Time-optimal memetic whale optimization algorithm for hypersonic vehicle reentry trajectory optimization with no-fly zones

被引:0
作者
Huiping Zhang
Honglun Wang
Na Li
Yue Yu
Zikang Su
Yiheng Liu
机构
[1] Beijing Institute of Technology,School of Automation
[2] Beijing Aerospace Automatic Control Institute,School of Automation Science and Electrical Engineering
[3] Beihang University,Science and Technology on Aircraft Control Laboratory
[4] Beihang University,undefined
[5] Unmanned System Research Institute,undefined
[6] Beihang University,undefined
来源
Neural Computing and Applications | 2020年 / 32卷
关键词
Trajectory optimization; Hypersonic vehicle; Whale optimization algorithm; Gauss pseudo-spectral method;
D O I
暂无
中图分类号
学科分类号
摘要
A novel time-optimal memetic whale optimization algorithm (WOA) integrating the Gauss pseudo-spectral methods (GPM), is proposed in this paper for the hypersonic vehicle entry trajectory optimization problem with no-fly zones. The WOA is featured with the strong global search ability and non-sensitive to the initial values, but also shows poor searching convergence speed around the global optimum. Conversely, GPM may be sensitive to the initial solution and easily trapped in a local optimum, but it also possesses more rapid convergence speed around the optimum and higher searching accuracy. Thus, a memetic optimization algorithm which contains a two-stage approach mechanism is proposed for searching the global optimum. The first searching stage, which is driven by an improved WOA (IWOA), works as an initializer of the entire searching due to its strong global search ability and non-sensitive to the initial values. The local optimum reservation and adaptive amplitude factor updating strategy are established to improve the convergent speed and the global search ability of the WOA. Once the changing of fitness value satisfies the predefined criterion, the next searching stage driven by GPM will take the place of the IWOA to expedite the search process around optimum and to obtain a precise global optimal solution. By this hybrid way, the proposed optimization algorithm may find an optimum more quickly and accurately. Simulation results show the proposed algorithm possesses faster convergence speed, higher accuracy, and stronger robustness for the hypersonic vehicle entry trajectory optimization.
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页码:2735 / 2749
页数:14
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