TY - GEN
T1 - Research on modeling and simulation of satellite attitude control system
AU - Hu, Xiaoguang
AU - Li, Xiang
PY - 2014
Y1 - 2014
N2 - Satellite is a specific product with a 4-H characteristic: high-tech, high-cost, high-benefit and high-risk, which makes satellite difficult to develop. However, simulation technology has the potential to fix the problem. It is highly reliable, non-destructive and can be recycled regardless of the time and space. All the advantages enable the technology to provide an effective way to reduce the cost and risk of satellite production. The paper focuses on the modeling technology which is used for simulating satellite on-orbit performance and dynamic environment, thus it can provide a general simulation framework for test during the development of a satellite.
AB - Satellite is a specific product with a 4-H characteristic: high-tech, high-cost, high-benefit and high-risk, which makes satellite difficult to develop. However, simulation technology has the potential to fix the problem. It is highly reliable, non-destructive and can be recycled regardless of the time and space. All the advantages enable the technology to provide an effective way to reduce the cost and risk of satellite production. The paper focuses on the modeling technology which is used for simulating satellite on-orbit performance and dynamic environment, thus it can provide a general simulation framework for test during the development of a satellite.
UR - https://www.scopus.com/pages/publications/84906562442
U2 - 10.1109/ICCA.2014.6871014
DO - 10.1109/ICCA.2014.6871014
M3 - 会议稿件
AN - SCOPUS:84906562442
SN - 9781479928378
T3 - IEEE International Conference on Control and Automation, ICCA
SP - 744
EP - 749
BT - 11th IEEE International Conference on Control and Automation, IEEE ICCA 2014
PB - IEEE Computer Society
T2 - 11th IEEE International Conference on Control and Automation, IEEE ICCA 2014
Y2 - 18 June 2014 through 20 June 2014
ER -