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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Bibliographic Details
Main Authors:	Xu Liu, Xiang Li, Houjun Zhang, Hao Huang, Yonghui Wu
Format:	Article
Language:	English
Published:	MDPI AG 2025-06-01
Series:	Aerospace
Subjects:	hypersonic glide vehicle entry guidance sequential convex programming adaptive mesh refinement real-time trajectory optimization
Online Access:	https://www.mdpi.com/2226-4310/12/6/539
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Entry Guidance for Hypersonic Glide Vehicles via Two-Phase hp-Adaptive Sequential Convex Programming

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