{"title":"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","authors":"Changzhu Wei , Yankun Zhang , Jialun Pu , Feng Zhang","doi":"10.1016/j.ast.2025.111019","DOIUrl":null,"url":null,"abstract":"<div><div>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.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"168 ","pages":"Article 111019"},"PeriodicalIF":5.8000,"publicationDate":"2025-10-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Online entry trajectory planning with simultaneous constraints on terminal full-states, flight time and no-fly zones\",\"authors\":\"Changzhu Wei , Yankun Zhang , Jialun Pu , Feng Zhang\",\"doi\":\"10.1016/j.ast.2025.111019\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>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.</div></div>\",\"PeriodicalId\":50955,\"journal\":{\"name\":\"Aerospace Science and Technology\",\"volume\":\"168 \",\"pages\":\"Article 111019\"},\"PeriodicalIF\":5.8000,\"publicationDate\":\"2025-10-02\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerospace Science and Technology\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S127096382501082X\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S127096382501082X","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
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.
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.