Real-Time Lateral Predictor-Corrector Entry Guidance With Terminal Heading Angle Constraint

Predictor-corrector guidance (PCG) methods for entry flight are valued for their flexibility and adaptability. This study focuses on the lateral control of PCG with an added terminal heading angle constraint. Specifically, we propose a real-time lateral PCG algorithm that first achieves the online c...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems Jg. 61; H. 2; S. 2106 - 2119
Hauptverfasser:	Shi, Peng, Xu, Jingjing, Cheng, Lin, Dong, Changhong, Huang, Xu
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York IEEE 01.04.2025 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Aerodynamics Aerospace and electronic systems Algorithms Artificial neural networks Constraints Controllability Cooperative guidance entry guidance Flight heading coordination Heuristic algorithms Lateral control lateral guidance logic Prediction algorithms Predictor-corrector methods predictor–corrector guidance (PCG) Real time Real-time systems Sliding mode control terminal heading angle constraint Tracking errors Trajectories Trajectory Vehicle dynamics
ISSN:	0018-9251, 1557-9603
Online-Zugang:	Volltext
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