TY - GEN
T1 - High frequency vibration isolation of control moment gyroscope on satellites
AU - Zhang, Yao
AU - Xu, Shijie
PY - 2010
Y1 - 2010
N2 - The high frequency vibration isolation of Control Moment Gyroscopes on satellites is discussed in this paper. Firstly, the theory of vibration isolator is presented and the reason of choosing correlative parameters is explained. Then an integrated satellite dynamic model including vibration isolation platform and pyramid configuration CMGs is proposed. The influence of the vibration isolation system to the attitude control system of the satellite is also analyzed. The validity of the dynamic model of the vibration isolation platform is then verified by using the commercial software, Adams. Finally the ameliorative effect of vibration isolation device to the satellite attitude stabilization is testified by integrated simulation.
AB - The high frequency vibration isolation of Control Moment Gyroscopes on satellites is discussed in this paper. Firstly, the theory of vibration isolator is presented and the reason of choosing correlative parameters is explained. Then an integrated satellite dynamic model including vibration isolation platform and pyramid configuration CMGs is proposed. The influence of the vibration isolation system to the attitude control system of the satellite is also analyzed. The validity of the dynamic model of the vibration isolation platform is then verified by using the commercial software, Adams. Finally the ameliorative effect of vibration isolation device to the satellite attitude stabilization is testified by integrated simulation.
UR - http://www.scopus.com/inward/record.url?scp=79959471561&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:79959471561
SN - 9781617823688
T3 - 61st International Astronautical Congress 2010, IAC 2010
SP - 8444
EP - 8452
BT - 61st International Astronautical Congress 2010, IAC 2010
T2 - 61st International Astronautical Congress 2010, IAC 2010
Y2 - 27 September 2010 through 1 October 2010
ER -