TY - GEN
T1 - Ground test platform for attitude and orbit control system of small satellite
AU - Hua-Yi, Li
N1 - Publisher Copyright:
© 2014 IEEE.
PY - 2015/8/31
Y1 - 2015/8/31
N2 - 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.
AB - 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.
KW - close-loop control
KW - in-orbit flying experiment
KW - simulators
UR - https://www.scopus.com/pages/publications/84953790374
U2 - 10.1109/ICMC.2014.7231780
DO - 10.1109/ICMC.2014.7231780
M3 - 会议稿件
AN - SCOPUS:84953790374
T3 - Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014
SP - 1383
EP - 1387
BT - Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - International Conference on Mechatronics and Control, ICMC 2014
Y2 - 3 July 2014 through 5 July 2014
ER -