Convex optimization of stochastic path-constrained trajectories near asteroids

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-08-08 DOI:10.1016/j.ast.2024.109463
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Abstract

The environment around asteroids is of significant uncertainties, which could cause great challenges of exploration missions to asteroids. This paper presents a novel approach to stochastic optimal problem in path-constrained trajectory optimization near asteroids based on convex approach. The path constraints that prevent the spacecraft from colliding with asteroid in different scenarios are composed of keep-out zone constraint and glide-slope constraint, which are formulated in chance-constraint forms due to the uncertain state. To convexify these constraints, the first-order Taylor expansion is applied for linearization and the nonconvexity is tackled with the introduction of additional intermediate variable and virtual buffer. Thereafter, a convex optimization based method is proposed to solve stochastic optimal problem. The effectiveness of the proposed method is validated through simulations of soft landing and hopping transfer scenarios near irregular-shaped asteroid 1996HW1. The results indicate that the proposed method can generate path-constrained trajectories under uncertainties using convex optimization.

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小行星附近随机路径受限轨迹的凸优化
小行星周围的环境具有很大的不确定性,这可能给小行星探测任务带来巨大挑战。本文提出了一种基于凸方法的小行星附近路径约束轨迹优化随机最优问题的新方法。防止航天器在不同情况下与小行星相撞的路径约束由远离区约束和滑行斜率约束组成,由于状态的不确定性,这些约束以偶然约束的形式提出。为了使这些约束条件凸性化,采用了一阶泰勒展开进行线性化,并通过引入额外的中间变量和虚拟缓冲区来解决非凸性问题。随后,提出了一种基于凸优化的方法来解决随机最优问题。通过模拟不规则形小行星 1996HW1 附近的软着陆和跳跃转移情况,验证了所提方法的有效性。结果表明,所提出的方法可以利用凸优化生成不确定情况下的路径受限轨迹。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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