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LAYOUT METHOD FOR AIRCRAFT ON THE FLIGHT DECK OF CARRIER USING NO-FIT POLYGON, 101-110.
Tiantian Luan and Mingxiao Sun
References
[1] G.Q. Xia, T.T. Luan, and M.X. Sun, Evaluation analysis for sortie generation of carrier aircrafts based on nonlinear fuzzy matter-element method, Journal of Intelligent & Fuzzy Systems, 31(6), 2016, 3055–3066.
[2] G.Q. Xia, T.T. Luan, and M.X. Sun, An evaluation method for sortie generation capacity of carrier aircrafts with principal component reduction and catastrophe progression method, Mathematical Problems in Engineering, 4, 2017, 1–10.
[3] G.Q. Xia, T.T. Luan, and M.X. Sun, Research on uncertain and nonlinear dynamic weapons dispatching system using fuzzy robust control, Proc. of International Conf. on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC- FSKD), Changsha, China, 2016, 1038–1043.
[4] T.T. Luan, M.X. Sun, G.Q. Xia, and D.D. Chen, Evaluation for sortie generation capacity of the carrier aircraft based on the variable structure RBF neural network with the fast learning rate, Complexity, 2018, 2018, 1–19.
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Abstract
DOI:
10.2316/J.2020.206-0222
From Journal
(206) International Journal of Robotics and Automation - 2020
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