民用飞机设计与研究
民用飛機設計與研究
민용비궤설계여연구
CIVIL AIRCRAFT DESIGN AND RESEARCH
2015年
1期
105-108
,共4页
飞控襟翼硬件仿真系统%铁鸟%飞控系统
飛控襟翼硬件倣真繫統%鐵鳥%飛控繫統
비공금익경건방진계통%철조%비공계통
flight control system of flap hardware simulator%iron bird%flight control system
以飞机控制系统的设计要求为依据设计飞控襟翼硬件仿真系统，该系统是参照真实飞控襟翼系统的功能和接口要求，采用基于数字仿真扩展模拟电路接口的硬件仿真系统。其与真实襟翼具有相似功能、相同接口、完全可以替代真实襟翼完成相关试验。试验结果表明：该系统为飞控襟翼试验的圆满完成提供有效的保障。
以飛機控製繫統的設計要求為依據設計飛控襟翼硬件倣真繫統，該繫統是參照真實飛控襟翼繫統的功能和接口要求，採用基于數字倣真擴展模擬電路接口的硬件倣真繫統。其與真實襟翼具有相似功能、相同接口、完全可以替代真實襟翼完成相關試驗。試驗結果錶明：該繫統為飛控襟翼試驗的圓滿完成提供有效的保障。
이비궤공제계통적설계요구위의거설계비공금익경건방진계통，해계통시삼조진실비공금익계통적공능화접구요구，채용기우수자방진확전모의전로접구적경건방진계통。기여진실금익구유상사공능、상동접구、완전가이체대진실금익완성상관시험。시험결과표명：해계통위비공금익시험적원만완성제공유효적보장。
In this paper, the control system of flap hardware simulator is carried out based on the request of flight control system. The interfaces and functions of this system are the same with the real flap flight control system. Hardware simulation methods based on digital simulation module expansion analog circuit connection are adopted to investigate the hardware simulation module of the flap flight control system which have the same function and con-nections with the real flap system. The related experiments could be done by using the flight control system of flap hardware simulator instead of the real flap system. The results show that the system could provide security for flap flight control system.
