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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1987, Vol. 8 ›› Issue (2): 105-109.

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PARAMETER OPTIMIZATION PROGRAM FOR THE DAMPED (STABILITY AUGMENTED) SYSTEM OF AIRCRAFTS

Feng Yachang, Suo jin   

  1. Beijing Institute of Aeronautics and Astronautics
  • Received:1985-03-16 Revised:1900-01-01 Online:1987-02-25 Published:1987-02-25

Abstract: This paper, presents a calculation Method of Powell optimization under certain constraints, which is specifically made and designed by authors. Then authors suggest a practical .. method which .. optimizes two parameters, a gain K and a time constant of washout. networkm In the damped (stability augmented) system (containing nonlinear links) of aircrafts by means of Powell optimization method according to level quality requirement . for MIL-F-8785C specifications under stick shift at sinusoidal signal input and aircraft fuselage . being instantly subjected to impulse wind.