#include "Aerodynamics_output.hpp"
namespace XNSim::C909::ATA04
{
Aerodynamics_output_Interface::Aerodynamics_output_Interface()
{
	MAP_DATA_FUNC(l_04_o_aerocomac_fxb_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_fyb_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_fzb_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_mxb_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_myb_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_mzb_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_cls_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_cl_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_cd_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_cm_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_cr_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_cy_f8);
	MAP_DATA_FUNC(l_04_o_aerocomac_cn_f8);
	this->header[0] = 0xa6; // XNSim头，0xa6
	this->header[1] = 0xc0; // 机型头，0xc0表示C909
	this->header[2] = 0x04; // 章节头，0x04表示ATA04
	this->header[3] = 0x01; // 模型头，0x01表示GroundHandling
	this->header[4] = 0x00; // 结构体头，0x00表示输入结构体
	this->header[5] = 0x00; // 数据方向，0x00表示外部输入
	this->header[6] = 0x00; // 数据大小
	this->header[7] = 0x00; // 数据大小
}
Aerodynamics_output_Interface::~Aerodynamics_output_Interface()
{
}
void Aerodynamics_output_Interface::Initialize(XNFrameworkPtr framework, uint32_t modelId,uint32_t DDS_type)
{
	auto ddsManager = framework->GetDDSManager();
	if (!ddsManager) {
		LOG_ERROR("DDSManager is nullptr");
		return;
	}
	if (DDS_type == 0) {
		dataWriter = ddsManager->RegisterPublisher<XNSim::C909::ATA04::Aerodynamics_outputPubSubType>("XNSim::C909::ATA04::Aerodynamics_output", modelId);
		ddsManager->RegisterSubscriber<XNSim::C909::ATA04::Aerodynamics_outputPubSubType>("XNSim::C909::ATA04::Aerodynamics_output", modelId, std::bind(&Aerodynamics_output_Interface::inputDataListener, this, std::placeholders::_1));
	}
	else if (DDS_type == 1) {
		ddsManager->RegisterSubscriber<XNSim::C909::ATA04::Aerodynamics_outputPubSubType>("XNSim::C909::ATA04::Aerodynamics_output", modelId, std::bind(&Aerodynamics_output_Interface::inputDataListener, this, std::placeholders::_1));
	}
	else if (DDS_type == 2) {
		dataWriter = ddsManager->RegisterPublisher<XNSim::C909::ATA04::Aerodynamics_outputPubSubType>("XNSim::C909::ATA04::Aerodynamics_output", modelId);
	}
}
void Aerodynamics_output_Interface::clearOutData()
{
	this->out_data = XNSim::C909::ATA04::Aerodynamics_output();
}
void Aerodynamics_output_Interface::sendOutData()
{
	if (dataWriter) {
		dataWriter->write(&this->out_data);
	}
}
void Aerodynamics_output_Interface::inputDataListener(const XNSim::C909::ATA04::Aerodynamics_output &input)
{
	this->data = input;
}
}