Journal of South China University of Technology(Natural Science Edition) ›› 2012, Vol. 40 ›› Issue (6): 76-83.

• Electronics, Communication & Automation Technology • Previous Articles     Next Articles

Design of Hierarchical Hybrid Virtual Prototype of MAV Flight Control System

Wang Xi-chao1  Cao Yun-feng1  Liu Xing-hua1  Ding Meng1  Zhuang Li-kui1  Wang Biao1  Yang Bin2   

  1. 1. College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,Jiangsu,China; 2.  College of Electrical Engineering,University of South China,Hengyang 421001,Hunan,China
  • Received:2011-11-03 Revised:2011-12-19 Online:2012-06-25 Published:2012-05-03
  • Contact: 王西超(1982-) ，男，博士生，主要从事虚拟样机技术、飞行控制系统设计与仿真等的研究． E-mail:wangxichao@nuaa.edu.cn
  • About author:王西超(1982-) ，男，博士生，主要从事虚拟样机技术、飞行控制系统设计与仿真等的研究．
  • Supported by:

    国家自然科学基金资助项目( 61102108) ; 南京航空航天大学引进人才基金资助项目( 1007-56YAH10047) ; 航空科学基金资助项目( 20110752005)

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Abstract:

In order to overcome the problems existing in the traditional design method of micro air vehicles ( MAVs) ,such as long period,high cost and low efficiency,a design environment of virtual prototype of the flight control system ( FCS-VP) is constructed. In this environment,the FCS-VP of a MAV, which is in a hybrid three-layer structure consisting of a task-scheduling layer,an action-planning layer and a basic regulation layer,is designed with SysML and Simulink. Simulation results demonstrate that the designed FCS-VP well simulates the FCS of MAV in terms of structure,f unction, behavior and performance,supports the further model-driven development of flight control software and improves the efficiency of MAV design.

Key words: micro air vehicle, flight control system, virtual prototype, SysML, model-driven development