基于终端全状态、飞行时间和禁飞区约束的在线入境轨迹规划

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Changzhu Wei , Yankun Zhang , Jialun Pu , Feng Zhang
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引用次数: 0

摘要

终端全状态约束、飞行时间约束和禁飞区约束的综合作用使得再入弹道规划成为一个高度欠驱动的规划问题,其中基于剖面的规划方法效率低下,分析方法难以满足多约束条件。为了实现对复杂约束的高适应性和低计算成本,本文提出了一种新的轨迹规划方法。该方法首先使用基于有向图的策略生成最优的禁飞区避开路径。随后,在路径上构建双层纵剖面,包括速度-高度子剖面和高度-距离-行驶子剖面。这种双剖面结构有利于分析满足终端对高度、速度和航迹角的约束。此外,通过切比雪夫多项式近似将飞行时间积分转化为快速的代数表达式,实现了显式和低成本的时间控制。针对横向轨迹生成问题,提出了一种基于纵剖面的岸反转时机优化方法,通过调整岸反转时机来满足纬度、经度和航向角等终端约束。数值仿真验证了该方法在复杂环境下高超声速滑翔飞行器弹道规划中的可行性和鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Online entry trajectory planning with simultaneous constraints on terminal full-states, flight time and no-fly zones
The integration of terminal full-state constraints, flight time constraints, and no-fly zone constraints makes the reentry trajectory planning a highly underactuated planning problem, where profile-based methods are inefficient and analytical methods struggle to satisfy multi-constraints. To achieve both high adaptability to complex constraints and low computation cost, this paper proposes a novel trajectory planning approach. The approach begins by generating an optimal no-fly-zone-avoiding path using a directed graph-based strategy. Subsequently, a dual-layer longitudinal profile is constructed upon the path, comprising a velocity-altitude sub-profile and an altitude versus range-to-go sub-profile. This dual-profile structure facilitates the analytical satisfaction of terminal constraints on altitude, velocity, and flight path angle. Furthermore, the flight time integral is transformed into a fast algebraic expression via Chebyshev polynomial approximation, enabling explicit and low-cost time control. For lateral trajectory generation, a method based on bank reversal timing optimization is developed with the use of the longitudinal profile, where terminal constraints on latitude, longitude, and heading angle are satisfied by adjusting bank reversal timing. Numerical simulations validate the feasibility and robustness of the proposed method for trajectory planning of hypersonic glide vehicles (HGVs) operating in complex environments.
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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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