Aircraft pitch and heave rate control

被引：1

作者：

Whalley, R ^{[1
]}

Ebrahimi, RI ^{[1
]}

机构：

[1] Univ Bradford, Dept Mech & Med Engn, Bradford BD7 1DP, W Yorkshire, England

来源：

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | 2000年 / 214卷 / G1期

关键词：

aircraft; pitch; heave; control; feedback;

D O I：

10.1243/0954410001531872

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The dynamic model of a high-performance military aircraft is considered. An input-output representation relating the open-loop pitch and heave rate characteristics to elevator movement is derived. Effective closed-loop design techniques are invoked. Simulated response transients are presented.

引用

页码：1 / 8

页数：8