TRANSONIC AND SUPERSONIC LATERAL CONTROL OF AIRCRAFT BY ADAPTIVE PERFECT SERVO

被引：0

作者：

CHUBACHI, T

HASHIMOTO, A

机构：

[1] Iwate Univ, Morioka, Jpn, Iwate Univ, Morioka, Jpn

来源：

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 1986年 / 29卷 / 85期

关键词：

AERODYNAMICS - Buffeting - CONTROL SYSTEMS; ADAPTIVE - Synthesis - MATHEMATICAL TECHNIQUES - Transfer Functions - SERVOMECHANISMS;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A system is proposed which is a kind of adaptive tracking servo implying saturation of the internal signals in the transient state. The closed-loop transfer function is I//2 for this system, and hence the outputs follow the bounded arbitrary inputs without steady errors, if the system constitution is exact. The system is analogous to the so-called predifferential servo. This system is applied to transonic and supersonic flight control of the lateral system of an F4C figher aircraft. The simulation showed fairly good results.

引用

页码：121 / 133

页数：13