论文信息 - Study on Virtual Prototyping testing platform for Flight Control Computer System of civil aircraft

Study on Virtual Prototyping testing platform for Flight Control Computer System of civil aircraft

Virtual prototyping is introduced and the future development trends of Virtual Prototyping for Flight Control System are summarized. For analyzing redundancy Flight Control Computer Systems (FCCS) of Boeing, Airbus series and BUAA civil aircraft scheme, a VP testing platform for FCCS of civil aircraft is proposed. This platform is based on COTS products, modular components and user interactive interface. It can produce virtual prototypes of dissimilar redundancy FCCSs of Boeing 777, Airbus A340 and BUAA civil aircraft scheme. This platform is open and expandable, supporting concurrent multidisciplinary design.

Zongji Chen | Xiaozhe Sun | Xudong Qin

[1] E. Kane Casani,et al. Flight system testbed , 1994, Defense, Security, and Sensing.

[2] Xiong Guang-leng. Virtual Prototyping Technology , 2001 .

[3] K. Vogel,et al. An integrated COTS prototyping and test environment for spacecraft control systems , 1993 .

[4] G. Gary Wang,et al. Definition and Review of Virtual Prototyping , 2002, J. Comput. Inf. Sci. Eng..

[5] Pascal Traverse,et al. AIRBUS A320/A330/A340 electrical flight controls - A family of fault-tolerant systems , 1993, FTCS-23 The Twenty-Third International Symposium on Fault-Tolerant Computing.

[6] Peng Wang,et al. The recent research on virtual prototyping engineering for complex products , 2004, 8th International Conference on Computer Supported Cooperative Work in Design.

[7] Chen Zong. VIRTUAL PROTOTYPING FOR FLIGHT CONTROL SYSTEMS , 2002 .

[8] M. H. Smaili. Simulation of an Affordable Fly-By-Wire System for Small Commercial Aircraft , 2001 .

[9] Gao Jin-yuan. Dissimilar Redundant Flight Control Computer System , 2005 .