导航

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1988, Vol. 9 ›› Issue (6): 303-308.

• 论文 • Previous Articles     Next Articles

THE CORRECTION PRINCIPLE OF A SPRING BAR AND ITS APPLICATION TO THE MOMENT CONTROL SYSTEM

Liu Kunhua   

  1. No. 014 Centre of Aviation Ministry
  • Received:1987-08-20 Revised:1900-01-01 Online:1988-06-25 Published:1988-06-25

Abstract: It is necessary to study how a loaded object ( e.g. the actuator of an aircraft) affects the dynamic characteristics of a moment control system. This paper presents a correction principle by using a spring bar to the moment control system. By comparing theoretical data withexperimental ones, a basic method for selecting optimum spring bar is then given. It is necessary to study the special design priciples to extend the band-width of the system.