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SCIENCE CHINA Information Sciences, Volume 62, Issue 5: 050212(2019) https://doi.org/10.1007/s11432-018-9683-y

Disturbance observer-based optimal longitudinal trajectory control of near space vehicle

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  • ReceivedAug 14, 2018
  • AcceptedNov 7, 2018
  • PublishedFeb 26, 2019

Abstract

There is no abstract available for this article.


Acknowledgment

This work was supported by Aeronautical Science Foundation of China (Grant No. 20165752049) and Natural Science Foundation of Jiangsu Province (Grant No. BK20171417).


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