用于六自由度动力下降制导的自适应伪谱连续凸优化技术

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
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引用次数: 0

摘要

与三自由度动力下降相比,六自由度动力下降的非线性更强,因此其制导更具挑战性。标准的凸编程算法一直难以有效解决这一问题。为了从最优性和准确性两方面提高连续凸编程的性能,本文提出了一种自适应伪谱连续凸优化算法。首先,它通过将全局伪谱离散化与局部线性化相结合,将非线性最优控制问题转化为凸子问题。其次,本文提出了一种参数自适应连续凸化算法,该算法可根据最优轨迹的更新率自适应地调整信任区域的大小。最后,基于伪谱法精确计算了全局误差和局部误差。为解决非线性引起的局部误差过大问题,提出了一种自适应网格方法来细化网格。仿真结果证明了所提出的伪谱凸优化方法和自适应网格方法在减少局部误差和提高求解精度方面的有效性。此外,所提出的参数自适应连续凸优化算法在不同初始条件下表现出适应性和最优性,同时也提高了求解精度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Adaptive pseudospectral successive convex optimization for six-degree-of-freedom powered descent guidance

Guidance for six-degrees-of-freedom powered descent is more challenging due to its stronger nonlinearity compared to three-degrees-of-freedom. The standard convex programming algorithm has been difficult to effectively address this problem. To enhance the performance of successive convex programming in terms of both optimality and accuracy, an adaptive pseudospectral successive convex optimization algorithm is proposed in this paper. First, it transforms the nonlinear optimal control problem into a convex subproblem by integrating global pseudospectral discretization with local linearization. Second, a parameter-adaptive successive convexification algorithm is proposed, which adaptively adjusts the trust region size based on the update rate of the optimal trajectory. Last, the global error and local error are accurately calculated based on the pseudospectral method. To tackle the issue of excessively large local errors caused by nonlinearity, an adaptive grid method is proposed to refine the mesh grid. Simulation results demonstrate the efficacy of the proposed pseudospectral convex optimization method and adaptive mesh grid method in reducing local errors and improving solution accuracy. Furthermore, the proposed parameter-adaptive successive convex optimization algorithm exhibits adaptability and optimality across different initial conditions, while also improving solution accuracy.

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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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