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Simulation of Control and Guidance System for the Spinning Missile
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作者 Meng Daikui (China Changfeng System Engineering Corporation, P.O.Box 142-30, Beiging 100854, China) 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 1994年第3期49-56,共8页
Adopted for some small-size short range surface-to-air missiles and antitank guided missiles is a single-channel control method of making missile rotating around its longitudinal axis. In hardware-in-the-loop simulati... Adopted for some small-size short range surface-to-air missiles and antitank guided missiles is a single-channel control method of making missile rotating around its longitudinal axis. In hardware-in-the-loop simulations of the guidance and control system for these kinds of spinning missiles, improper use of special simulation equipment and test method will cause significant errors, even lead to failure of the simulation. In this article, the author gives an analysis of the causes of significant errors and failure of the simulation, and puts forward a solution, which is improved workable in making the hardward-in-the-loop simulation successful. 展开更多
关键词 computer simulation Error analysis computer system recovery Missiles
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