Planning Allocation for GTO-GEO Transfer Spacecraft with Triple Orthogonal Gimbaled Thruster Boom

This paper proposes an electric propulsion platform based on a triple orthogonal gimbaled thruster boom to realize the GTO-GEO transfer process. The adjustment mechanism of the gimbaled thruster boom significantly improves the range of thrust vector variation enhances the efficiency of thrust vector...

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Veröffentlicht in:Mathematics (Basel) Jg. 11; H. 13; S. 2844
Hauptverfasser: Ma, Guangfu, Kong, Xianglong
Format: Journal Article
Sprache:Englisch
Veröffentlicht: Basel MDPI AG 01.07.2023
Schlagworte:
Aerospace engineering
Algorithms
Artificial satellites
Efficiency
Electric propulsion
Energy consumption
GTO-GEO transfer process
Mathematical models
model predictive algorithm
Numerical analysis
planning allocation
Robotics
Satellites
Simulation methods
Spacecraft
Spacecraft propulsion
Thrust
triple orthogonal gimbaled thruster boom
ISSN:2227-7390, 2227-7390
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Beschreibung
Zusammenfassung:This paper proposes an electric propulsion platform based on a triple orthogonal gimbaled thruster boom to realize the GTO-GEO transfer process. The adjustment mechanism of the gimbaled thruster boom significantly improves the range of thrust vector variation enhances the efficiency of thrust vector adjustment, and reduces the spacecraft burn-up. Additionally, to achieve the application performance, a planning allocation method based on the model prediction algorithm is proposed and verified through numerical simulation.
Bibliographie:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
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ISSN:2227-7390
2227-7390
DOI:10.3390/math11132844