具有修正机动的最优稳健二体弹道设计

IF 1.3 4区 工程技术 Q2 ENGINEERING, AEROSPACE Journal of Spacecraft and Rockets Pub Date : 2023-08-02 DOI:10.2514/1.a35725
Scott Kelly, D. Geller
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引用次数: 0

摘要

本文研究的重点是随机效应下脉冲传递轨迹的优化问题。介绍了一种考虑初始状态弥散正态分布并使标称脉冲[公式:见文]和[公式:见文]弹道修正机动(TCM)量级之和最小的弹道设计方法。提出了四个主要问题。首先,建立了确定性最优轨迹;在共面情况下,最优解为霍曼转移。对于第二个问题,引入了初始状态色散和目标位置色散约束。结果表明,修改名义双脉冲轨迹以满足色散约束是可能的。在第三个问题中,沿着确定性最优轨迹在最优点执行TCM,从而获得更有效的影响目标位置色散的方法。问题4是鲁棒轨迹的发展,其中标称脉冲机动和TCM[公式:见文本]同时优化。结果是一个不同的标称轨迹和TCM,它比问题3的总成本更便宜。利用数值传播的状态转移矩阵历史作为优化算法内部的一个步骤,沿着每个标称轨迹快速计算最优TCM。
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Optimal Robust Two-Body Trajectory Design with Corrective Maneuvers
The focus of this research is the optimization of impulsive transfer trajectories in the presence of stochastic effects. A trajectory design method is introduced that accounts for a normally distributed initial state dispersion and minimizes the sum of nominal impulsive [Formula: see text] plus [Formula: see text] trajectory correction maneuver (TCM) magnitude. Four main problems are presented. First, a deterministic optimal trajectory is developed; in the coplanar cases, the optimal solution is Hohmann transfer. For the second problem, an initial state dispersion and a target position dispersion constraint are introduced. It is shown to be possible to modify the nominal two-impulse trajectory to satisfy the dispersion constraint. In the third problem, a TCM is performed at the optimal point along the deterministic optimal trajectory, resulting in a more efficient method to influence the target position dispersion. Problem 4 is the development of a robust trajectory, where the nominal impulsive maneuvers and [Formula: see text] TCM [Formula: see text] are simultaneously optimized. The result is a different nominal trajectory and TCM that is less expensive than the total cost of problem 3. The optimal TCM is rapidly computed along each nominal trajectory using the numerically propagated state transition matrix history as a step inside the optimization algorithm.
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来源期刊
Journal of Spacecraft and Rockets
Journal of Spacecraft and Rockets 工程技术-工程:宇航
CiteScore
3.60
自引率
18.80%
发文量
185
审稿时长
4.5 months
期刊介绍: This Journal, that started it all back in 1963, is devoted to the advancement of the science and technology of astronautics and aeronautics through the dissemination of original archival research papers disclosing new theoretical developments and/or experimental result. The topics include aeroacoustics, aerodynamics, combustion, fundamentals of propulsion, fluid mechanics and reacting flows, fundamental aspects of the aerospace environment, hydrodynamics, lasers and associated phenomena, plasmas, research instrumentation and facilities, structural mechanics and materials, optimization, and thermomechanics and thermochemistry. Papers also are sought which review in an intensive manner the results of recent research developments on any of the topics listed above.
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