#include "XNAerodynamics.h"
#include "XNAerodynamics_p.h"
#include <XNCore/XNModelManager.h>

XN_MODEL_INITIALIZE(XNAerodynamics)

XNAerodynamics::XNAerodynamics() : XNModelObject(new XNAerodynamicsPrivate())
{
}

XNAerodynamics::~XNAerodynamics()
{
}

XNAerodynamics::XNAerodynamics(PrivateType *p) : XNModelObject(p)
{
}

void XNAerodynamics::Initialize()
{
	T_D();
	SuperType::Initialize();
	if (d->_dynamicLib) {
		d->_fun = (FunctionType)dlsym(d->_dynamicLib, d->_entryPointName.c_str());
		if (!d->_fun) {
			LOG_WARNING("Failed to resolve _Z27SACSCAerodynamicsEntryPointP20ComacDataStructure_S");
		}
	}
	/* 在这里进行其它初始化 */
}

void XNAerodynamics::PrepareForExecute()
{
	T_D();
	SuperType::PrepareForExecute();
	InitializeData();
	d->_inputInterface.Initialize(GetFramework(), GetUniqueId(), 1);
	d->_outputInterface.Initialize(GetFramework(), GetUniqueId(), 2);
	d->_heartbeatInterface.Initialize(GetFramework(), GetUniqueId(), 2);
	/* 在这里进行其它运行前准备工作 */
}

void XNAerodynamics::StepUpdate()
{
	T_D();
	SuperType::StepUpdate();
	if (d->_fun) {
		d->_inputInterface.getData(d->_data.input_aero);
		d->_fun(&d->_data);
		d->_outputInterface.setData(d->_data.output_aero);
		d->_heartbeatInterface.setData(&d->_data);
	}
	/* 在这里进行其它运行时计算 */
}

void XNAerodynamics::InitializeData()
{
	T_D();
	d->_data.input_aero = new input_aero_S;
	// TODO: 在这里初始化输入数据
	d->_data.input_aero->l_04_i_aerocomac_ail_f8  = new double[10];
	d->_data.input_aero->l_04_i_aerocomac_elv_f8  = new double[4];
	d->_data.input_aero->l_04_i_aerocomac_rud_f8  = new double[2];
	d->_data.input_aero->l_04_i_aerocomac_gear_f8 = new double[7];
	d->_data.input_aero->l_04_i_aerocomac_flap_f8 = new double[10];
	d->_data.input_aero->l_04_i_aerocomac_slat_f8 = new double[20];
	d->_data.input_aero->l_04_i_aerocomac_spl_f8  = new double[20];
	d->_data.input_aero->l_04_i_aerocomac_tnet_f8 = new double[4];
	d->_data.input_aero->l_04_i_aerocomac_kice_f8 = new double[20];
	d->_data.output_aero						  = new output_aero_S;
	// TODO: 在这里初始化输出数据

	d->_data.aero_model_heartbeat = 0;
}

void XNAerodynamics::ReleaseData()
{
	T_D();
	// TODO: 在这里释放输入数据

	if (d->_data.input_aero) {
		if (d->_data.input_aero->l_04_i_aerocomac_ail_f8) {
			delete[] d->_data.input_aero->l_04_i_aerocomac_ail_f8;
		}
		if (d->_data.input_aero->l_04_i_aerocomac_elv_f8) {
			delete[] d->_data.input_aero->l_04_i_aerocomac_elv_f8;
		}
		if (d->_data.input_aero->l_04_i_aerocomac_rud_f8) {
			delete[] d->_data.input_aero->l_04_i_aerocomac_rud_f8;
		}
		if (d->_data.input_aero->l_04_i_aerocomac_gear_f8) {
			delete[] d->_data.input_aero->l_04_i_aerocomac_gear_f8;
		}
		if (d->_data.input_aero->l_04_i_aerocomac_flap_f8) {
			delete[] d->_data.input_aero->l_04_i_aerocomac_flap_f8;
		}
		if (d->_data.input_aero->l_04_i_aerocomac_slat_f8) {
			delete[] d->_data.input_aero->l_04_i_aerocomac_slat_f8;
		}
		if (d->_data.input_aero->l_04_i_aerocomac_spl_f8) {
			delete[] d->_data.input_aero->l_04_i_aerocomac_spl_f8;
		}
		if (d->_data.input_aero->l_04_i_aerocomac_tnet_f8) {
			delete[] d->_data.input_aero->l_04_i_aerocomac_tnet_f8;
		}
		if (d->_data.input_aero->l_04_i_aerocomac_kice_f8) {
			delete[] d->_data.input_aero->l_04_i_aerocomac_kice_f8;
		}
		delete d->_data.input_aero;
		d->_data.input_aero = nullptr;
	}
	// TODO: 在这里释放输出数据

	if (d->_data.output_aero) {
		delete d->_data.output_aero;
		d->_data.output_aero = nullptr;
	}
}