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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1996, Vol. 17 ›› Issue (2): 251-255.

• 论文 • Previous Articles    

OPTIMAL DESIGN OF MECHANICAL CONTROL SYSTEM OF AIRCRAFT

Wang Yibing1, Wang Zhanlin2, Cui Jinbao2, Feng Yachang2   

  1. 1. Faculty 303 of Beijing University of Aeronautics and Astronautics,Beijing, 100083;2. Dept.of Science Research, Qingdao University, 266071
  • Received:1994-02-05 Revised:1995-01-14 Online:1996-04-25 Published:1996-04-25

Abstract: Without perfect design guidance, the work of MCS(Mechanical Control System)can not meet the first grade handling quality of the aircraft's specification in our country. The paper proposes an optimal design method which aims at the specification to construct design objects.Using this method, an aircraft's MCS is modified . All flying states go into the first grade handling quality of the specification.

Key words: transmission line, handling quality, optimal design

CLC Number: