Robust multivariable control of rotorcraft in forward flight

被引:20
|
作者
Rozak, JN
Ray, A
机构
关键词
D O I
10.4050/JAHS.42.149
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents the synthesis and analysis of multivariable robust control systems for a UH-60 Black Hawk helicopter in forward flight based on the ADS-33C specification and the Structured Singular Value (mu) analysis, Several robust controllers with different configurations (e.g., a rate or attitude command, 3 or 4-axis design) were constructed to determine which configuration provides the best overall handling qualities performance. It was determined that the Rate Command 3-axis, designed with an ideal model structure, yielded the best overall performance.
引用
收藏
页码:149 / 160
页数:12
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