFBFBD>Ͳο<CDB2>ʱ<EFBFBD><CAB1>
virtual long double getSatelliteOribtStartTime() override;// <20><>ȡ<EFBFBD><C8A1><EFBFBD><EFBFBD>ģ<EFBFBD>Ͳο<CDB2>ʱ<EFBFBD><CAB1>
public: // <20><><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ز<EFBFBD><D8B2><EFBFBD>
virtual void setbeamAngle(double beamAngle, bool RightLook) override;// <20><><EFBFBD>ò<EFBFBD>λ<EFBFBD><CEBB>
public: // <20><><EFBFBD>߰ڶ<DFB0><DAB6><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ز<EFBFBD><D8B2><EFBFBD>
virtual void setAzAngleRange(double cycletime, double minAzAngle, double maxAzAngle, double referenceAzAngle, double referenceTimeFromStartTime) override;//<2F><>λ<EFBFBD>DZ任ѭ<E4BBBB><D1AD>ʱ<EFBFBD><CAB1> ;<3B><>λ<EFBFBD>DZ任<C7B1><E4BBBB>Χ<EFBFBD><CEA7> <20>ض<EFBFBD>ʱ<EFBFBD><CAB1><EFBFBD>ķ<EFBFBD>λ<EFBFBD>ǣ<EFBFBD><C7A3><EFBFBD><EFBFBD>ڼ<EFBFBD><DABC>㷽λ<E3B7BD>DZ仯<C7B1><E4BBAF><EFBFBD><EFBFBD>
virtual double getAzAngleInCurrentTimeFromStartTime(double& currentTime) override;// <20><>ȡ<EFBFBD><C8A1>ǰʱ<C7B0><CAB1><EFBFBD><EFBFBD> <20><><EFBFBD>߰ڶ<DFB0><DAB6><EFBFBD>
virtual ErrorCode getAzAngleInCurrentTimeFromStartTime(double& currentTime, double& AzAngle);// <20><>ȡ<EFBFBD><C8A1>ǰʱ<C7B0><CAB1><EFBFBD><EFBFBD> <20><><EFBFBD>߰ڶ<DFB0><DAB6><EFBFBD>
public: // <20><><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ԭʼ<D4AD><CABC><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>µ<EFBFBD><C2B5><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ϵ<EFBFBD>ĵ<EFBFBD><C4B5><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>Ȼ<EFBFBD><C8BB><EFBFBD><EFBFBD>-Z <20><>Ϊ <20><><EFBFBD><EFBFBD>ָ<EFBFBD><D6B8><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
virtual void setAntnnaAxisX(double X, double Y, double Z) override; // <20><><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>X<EFBFBD><58>ָ<EFBFBD><D6B8>
virtual void setAntnnaAxisY(double X, double Y, double Z) override; // <20><><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>X<EFBFBD><58>ָ<EFBFBD><D6B8>
virtual void setAntnnaAxisZ(double X, double Y, double Z) override; // <20><><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>X<EFBFBD><58>ָ<EFBFBD><D6B8>
virtual ErrorCode getAntnnaDirection(SatelliteOribtNode& node) override; // <20><>ȡ<EFBFBD><C8A1><EFBFBD><EFBFBD>ָ<EFBFBD><D6B8><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
为工具增加界面
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virtual ErrorCode getZeroDopplerAntDirect(SatelliteOribtNode& node) override;
合并仿真、成像、影像合并的代码
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private: // <20><><EFBFBD><EFBFBD>
同步轨道模型的修改
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合并仿真、成像、影像合并的代码
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double beamAngle; // <20><>λ<EFBFBD><CEBB>
bool RightLook; // <20><><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
double cycletime; // <20><>λ<EFBFBD>DZ任ѭ<E4BBBB><D1AD>ʱ<EFBFBD><CAB1>
double minAzAngle; // <20><>λ<EFBFBD>DZ任<C7B1><E4BBBB>Χ
double maxAzAngle; // <20><>λ<EFBFBD>DZ任<C7B1><E4BBBB>Χ
double referenceAzAngle; // <20>ض<EFBFBD>ʱ<EFBFBD><CAB1><EFBFBD>ķ<EFBFBD>λ<EFBFBD>ǣ<EFBFBD><C7A3><EFBFBD><EFBFBD>ڼ<EFBFBD><DABC>㷽λ<E3B7BD>DZ仯<C7B1><E4BBAF><EFBFBD><EFBFBD>
double referenceTimeFromStartTime; // <20>ض<EFBFBD>ʱ<EFBFBD><CAB1><EFBFBD>ķ<EFBFBD>λ<EFBFBD>ǣ<EFBFBD><C7A3><EFBFBD><EFBFBD>ڼ<EFBFBD><DABC>㷽λ<E3B7BD>DZ仯<C7B1><E4BBAF><EFBFBD><EFBFBD>
Point3 AntnnaAxisX; // <20><><EFBFBD><EFBFBD>X<EFBFBD><58>ָ<EFBFBD><D6B8>
Point3 AntnnaAxisY; // <20><><EFBFBD><EFBFBD>Y<EFBFBD><59>ָ<EFBFBD><D6B8>
Point3 AntnnaAxisZ; // <20><><EFBFBD><EFBFBD>Z<EFBFBD><5A>ָ<EFBFBD><D6B8>
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private: // <20><><EFBFBD><EFBFBD>ģ<EFBFBD><C4A3>
合并仿真、成像、影像合并的代码
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std::vector<SatelliteOribtNode> oribtNodes;
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long double oribtStartTime; // <20><><EFBFBD><EFBFBD>ģ<EFBFBD>Ͳο<CDB2>ʱ<EFBFBD><CAB1>
合并仿真、成像、影像合并的代码
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std::vector<double> polyfitPx; // <20>ռ<EFBFBD><D5BC><EFBFBD><EFBFBD><EFBFBD>
std::vector<double> polyfitPy;
std::vector<double> polyfitPz;
std::vector<double> polyfitVx; // <20>ٶ<EFBFBD><D9B6><EFBFBD><EFBFBD>ϲ<EFBFBD><CFB2><EFBFBD>
std::vector<double> polyfitVy;
std::vector<double> polyfitVz;
double Pxchisq; // <20><><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD> X2
double Pychisq;
double Pzchisq;
double Vxchisq;
double Vychisq;
double Vzchisq;
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private:
double Pt; // <20><><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ѹ
double Gri;// ϵͳ<CFB5><CDB3><EFBFBD><EFBFBD>
增加了DEM重采样工具
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public:
long double getOribtStartTime(); // <20><><EFBFBD><EFBFBD>ģ<EFBFBD>Ͳο<CDB2>ʱ<EFBFBD><CAB1>
std::vector<double> getPolyfitPx(); // <20>ռ<EFBFBD><D5BC><EFBFBD><EFBFBD><EFBFBD>
std::vector<double> getPolyfitPy();
std::vector<double> getPolyfitPz();
std::vector<double> getPolyfitVx(); // <20>ٶ<EFBFBD><D9B6><EFBFBD><EFBFBD>ϲ<EFBFBD><CFB2><EFBFBD>
std::vector<double> getPolyfitVy();
std::vector<double> getPolyfitVz();
同步轨道模型的修改
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public: // <20><><EFBFBD>ӽڵ<D3BD>
void addOribtNode(SatelliteOribtNode node);
ErrorCode polyFit(int polynum = 3, bool input_timeFromReferenceTime = false);
合并仿真、成像、影像合并的代码
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同步轨道模型的修改
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合并仿真、成像、影像合并的代码
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public:
virtual double getPt() override;
virtual double getGri() override;
virtual void setPt(double Pt) override;
virtual void setGri(double gri) override;
//virtual double getPt();
//virtual double getGri();
//virtual void setPt(double Pt);
//virtual void setGri(double gri);
同步轨道模型的修改
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合并仿真、成像、影像合并的代码
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};
std::shared_ptr<AbstractSatelliteOribtModel> CreataPolyfitSatelliteOribtModel(std::vector<SatelliteOribtNode> &nodes, long double startTime,int polynum=3);