Entry Guidance for Hypersonic Glide Vehicles via Two-Phase hp-Adaptive Sequential Convex Programming

This paper addresses the real-time trajectory generation problem for hypersonic glide vehicles (HGVs) during atmospheric entry, subject to complex constraints including aerothermal limits, actuator bounds, and no-fly zones (NFZs). To achieve efficient and reliable trajectory planning, a two-phase hp...

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Veröffentlicht in:	Aerospace Jg. 12; H. 6; S. 539
Hauptverfasser:	Liu, Xu, Li, Xiang, Zhang, Houjun, Huang, Hao, Wu, Yonghui
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Basel MDPI AG 01.06.2025
Schlagworte:	Accuracy Actuators adaptive mesh refinement Algorithms Approximation Atmospheric entry Collocation methods Convex analysis Convexity Design and construction Efficiency entry guidance Error reduction Geometric constraints Gliding and soaring Grid refinement (mathematics) hypersonic glide vehicle Hypersonic planes Linear quadratic regulator Objective function Optimization Real time real-time trajectory optimization sequential convex programming Trajectory planning Vehicles China
ISSN:	2226-4310, 2226-4310
Online-Zugang:	Volltext
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