SCIENCE CHINA Information Sciences, Volume 63 , Issue 2 : 124202(2020) https://doi.org/10.1007/s11432-018-9795-y

Thrust vectoring control of vertical/short takeoff and landing aircraft

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  • ReceivedNov 6, 2018
  • AcceptedFeb 18, 2019
  • PublishedJan 16, 2020


There is no abstract available for this article.


This work was supported by National Natural Science Foundation of China (Grant Nos. 61603210, 61673240) and Aeronautical Science Foundation of China (Grant No. 20160758001).


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  • Figure 1

    (Color online) THU-F35B, 3BSD nozzle and flight control structure. (a) The THU-F35B aircraft;protect łinebreak (b) 3BSD nozzle with deflection angle of 90 degrees;protect łinebreak (c) structure of the LTV MPC controller.