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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Vydané v:	Aircraft Engineering and Aerospace Technology Ročník 79; číslo 2; s. 144 - 149
Hlavní autori:	Yuan, Ren, Pingyuan, Cui, Enjie, Luan
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Bradford Emerald Group Publishing Limited 30.01.2007
Predmet:	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
On-line prístup:	Získať plný text
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