Solving orbit maintenance problems by the synthesis of evolution algorithms and traditional optimization methods

Solving orbit maintenance problems by the synthesis of evolution algorithms and traditional optimization methods

Orbit maintenance problems are solved by the synthesis of the traditional penalty function method and evolution algorithms (EAs). A general method is presented for the n-time impulse problem of orbit maintenance. The algorithm is proved to be effective according to a simulation example which adjusts...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Shi Wang, Shouyi Liao, Jinhai Dai
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Algebra
Constraint optimization
Control systems
Educational institutions
Engines
Mathematics
Optimization methods
Satellites
Space missions
Space technology
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Beschreibung
Zusammenfassung:Orbit maintenance problems are solved by the synthesis of the traditional penalty function method and evolution algorithms (EAs). A general method is presented for the n-time impulse problem of orbit maintenance. The algorithm is proved to be effective according to a simulation example which adjusts the semi-major axis with 3,4,5 impulse times.
DOI:10.1109/WCICA.2002.1020812