#include "stdafx.h"
#include "GF3PSTNClass.h"
#include "GeoOperator.h"
#include <boost/math/tools/polynomial.hpp> // 多项式
#include "BaseTool.h"
#include <QDebug>



GF3PolyfitSatelliteOribtModel::GF3PolyfitSatelliteOribtModel()
{
	this->oribtStartTime = 0;
	this->beamAngle = 0;
	this->RightLook = true;
	this->cycletime = 0;
	this->minAzAngle = 0;
	this->maxAzAngle = 0;
	this->referenceAzAngle = 0;
	this->referenceTimeFromStartTime = 0;
	this->AntnnaAxisX = Point3{ 1,0,0 };
	this->AntnnaAxisY = Point3{ 0,1,0 };
	this->AntnnaAxisZ = Point3{ 0,0,1 };
	this->Pxchisq = 0;
	this->Pychisq = 0;
	this->Pzchisq = 0;
	this->Vxchisq = 0;
	this->Vychisq = 0;
	this->Vzchisq = 0;
	this->Pt = 1;
	this->Gri = 1;
}

GF3PolyfitSatelliteOribtModel::~GF3PolyfitSatelliteOribtModel()
{
	//TODO: 析构函数


}

QString GF3PolyfitSatelliteOribtModel::getSatelliteOribtModelParamsString()
{
	QString result = "";
	result += this->polyfitPx.size() - 1 + "\n";
	result += "----------- poly Position X  -------------------------\n";
	for (long i = 0; i < this->polyfitPx.size(); i++) { // 求解平方
		result += QString::number(this->polyfitPx[i], 'e', 6) + "\n";
	}
	result += "----------- poly Position Y  -------------------------\n";
	for (long i = 0; i < this->polyfitPx.size(); i++) { // 求解平方
		result += QString::number(this->polyfitPy[i], 'e', 6) + "\n";
	}
	result += "----------- poly Position Z  -------------------------\n";
	for (long i = 0; i < this->polyfitPx.size(); i++) { // 求解平方
		result += QString::number(this->polyfitPz[i], 'e', 6) + "\n";
	}
	result += "----------- poly Position Vector X  ------------------\n";
	for (long i = 0; i < this->polyfitPx.size(); i++) { // 求解平方
		result += QString::number(this->polyfitVx[i], 'e', 6) + "\n";
	}
	result += "----------- poly Position Vector Y  ------------------\n";
	for (long i = 0; i < this->polyfitPx.size(); i++) { // 求解平方
		result += QString::number(this->polyfitVy[i], 'e', 6) + "\n";
	}
	result += "----------- poly Position Vector Z  ------------------\n";
	for (long i = 0; i < this->polyfitPx.size(); i++) { // 求解平方
		result += QString::number(this->polyfitVz[i], 'e', 6) + "\n";
	}
	result += "------------------------------------------------------\n";
	printf("%s\n", result.toUtf8().constData());
	return result;
}

SatelliteOribtNode GF3PolyfitSatelliteOribtModel::getSatelliteOribtNode(double& timeFromStartTime, bool& antAzAngleFlag)
{
	// 位置、速度
	SatelliteOribtNode node;
	ErrorCode state = getSatelliteOribtNode(timeFromStartTime, node, antAzAngleFlag);
	return node;
}

ErrorCode GF3PolyfitSatelliteOribtModel::getSatelliteOribtNode(double& timeFromStartTime, SatelliteOribtNode& node, bool& antAzAngleFlag)
{
	// 卫星坐标，速度方向
	node.time = timeFromStartTime;
	node.Px = 0;
	node.Py = 0;
	node.Pz = 0;
	node.Vx = 0;
	node.Vy = 0;
	node.Vz = 0;

	for (long i = 0; i < this->polyfitPx.size(); i++) { // 求解平方
		node.Px += this->polyfitPx[i] * pow(timeFromStartTime, i);
		node.Py += this->polyfitPy[i] * pow(timeFromStartTime, i);
		node.Pz += this->polyfitPz[i] * pow(timeFromStartTime, i);
		node.Vx += this->polyfitVx[i] * pow(timeFromStartTime, i);
		node.Vy += this->polyfitVy[i] * pow(timeFromStartTime, i);
		node.Vz += this->polyfitVz[i] * pow(timeFromStartTime, i);
	}


	node.beamAngle = this->beamAngle; // 波位角
	ErrorCode Azstatecode = this->getAzAngleInCurrentTimeFromStartTime(timeFromStartTime, node.AzAngle); // 摆动角
	if (Azstatecode != ErrorCode::SUCCESS) {
		return Azstatecode;
	}
	else {}


	if (!antAzAngleFlag) {
		return ErrorCode::SUCCESS;
	}
	else {
	}
	// 计算卫星天线指向
	ErrorCode state = getAntnnaDirection(node);

	if (state != ErrorCode::SUCCESS) {
		return state;
	}
	else {}

	state = getZeroDopplerAntDirect(node);
	if (state != ErrorCode::SUCCESS) {
		return state;
	}
	else {}
	return ErrorCode::SUCCESS;
}


ErrorCode GF3PolyfitSatelliteOribtModel::getSatelliteAntDirectNormal(SatelliteOribtNode& Rs, Vector3D& Rt, SatelliteAntDirect& antNode)
{
	//Vector3D Rts = Vector3D{Rt.x-Rs.Px,Rt.y- Rs.Py,Rt.z-Rs.Pz}; // Rts t-->s
	antNode.Xst = (Rt.x - Rs.Px); // 卫星 -->  地面
	antNode.Yst = (Rt.y - Rs.Py);
	antNode.Zst = (Rt.z - Rs.Pz);
	antNode.Vxs = Rs.Vx;		  // 卫星速度
	antNode.Vys = Rs.Vy;
	antNode.Vzs = Rs.Vz;
	// 天线指向在天线坐标系下的值
	antNode.Xant = (antNode.Xst * (Rs.AntYaxisY * Rs.AntZaxisZ - Rs.AntYaxisZ * Rs.AntZaxisY) + antNode.Xst * (Rs.AntXaxisZ * Rs.AntZaxisY - Rs.AntXaxisY * Rs.AntZaxisZ) + antNode.Xst * (Rs.AntXaxisY * Rs.AntYaxisZ - Rs.AntXaxisZ * Rs.AntYaxisY)) / (Rs.AntXaxisX * (Rs.AntYaxisY * Rs.AntZaxisZ - Rs.AntZaxisY * Rs.AntYaxisZ) - Rs.AntYaxisX * (Rs.AntXaxisY * Rs.AntZaxisZ - Rs.AntXaxisZ * Rs.AntZaxisY) + Rs.AntZaxisX * (Rs.AntXaxisY * Rs.AntYaxisZ - Rs.AntXaxisZ * Rs.AntYaxisY));
	antNode.Yant = (antNode.Yst * (Rs.AntYaxisZ * Rs.AntZaxisX - Rs.AntYaxisX * Rs.AntZaxisZ) + antNode.Yst * (Rs.AntXaxisX * Rs.AntZaxisZ - Rs.AntXaxisZ * Rs.AntZaxisX) + antNode.Yst * (Rs.AntYaxisX * Rs.AntXaxisZ - Rs.AntXaxisX * Rs.AntYaxisZ)) / (Rs.AntXaxisX * (Rs.AntYaxisY * Rs.AntZaxisZ - Rs.AntZaxisY * Rs.AntYaxisZ) - Rs.AntYaxisX * (Rs.AntXaxisY * Rs.AntZaxisZ - Rs.AntXaxisZ * Rs.AntZaxisY) + Rs.AntZaxisX * (Rs.AntXaxisY * Rs.AntYaxisZ - Rs.AntXaxisZ * Rs.AntYaxisY));
	antNode.Zant = (antNode.Zst * (Rs.AntYaxisX * Rs.AntZaxisY - Rs.AntYaxisY * Rs.AntZaxisX) + antNode.Zst * (Rs.AntXaxisY * Rs.AntZaxisX - Rs.AntXaxisX * Rs.AntZaxisY) + antNode.Zst * (Rs.AntXaxisX * Rs.AntYaxisY - Rs.AntYaxisX * Rs.AntXaxisY)) / (Rs.AntXaxisX * (Rs.AntYaxisY * Rs.AntZaxisZ - Rs.AntZaxisY * Rs.AntYaxisZ) - Rs.AntYaxisX * (Rs.AntXaxisY * Rs.AntZaxisZ - Rs.AntXaxisZ * Rs.AntZaxisY) + Rs.AntZaxisX * (Rs.AntXaxisY * Rs.AntYaxisZ - Rs.AntXaxisZ * Rs.AntYaxisY));
	// 计算theta 与 phi
	antNode.Norm = std::sqrt(antNode.Xant * antNode.Xant + antNode.Yant * antNode.Yant + antNode.Zant * antNode.Zant); // 计算 pho
	antNode.ThetaAnt = std::acos(antNode.Zant / antNode.Norm); // theta 与 Z轴的夹角
	antNode.PhiAnt = (antNode.Yant * std::sin(antNode.ThetaAnt) / std::abs(antNode.Yant * std::sin(antNode.ThetaAnt))) * std::acos(antNode.Xant / (antNode.Norm * std::sin(antNode.ThetaAnt)));
	return ErrorCode::SUCCESS;
}

void GF3PolyfitSatelliteOribtModel::setSatelliteOribtStartTime(long double oribtStartTime)
{
	this->oribtStartTime = oribtStartTime;
}

long double GF3PolyfitSatelliteOribtModel::getSatelliteOribtStartTime()
{
	return this->oribtStartTime;
}

void GF3PolyfitSatelliteOribtModel::setbeamAngle(double beamAngle, bool RightLook)
{
	this->beamAngle = beamAngle;
	this->RightLook = RightLook;
}

void GF3PolyfitSatelliteOribtModel::setAzAngleRange(double cycletime, double minAzAngle, double maxAzAngle, double referenceAzAngle, double referenceTimeFromStartTime)
{
	this->cycletime = cycletime;
	this->minAzAngle = minAzAngle;
	this->maxAzAngle = maxAzAngle;
	this->referenceAzAngle = referenceAzAngle;
	this->referenceTimeFromStartTime = referenceTimeFromStartTime;
}

double GF3PolyfitSatelliteOribtModel::getAzAngleInCurrentTimeFromStartTime(double& currentTime)
{
	// 计算角度
	double Azangle = 0;
	ErrorCode state = getAzAngleInCurrentTimeFromStartTime(currentTime, Azangle);
	return Azangle;
}

/// 
///   X=Y x Z          摆动角(-）				    摆动角（+）
///      Z				  Z					            Z		
/// 	 ^				   \						   /
/// 	 |					\						  /
///  y<--X---			 y<--X---				 y<--X---
///      |				     |\    				    /|    
/// 	 |					   \				   /  	
/// 

ErrorCode GF3PolyfitSatelliteOribtModel::getAzAngleInCurrentTimeFromStartTime(double& currentTime, double& AzAngle)
{
	if (std::abs(this->maxAzAngle - this->minAzAngle) < 1e-7 || std::abs(this->cycletime) < 1e-7) {
		AzAngle = this->referenceAzAngle;
		return ErrorCode::SUCCESS;
	}
	else {
		AzAngle = this->referenceAzAngle + (currentTime - this->referenceTimeFromStartTime) / this->cycletime * (this->maxAzAngle - this->minAzAngle);
		return ErrorCode::SUCCESS;
	}
}

void GF3PolyfitSatelliteOribtModel::setAntnnaAxisX(double X, double Y, double Z)
{
	this->AntnnaAxisX = Point3{ X, Y, Z };
}

void GF3PolyfitSatelliteOribtModel::setAntnnaAxisY(double X, double Y, double Z)
{
	this->AntnnaAxisY = Point3{ X, Y, Z };
}

void GF3PolyfitSatelliteOribtModel::setAntnnaAxisZ(double X, double Y, double Z)
{
	this->AntnnaAxisZ = Point3{ X, Y, Z };
}

///           左视(+）				        右视（-）
///      Z				  Z					            Z		
/// 	 ^				   \						   /
/// 	 |					\						  /
///  x<--O---			 x<--O---				 x<--O---
///      |				     |\    				    /|    
/// 						   \				   /  	
/// 
ErrorCode GF3PolyfitSatelliteOribtModel::getAntnnaDirection(SatelliteOribtNode& node)
{
	bool flag = false;
	double nexttime = node.time + 1e-6;
	SatelliteOribtNode node1 = this->getSatelliteOribtNode(nexttime, flag);

	//qDebug() << "getAntnnaDirection  corrdination " << std::endl;

	double Vx = (node1.Px - node.Px);
	double Vy = (node1.Py - node.Py);
	double Vz = (node1.Pz - node.Pz);

	// 代码测试部分
	//node.Px = 0;
	//node.Py = 0;
	//node.Pz = 1;

	//Vx = 1, Vy = 0, Vz = 0;


	// 1. 计算天线指向
	Eigen::Vector3d axisZ0 = { -1 * node.Px ,-1 * node.Py,-1 * node.Pz };	// z 轴 --波位角为0时，天线指向的反方向
	Eigen::Vector3d axisX0 = { Vx,Vy,Vz };	// x 轴 --飞行方向
	Eigen::Vector3d axisY0 = axisZ0.cross(axisX0);			// y 轴 --右手定则  -- 初始坐标系

	//qDebug() << "axis_X0=[ " << axisX0.x() << "," << axisX0.y() << "," << axisX0.z() << "]" << std::endl;
	//qDebug() << "axis_Y0=[ " << axisY0.x() << "," << axisY0.y() << "," << axisY0.z() << "]" << std::endl;
	//qDebug() << "axis_Z0=[ " << axisZ0.x() << "," << axisZ0.y() << "," << axisZ0.z() << "]" << std::endl;

	double rotateAngle = this->RightLook ? -this->beamAngle : this->beamAngle; // 旋转角度 左（逆时针）：theta , 右（顺时针）： -theta 
	//qDebug() << "rotateAngle=" << rotateAngle << std::endl;
	//qDebug() << "Look side:\t" << (this->RightLook ? "right" : "left") << std::endl;
	// 1.2. 根据波位角，确定卫星绕X轴-飞行轴
	Eigen::Matrix3d rotateMatrixBeam = rotationMatrix(axisX0, rotateAngle * d2r); // 旋转矩阵
	axisZ0 = rotateMatrixBeam * axisZ0; // 旋转矩阵
	axisY0 = rotateMatrixBeam * axisY0;
	axisX0 = rotateMatrixBeam * axisX0;
	// 1.3. 根据方位角，确定卫星绕Y轴旋转
	double azangle = node.AzAngle;
	Eigen::Matrix3d rotateMatrixAzAngle = rotationMatrix(axisY0, azangle * d2r); // 旋转矩阵
	axisZ0 = rotateMatrixAzAngle * axisZ0; // 旋转矩阵
	axisY0 = rotateMatrixAzAngle * axisY0;
	axisX0 = rotateMatrixAzAngle * axisX0;

	// 1.4. 计算实际指向
	node.AntDirecX = axisZ0[0];
	node.AntDirecY = axisZ0[1];
	node.AntDirecZ = axisZ0[2];

	// 2. 计算天线坐标系,方便计算天线方向图

	node.AntXaxisX = axisX0[0]; // 实际天线坐标系 在 WGS84 坐标系
	node.AntXaxisY = axisX0[1];
	node.AntXaxisZ = axisX0[2];

	node.AntYaxisX = axisY0[0];
	node.AntYaxisY = axisY0[1];
	node.AntYaxisZ = axisY0[2];

	node.AntZaxisX = axisZ0[0];
	node.AntZaxisY = axisZ0[1];
	node.AntZaxisZ = axisZ0[2];


	//qDebug() << "axis_X=[" << axisX0.x() << "," << axisX0.y() << "," << axisX0.z() << "]" << std::endl;
	//qDebug() << "axis_Y=[" << axisY0.x() << "," << axisY0.y() << "," << axisY0.z() << "]" << std::endl;
	//qDebug() << "axis_Z=[" << axisZ0.x() << "," << axisZ0.y() << "," << axisZ0.z() << "]" << std::endl;
	//qDebug() << "------------------------------------" << std::endl;
	return ErrorCode::SUCCESS;
}

ErrorCode GF3PolyfitSatelliteOribtModel::getZeroDopplerAntDirect(SatelliteOribtNode& node)
{
	bool flag = false;
	double nexttime = node.time + 1e-6;
	SatelliteOribtNode node1 = this->getSatelliteOribtNode(nexttime, flag);

	// 1. 计算天线指向
	Eigen::Vector3d axisZ0 = { -1 * node.Px ,-1 * node.Py,-1 * node.Pz };	// z 轴 --波位角为0时，天线指向的反方向
	Eigen::Vector3d axisX0 = { (node1.Px - node.Px)  , (node1.Py - node.Py)  , (node1.Pz - node.Pz) };	// x 轴 --飞行方向
	Eigen::Vector3d axisY0 = axisZ0.cross(axisX0);			// y 轴 --右手定则  -- 初始坐标系

	double rotateAngle = this->RightLook ? -this->beamAngle : this->beamAngle; // 旋转角度 左（逆时针）：theta , 右（顺时针）： -theta 

	// 1.2. 根据波位角，确定卫星绕X轴-飞行轴
	Eigen::Matrix3d rotateMatrixBeam = rotationMatrix(axisX0, rotateAngle * d2r); // 旋转矩阵
	axisZ0 = rotateMatrixBeam * axisZ0; // 旋转矩阵
	axisY0 = rotateMatrixBeam * axisY0;
	axisX0 = rotateMatrixBeam * axisX0;
	// 1.3. 根据方位角，确定卫星绕Y轴旋转
	double azangle = 0;
	Eigen::Matrix3d rotateMatrixAzAngle = rotationMatrix(axisY0, azangle * d2r); // 旋转矩阵
	axisZ0 = rotateMatrixAzAngle * axisZ0; // 旋转矩阵
	axisY0 = rotateMatrixAzAngle * axisY0;
	axisX0 = rotateMatrixAzAngle * axisX0;

	// 1.4. 计算实际指向
	node.zeroDopplerDirectX = axisZ0[0];
	node.zeroDopplerDirectY = axisZ0[1];
	node.zeroDopplerDirectZ = axisZ0[2];

	return ErrorCode::SUCCESS;
}

void GF3PolyfitSatelliteOribtModel::addOribtNode(SatelliteOribtNode node)
{
	this->oribtNodes.push_back(node);
}



ErrorCode GF3PolyfitSatelliteOribtModel::polyFit(int polynum/*=3*/, bool input_timeFromReferenceTime)
{
	if (polynum > this->oribtNodes.size() - 1) {
		return ErrorCode::OrbitNodeNotEnough;
	}
	else {}

	this->polyfitPx = std::vector<double>(polynum + 1, 0);
	this->polyfitPy = std::vector<double>(polynum + 1, 0);
	this->polyfitPz = std::vector<double>(polynum + 1, 0);
	this->polyfitVx = std::vector<double>(polynum + 1, 0);
	this->polyfitVy = std::vector<double>(polynum + 1, 0);
	this->polyfitVz = std::vector<double>(polynum + 1, 0);

	std::vector<double> timeArr = std::vector<double>(this->oribtNodes.size(), 0);
	std::vector<double> PxArr = std::vector<double>(this->oribtNodes.size(), 0);
	std::vector<double> PyArr = std::vector<double>(this->oribtNodes.size(), 0);
	std::vector<double> PzArr = std::vector<double>(this->oribtNodes.size(), 0);
	std::vector<double> VxArr = std::vector<double>(this->oribtNodes.size(), 0);
	std::vector<double> VyArr = std::vector<double>(this->oribtNodes.size(), 0);
	std::vector<double> VzArr = std::vector<double>(this->oribtNodes.size(), 0);

	// 数据准备
	for (long i = 0; i < this->oribtNodes.size(); i++) {
		if (input_timeFromReferenceTime) {
			timeArr[i] = this->oribtNodes[i].time;
		}
		else {
			timeArr[i] = this->oribtNodes[i].time - this->oribtStartTime; // 以参考时间为基准
			qDebug() << this->oribtNodes[i].time << "\t--->\t" << timeArr[i];
		}
		PxArr[i] = this->oribtNodes[i].Px;
		PyArr[i] = this->oribtNodes[i].Py;
		PzArr[i] = this->oribtNodes[i].Pz;
		VxArr[i] = this->oribtNodes[i].Vx;
		VyArr[i] = this->oribtNodes[i].Vy;
		VzArr[i] = this->oribtNodes[i].Vz;
	}

	// 拟合Px Py Pz Vx Vy Vz
	ErrorCode codePx = polynomial_fit(timeArr, PxArr, polynum, this->polyfitPx, this->Pxchisq);
	ErrorCode codePy = polynomial_fit(timeArr, PyArr, polynum, this->polyfitPy, this->Pychisq);
	ErrorCode codePz = polynomial_fit(timeArr, PzArr, polynum, this->polyfitPz, this->Pzchisq);
	ErrorCode codeVx = polynomial_fit(timeArr, VxArr, polynum, this->polyfitVx, this->Vxchisq);
	ErrorCode codeVy = polynomial_fit(timeArr, VyArr, polynum, this->polyfitVy, this->Vychisq);
	ErrorCode codeVz = polynomial_fit(timeArr, VzArr, polynum, this->polyfitVz, this->Vzchisq);


	// 打印 this->polyfitPx
	qDebug() << "polyfit value:";
	qDebug() << "Px" << "\t" << "Py" << "\t" << "Pz" << "\t" << "Vx" << "\t" << "Vy" << "\t" << "Vz";
	for (long i = 0; i < this->polyfitPx.size(); i++) { // 求解平方
		qDebug() << this->polyfitPx[i] << "\t" << this->polyfitPy[i] << "\t" << this->polyfitPz[i] << "\t" << this->polyfitVx[i] << "\t" << this->polyfitVy[i] << "\t" << this->polyfitVz[i];
	}


	// 评价拟合情况
	double starttime = this->oribtStartTime;
	qDebug() << "oribt refrence time: " << starttime;
	qDebug() << "time" << "\t" << "dPx" << "\t" << "dPy" << "\t" << "dPz" << "\t" << "dVx" << "\t" << "dVy" << "\t" << "dVz";
	for (long i = 0; i < timeArr.size(); i++) {
		double time_temp = timeArr[i];
		bool flag = false;
		SatelliteOribtNode tempnode;
		this->getSatelliteOribtNode(time_temp, tempnode, flag);
		qDebug() << timeArr[i] << "\t" << PxArr[i] - tempnode.Px << "\t" << PyArr[i] - tempnode.Py << "\t" << PzArr[i] - tempnode.Pz << "\t" << VxArr[i] - tempnode.Vx << "\t" << VyArr[i] - tempnode.Vy << "\t" << VzArr[i] - tempnode.Vz;
	}
	return ErrorCode::SUCCESS;
}

double GF3PolyfitSatelliteOribtModel::getPt()
{
	return this->Pt;
}

double GF3PolyfitSatelliteOribtModel::getGri()
{
	return this->Gri;
}

void GF3PolyfitSatelliteOribtModel::setPt(double pt)
{
	this->Pt = pt;
}

void GF3PolyfitSatelliteOribtModel::setGri(double gri)
{
	this->Gri = gri;
}

std::shared_ptr<GF3PolyfitSatelliteOribtModel>    CreataGF3PolyfitSatelliteOribtModel(std::vector<SatelliteOribtNode>& nodes, long double startTime, int polynum)
{
	qDebug() << "CreataGF3PolyfitSatelliteOribtModel \t" << (double)startTime << "\t" << polynum;


	std::shared_ptr<GF3PolyfitSatelliteOribtModel> ployfitOribtModel = std::make_shared< GF3PolyfitSatelliteOribtModel>();
	for (long i = 0; i < nodes.size(); i++) {
		ployfitOribtModel->addOribtNode(nodes[i]);
	}
	ployfitOribtModel->setSatelliteOribtStartTime(startTime);
	ErrorCode stateCode = ployfitOribtModel->polyFit(polynum, false);
	if (stateCode != ErrorCode::SUCCESS) {
		qDebug() << QString::fromStdString(errorCode2errInfo(stateCode));
		return nullptr;
	}
	else {
		return ployfitOribtModel;
	}
	return ployfitOribtModel;
}