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Stability of dynamic inversion control laws applied to nonlinear aircraft pitch-axis models

 

作者: BLAISE MORTON,   DALE ENNS,   BING-YU ZHANG,  

 

期刊: International Journal of Control  （Taylor Available online 1996）
卷期: Volume 63, issue 1  

页码: 1-25

 

ISSN:0020-7179

 

年代: 1996

 

DOI:10.1080/00207179608921828

 

出版商: Taylor & Francis Group

 

数据来源: Taylor

 

摘要:

A global stability result is presented for nonlinear aircraft pitch-axis models with dynamic inversion control laws. The result is applied to the F-14 aircraft model. Using this result, we are able to sketch a stability region of the F-14 model in terms of the engine thrust and the selected pitch attitude.

 

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