Title :
Ground test platform for attitude and orbit control system of small satellite
Author_Institution :
Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin, China
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;
Conference_Titel :
Mechatronics and Control (ICMC), 2014 International Conference on
Print_ISBN :
978-1-4799-2537-7
DOI :
10.1109/ICMC.2014.7231780
