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Optimal control application in supersonic aircraft performance

 

作者: Ching-FangLin,  

 

期刊: IEE Proceedings D (Control Theory and Applications)  （IET Available online 1982）
卷期: Volume 129, issue 4  

页码: 113-117

 

年代: 1982

 

DOI:10.1049/ip-d.1982.0023

 

出版商: IEE

 

数据来源: IET

 

摘要:

Optimal control theory is used in the analysis of the three-dimensional turning performance of supersonic aircraft to generate real-time online optimal trajectories.

 

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