DocumentCode
3576018
Title
Ground test platform for attitude and orbit control system of small satellite
Author
Li Hua-Yi
Author_Institution
Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin, China
fYear
2014
Firstpage
1383
Lastpage
1387
Abstract
Ground test platform for attitude and orbit control system of small satellite is designed. Hardware interfaces between the real sensors/actuators and the onboard computer is simulated. Satellite dynamic and space environment is calculated in order to form a close-loop control system. Finally, the ground test system is validated by comparing the simulation result and in-orbit flying data.
Keywords
actuators; artificial satellites; attitude control; closed loop systems; control system synthesis; actuator; attitude control system; close-loop control system; ground test platform; hardware interface; onboard computer; orbit control system; satellite dynamic; space environment; Attitude control; Computational modeling; Computers; Orbits; Satellites; Sensors; Software; close-loop control; in-orbit flying experiment; simulators;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Control (ICMC), 2014 International Conference on
Print_ISBN
978-1-4799-2537-7
Type
conf
DOI
10.1109/ICMC.2014.7231780
Filename
7231780
Link To Document