Hardware Design of Test System for Missile Flight Control System

Abstract:

Before final assembly and while debugging a missile, in order to ensure the flight control system can work stably and reliably, it is necessary to develop an auto test system for a general performance test, including electrical performance, inertial measurement device and navigation accuracy. After describing the composition and working principle of the flight control system, summarizing the test requirements, this paper puts forward to a test plan based on a industrial computer, introduces the hardware design and hardware anti-jamming techniques in detail. The test system with self-test function has been applied in testing the flight control system generally and reliably.

• Periodical: Applied Mechanics and Materials (Volumes 241-244)
• Pages: 9-13
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.241-244.9
• Online since: December 2012
• Authors: Dan Qiang Chen, Guo Hua Cao, Hui Lin Fan, Man Yi Hou, Jing Hua Wang
• Keywords: Flight Control System, Hardware Anti-Jamming Technique, Hardware Design, Test System

References

[1] Yongfei Huang and Xinjie Peng: The test technique of a missile's flight control system. Journal of Projectiles, Rockets, Missiles and Guidance, Vol. 29-1 (2011), pp.65-67.

[2] Liangliang Zhao, Mingqing Xiao, Zhihong Wang, Jinjun Cheng and Lian, Chen: Design and implementation of integrated test system for inertial navigation system and flight control system. Computer Measurement and Control, Vol. 19-3 (2011), pp.575-578.

[3] Zhanping Zhang, Jian Tao, Shanwei Hu and Xiaoming Qiu: Design of ARINC429 aviation communication bus based on HS3282. Aeronautical Computing Technique, Vol. 39-5 (2009), pp.107-110.

[4] Jianying Liu: Design of digital telemetry receiving device of a missile flight control system. Aero weaponry, No. 1 (2007), pp.57-61.

[5] Jianying Liu: The design and realization of the synthetical performance test system for a missile flight control assembley. Journal of Projectiles, Rockets, Missiles and Guidance, Vol. 27-5 (2007), pp.68-70.

[6] Yao Yang, Gangmin Wang and Yuelou Zhao: The design of test system for flight control computer based on LabVIEW. Electronic Measurement Technology, Vol. 32-9 (2009), pp.96-99.

[7] Feifei Zhao, Mengjun Tian and Zhen Li: Design of signal processing module of flight control system based on DSP. Mechinery and electronics, No. 4 (2010), pp.17-20.