XNSim/Release/IDL/C909_V1/ATA04/Aerodynamics_input.hpp

#pragma once
#include "../C909_V1PubSubTypes.hpp"
#include "XNCore/XNDDSInterface.h"
namespace XNSim::C909::ATA04
{
class Aerodynamics_input_Interface final : public XNDDSInterface
{
public:
	Aerodynamics_input_Interface();
	virtual ~Aerodynamics_input_Interface();
	virtual void Initialize(XNFrameworkPtr framework, uint32_t modelId, uint32_t DDS_type) override;
	virtual void clearOutData() override;
	virtual void sendOutData() override;
	void inputDataListener(const XNSim::C909::ATA04::Aerodynamics_input &input);
	template <typename T>
	void getData(T *model_data)
	{
		if(model_data == nullptr)
			return;
		assign_value_get(data.l_04_i_aerocomac_alpha_f8(), model_data->l_04_i_aerocomac_alpha_f8);
		assign_value_get(data.l_04_i_aerocomac_alpdot_f8(), model_data->l_04_i_aerocomac_alpdot_f8);
		assign_value_get(data.l_04_i_aerocomac_beta_f8(), model_data->l_04_i_aerocomac_beta_f8);
		assign_value_get(data.l_04_i_aerocomac_press_alt_f8(), model_data->l_04_i_aerocomac_press_alt_f8);
		assign_value_get(data.l_04_i_aerocomac_tas_f8(), model_data->l_04_i_aerocomac_tas_f8);
		assign_value_get(data.l_04_i_aerocomac_mach_f8(), model_data->l_04_i_aerocomac_mach_f8);
		assign_value_get(data.l_04_i_aerocomac_nx_f8(), model_data->l_04_i_aerocomac_nx_f8);
		assign_value_get(data.l_04_i_aerocomac_ny_f8(), model_data->l_04_i_aerocomac_ny_f8);
		assign_value_get(data.l_04_i_aerocomac_nz_f8(), model_data->l_04_i_aerocomac_nz_f8);
		assign_value_get(data.l_04_i_aerocomac_p_f8(), model_data->l_04_i_aerocomac_p_f8);
		assign_value_get(data.l_04_i_aerocomac_q_f8(), model_data->l_04_i_aerocomac_q_f8);
		assign_value_get(data.l_04_i_aerocomac_r_f8(), model_data->l_04_i_aerocomac_r_f8);
		assign_value_get(data.l_04_i_aerocomac_qbar_f8(), model_data->l_04_i_aerocomac_qbar_f8);
		assign_value_get(data.l_04_i_aerocomac_blcg_f8(), model_data->l_04_i_aerocomac_blcg_f8);
		assign_value_get(data.l_04_i_aerocomac_bscg_f8(), model_data->l_04_i_aerocomac_bscg_f8);
		assign_value_get(data.l_04_i_aerocomac_wlcg_f8(), model_data->l_04_i_aerocomac_wlcg_f8);
		assign_value_get(data.l_04_i_aerocomac_ail_f8(), model_data->l_04_i_aerocomac_ail_f8);
		assign_value_get(data.l_04_i_aerocomac_elv_f8(), model_data->l_04_i_aerocomac_elv_f8);
		assign_value_get(data.l_04_i_aerocomac_rud_f8(), model_data->l_04_i_aerocomac_rud_f8);
		assign_value_get(data.l_04_i_aerocomac_stab_f8(), model_data->l_04_i_aerocomac_stab_f8);
		assign_value_get(data.l_04_i_aerocomac_gear_f8(), model_data->l_04_i_aerocomac_gear_f8);
		assign_value_get(data.l_04_i_aerocomac_flap_f8(), model_data->l_04_i_aerocomac_flap_f8);
		assign_value_get(data.l_04_i_aerocomac_slat_f8(), model_data->l_04_i_aerocomac_slat_f8);
		assign_value_get(data.l_04_i_aerocomac_spl_f8(), model_data->l_04_i_aerocomac_spl_f8);
		assign_value_get(data.l_04_i_aerocomac_tnet_f8(), model_data->l_04_i_aerocomac_tnet_f8);
		assign_value_get(data.l_04_i_aerocomac_kice_f8(), model_data->l_04_i_aerocomac_kice_f8);
		assign_value_get(data.l_04_i_aerocomac_alt_agl_f8(), model_data->l_04_i_aerocomac_alt_agl_f8);
	}
	template <typename T>
	void setData(T *model_data)
	{
		if(model_data == nullptr)
			return;
		clearOutData();
		assign_value_set(data.l_04_i_aerocomac_alpha_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_alpdot_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_beta_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_press_alt_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_tas_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_mach_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_nx_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_ny_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_nz_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_p_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_q_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_r_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_qbar_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_blcg_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_bscg_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_wlcg_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_ail_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_elv_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_rud_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_stab_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_gear_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_flap_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_slat_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_spl_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_tnet_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_kice_f8(), model_data->Aerodynamics_input);
		assign_value_set(data.l_04_i_aerocomac_alt_agl_f8(), model_data->Aerodynamics_input);
	}
private:
	XNSim::C909::ATA04::Aerodynamics_input data;
	XNSim::C909::ATA04::Aerodynamics_input out_data;
};
}