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变稳飞机结构谐振的抑制
引用本文:岳保康.变稳飞机结构谐振的抑制[J].飞行力学,1991(4):60-66.
作者姓名:岳保康
作者单位:618所
摘    要:本文介绍变稳飞机控制系统结构滤波器设计及结构谐振地面试验。通过试验,选择了合适的结构滤波器参数,有效地抑制了飞行控制系统与飞机弹性结构之间的耦合。

关 键 词:数字滤波器  稳定性  试验  飞机

RESTRAINT OF STRUCTURAL RESONANCE FOR VARIABLE STABILITY AIRCRAFT
Yue Baokang.RESTRAINT OF STRUCTURAL RESONANCE FOR VARIABLE STABILITY AIRCRAFT[J].Flight Dynamics,1991(4):60-66.
Authors:Yue Baokang
Institution:618 Research Institute Ministry of Aeronautic and Astronautic Industry
Abstract:This paper introduces the structural filter design of a variable stability aircraft control system and the ground test of structural resonance. Through ground test, suitable parameters of the structural filter are selected and the coupling between the flight control system and the aircraft elasticity structure is effectively restrained.
Keywords:digital filter  structural stability test  variable stability aircraft  
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