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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2000, Vol. 21 ›› Issue (3): 267-269.

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APPLICATION OF NORMALIZED LCF H METHOE IN FLIGHT/PROPULSEON CONTROLLER DESIGN

ZHANG Li-jun,XIAO Ying-yue,CHENG Peng   

  1. Faculty 301, Beijing University of Aeronautics and Astronautics, Beijing, 100083, China
  • Received:1999-01-26 Revised:1999-11-14 Online:2000-06-25 Published:2000-06-25

Abstract:

This article designed a longitudinal flight/propulsion controller for flight control systems by using normalized left coprime factorization(normalized LCF) of robust theories and summarized some character and experience for the normalized LCF. The controller satisfied practical engineering requirements. The effect of the controller was good.

Key words: normalized left coprime fact or ization, r obust control, loop shaping

CLC Number: