A low-thrust guidance law based on Lyapunov feedback control and hybrid genetic algorithm

Purpose - This paper seeks to examine the development of the on-board guidance law for multi-revolutions orbit transfer spacecraft with low-thrust propulsion systems.Design methodology approach - In the research, first, a set of equinoctial elements is utilized to avoid the singularities in dynamica...

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Veröffentlicht in:	Aircraft Engineering and Aerospace Technology Jg. 79; H. 2; S. 144 - 149
Hauptverfasser:	Yuan, Ren, Pingyuan, Cui, Enjie, Luan
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Bradford Emerald Group Publishing Limited 30.01.2007
Schlagworte:	Algorithms Control systems Control theory Efficiency Feedback Feedback control Genetic algorithms Guidance (motion) Liapunov functions Performance enhancement Performance indices Propulsion system design Singularities Spacecraft Spacecraft guidance Stationkeeping Studies Trajectory optimization China Feedback Algorithmic languages
ISSN:	1748-8842, 0002-2667, 1758-4213
Online-Zugang:	Volltext
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