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SCIENCE CHINA Information Sciences, Volume 64, Issue 3: 139201(2021) https://doi.org/10.1007/s11432-018-9582-6

Design of optimal trajectory transition controller for thrust-vectored V/STOL aircraft

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  • ReceivedJun 28, 2018
  • AcceptedAug 3, 2018
  • PublishedApr 14, 2020

Abstract

There is no abstract available for this article.


Acknowledgment

This work was supported by National Natural Science Foundation of China (Grant Nos. 61603210, 61673240).


References

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  • Figure 1

    (a) Computation process of the proposed method; (b) cost function values and cosine values of the original and proposed methods; (c) optimal trajectory controller structure.

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