Research on Parameter Optimization Method of an Air Vehicle Gliding Trajectory
Fang Peng Wang, Yong Xu, Chun Ying Li · Advanced materials research · 2014
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%.