Event-Triggered Nonlinear Model-Predictive Control for Optimal Ascent Guidance

Recent decades have seen a surge in research on trajectory optimization (or optimal control) as a means of achieving computational guidance, which can be regarded as a nonlinear model-predictive guidance (NMPG) framework. Most of the existing NMPG methods are time-triggered and can be classified as...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems Jg. 60; H. 6; S. 7771 - 7784
Hauptverfasser:	Zhang, Tengfei, Gong, Chunlin, Zhang, Licong
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York IEEE 01.12.2024 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Accuracy Aerospace and electronic systems Algorithms Ascent Computational modeling Control systems design Guidance systems Mathematical models Monte Carlo simulation Nonlinear control Optimal control Optimization Orbits Predictive control Predictive models Trajectory optimization
ISSN:	0018-9251, 1557-9603
Online-Zugang:	Volltext
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