一种进入飞行器机动能力分析与评价方法

Xing Wei, Yongji Wang, Lei Liu, QingXian Ge
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引用次数: 1

摘要

机动能力为进入飞行器的任务规划提供了重要信息。本文提出了一种生成进入阶段终点可达区域的方法,该方法描述了进入飞行器的全方向机动能力。该方法利用差分进化(DE)的并行特性和切比雪夫多项式插值的高精度,生成可达区域的一侧边界,而传统方法每次运行只能生成一个边界点。此外,为了评估车辆设计参数对机动能力的影响,提出了一种层次分析法(AHP)评分方法,大大减少了评估工作量。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A method for entry vehicle's maneuver capacity analysis and evaluation
Maneuver capacity provides crucial information for mission planning of entry vehicles. This paper proposes a method to generate the reachable area at the end points of the entry phase which describes the full directional maneuver capacity of the entry vehicles. This method utilizes the parallel characteristics of differential evolution (DE) and the high accuracy of Chebyshev polynomial interpolation to generate one side of the boundary of the reachable area, while conventional methods only generate one point of the boundary in each run. Furthermore, in order to assess the influence of the vehicle's design parameters on the maneuver capacity, a scoring method with analytic hierarchy process (AHP), which can greatly reduce the evaluation effort, is developed.
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