Features of space solar power station control system

The article is devoted to the creation of a control system for the orbital segment of a space solar power station and the main principles of its creation. The simulation of the functioning of a demonstrational space solar power station operating in an elliptical orbit with the energy transfer in low...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Acta astronautica Jg. 158; S. 111 - 120
Hauptverfasser: Yermoldina, G.T., Suimenbayev, B.T., Sysoev, V.K., Suimenbayeva, Zh.B.
Format: Journal Article
Sprache:Englisch
Veröffentlicht: Elmsford Elsevier Ltd 01.05.2019
Elsevier BV
Schlagworte:
Computer simulation
Control system
Control systems
Elliptical orbits
Energy transfer
High-precision guidance
Low altitude
Modeling
Orbit
Power plants
Solar energy
Solar generators
Solar power
Spacecraft
AB
DSSPS
Orbit
SSPS
Control system
Spacecraft
High-precision guidance
LV
BM
Modeling
BCCS
SB
SHF
PAA
RC
Energy transfer
EC
ISSN:0094-5765, 1879-2030
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:The article is devoted to the creation of a control system for the orbital segment of a space solar power station and the main principles of its creation. The simulation of the functioning of a demonstrational space solar power station operating in an elliptical orbit with the energy transfer in low orbit sections has been conducted and a high-precision control of the spacecraft at low altitudes has been considered. The result of the performed studies is the computational confirmation of the capabilities of the measuring, calculation and orientation to provide the required accuracy of the spacecraft orientation for demonstrating the energy transfer from orbit to the receiver system. The obtained results give grounds for the construction of a demonstrational space solar power station in the low orbit. •The demonstration space experiment is necessary in realizing the idea of SSPS.•The main task is to accurately guide the channel of energy transfer to the rectenna.•The experiment involves the placement of energy reception points in Kazakhstan.•The pointing accuracy of energy transfer device is no more than 1.5 angular seconds.•To improve accuracy, it is advisable to switch to more precise measuring instruments.
Bibliographie:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:0094-5765
1879-2030
DOI:10.1016/j.actaastro.2018.04.001