导航

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1998, Vol. 19 ›› Issue (3): 365-370.

Previous Articles     Next Articles

STUDY OF COLLISION BETWEEN SERVO MECHANISM AND BOOSTER IN CONTROL SYSTEMS OF AIRCRAFT

Wang Yibing1, Wang Zhanlin2   

  1. 1. Qingdao University,Qingdao,266071;2. Faculty 303, Beijing University of Aeronautics and Astronautics,Beijing,100083
  • Received:1997-08-16 Revised:1998-01-20 Online:1998-06-25 Published:1998-06-25

Abstract:

Because of the slower response of a booster than that of a servomechanism, collision exists in the aircraft′s control system. It affects the performance and flight safety. The reason and originality are analysed. A mathematical model is built. By the example, the most effective parameters are found and the way to eliminate collision is also obtained. [WT5”HZ〗

Key words: mechanical control system, ser vomechanism, booster, collision

CLC Number: