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This work was supported by National Natural Science Foundation of China (Grant Nos. 61603210, 61673240).
[1] Bordignon K, Bessolo J. Control Allocation for the X-35B. In: Proceedings of Biennial International Powered Lift Conference and Exhibit, Virginia, 2002. 5--7. Google Scholar
[2] Dickeson J, Miles D, et al. Robust LPV H-inf gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of CG variations. In: Proceedings of the 46th IEEE Conference on Decision and Control, Louisiana, 2007. 2773--2778. Google Scholar
[3] Xili Y, Yong F, Jihong Z. Transition Flight Control of Two Vertical/Short Takeoff and Landing Aircraft. J Guidance Control Dyn, 2008, 31: 371-385 CrossRef ADS Google Scholar
[4] Banazadeh A, Taymourtash N. Optimal Control of an Aerial Tail Sitter in Transition Flight Phases. J Aircraft, 2016, 53: 914-921 CrossRef Google Scholar
[5] Agrawal S, Fabien B. Optimization of Dynamic Systems. Kluwer Academic, 1999, 1: 103--106. Google Scholar
[6] Fan Y, Meng X Y, Yang X L. Control allocation for a V/STOL aircraft based on robust fuzzy control. Sci China Inf Sci, 2011, 54: 1321-1326 CrossRef Google Scholar
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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