航空学报 > 2005, Vol. 26 Issue (5): 550-555

飞机动力学虚拟样机技术

刘刚, 王行仁, 贾荣珍   

  1. 北京航空航天大学 先进仿真技术航空科技重点实验室,北京 100083
  • 收稿日期:2004-08-16 修回日期:2004-11-22 出版日期:2005-10-25 发布日期:2005-10-25

Technique for Dynamic Virtual Prototype of Aircraft

LIU Gang, WANG Xing-ren, JIA Rong-zhen   

  1. Key Lab of Advanced Simulation Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
  • Received:2004-08-16 Revised:2004-11-22 Online:2005-10-25 Published:2005-10-25

摘要:

飞机动力学虚拟样机以研究飞机的动态特性为核心,通过虚拟样机各系统的建模与仿真,在系统开发和运行环境中对飞机的气动特性、控制系统、发动机特性、飞行性能和飞行品质进行分析、评估和研究,支持飞机的需求分析、方案论证、概念设计和初步设计,同时,飞行员可参与在回路中的操纵完成虚拟试飞验证。系统提供分布虚拟战场威胁环境,可在武器平台体系对抗环境中验证和评估飞机的作战效能。利用飞机动力学虚拟样机系统环境还可进行飞机的多学科优化设计。

关键词: 虚拟样机, 基于仿真的设计, 虚拟试飞, 作战效能, 多学科优化设计

Abstract:

Dynamic virtual prototype(DVP) of aircraft focuses on studying dynamics characters. Based-on Modeling and Simulation(M&S) of each subsystem, the aerodynamic characters, control system, engine characters, flight performance and flying qualities are analyzed, tested and evaluated in the development environment and run environment. DVP supports the requirement analyzed, program demonstration, conceptual design and preliminary design. Pilot can achieve virtual flight testing with Human-in-the-Loop. Combat effectiveness is certified and analyzed in the confrontation environment of weapon platform system. Multidiscipline design optimization(MDO) of aircraft is achieved in the collaborative environment of DVP.

Key words: virtual prototype, simulation based design, virtual flight testing, combat effectiveness, multidiscipline design optimization

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