MODEL FOLLOWING RECONFIGURABLE FLIGHT CONTROL-SYSTEM FOR THE AFTI/F-16

被引：79

作者：

MORSE, WD ^{[1
]}

OSSMAN, KA ^{[1
]}

机构：

[1] OHIO STATE UNIV,ELECT ENGN,COLUMBUS,OH 43210

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1990年 / 13卷 / 06期

关键词：

D O I：

10.2514/3.20568

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

In the event of a control surface failure, the purpose of a reconfigurable flight control system is to redistribute and coordinate the control effort among the aircraft's remaining effective surfaces such that satisfactory flight performance is retained. In this paper, a model following reconfigurable flight control system designed for the AFTI/F-16 is discussed. The system utilizes an adaptive proportional plus integral controller with gain adjustment based on errors between desired performance and actual performance. Stability analysis and simulation results are presented.

引用

页码：969 / 976

页数：8

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