@inproceedings{8927789e05464dbf95c5648e2f692edf,
title = "Research on parameter optimization method of an air vehicle gliding trajectory",
abstract = "A mathematical model of air vehicle gliding trajectory was established and attack angle was regarded as control variable. Adaptive simulated annealing algorithm was adopted to optimize the 101 nodes of attack angle. By optimizing the control law of attack angle of gliding trajectory, the maximum range of air vehicle is increased significantly, which increases 107\%.",
keywords = "Adaptive simulated annealing algorithm, Air vehicle, Parameter optimization, Trajectory",
author = "Wang, \{Fang Peng\} and Yong Xu and Li, \{Chun Ying\}",
year = "2014",
doi = "10.4028/www.scientific.net/AMR.945-949.662",
language = "English",
isbn = "9783038351221",
series = "Advanced Materials Research",
publisher = "Trans Tech Publications Ltd.",
pages = "662--665",
booktitle = "Advances in Manufacturing Science and Engineering V",
address = "Switzerland",
}