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Real-time entry guidance framework via an optimization-oriented quadratic programming formulation

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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Published online on

Abstract

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Ahead of Print.
Conventional entry guidance methods, including drag-profile-based approaches and predictor–corrector schemes, often require extensive parameter tuning and may fail to satisfy terminal conditions under extreme entry scenarios. This paper presents a real-...