Active system for vibration isolation of spacecraft instruments

Advances in the Astronautical Sciences

Volumn 92, Issue , 1996, Pages 465-479

  Anderson, Eric H ^b   Leo, Donald J ^b   Holcomb, Mark D ^a  

^a CSA ENGINEERING   (United States)

^b NONE

Author keywords

[No Author keywords available]

Indexed keywords

EID: 3242868174     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (6)

1. Sullivan, J., Hoffman, T., Das A., Davis, P., "Design of a 6 DOF Vibration Isolation System Using Hybrid D-Strut Technology," 19th Annual AAS Guidance and Control Conf., Breckenridge, CO, Feb., 1996, Paper No. 96-062.
2. Beard, A.M., von Flotow, A.H., and Schubert, D.W., "A Practical Product Implementation of an Active/Passive Vibration Isolation System," SPIE, July 1994.
3. Leo, D. L. and Anderson, E. H., "Comparison of Multi-Axis Active Vibration Isolation Architectures", ASME Winter Annual Meeting, San Francisco, November, 1995.
4. Johnson, C.D., and Kienholz, D.A., "Finite Element Prediction of Damping in Structures with Constrained Viscoelastic Layers," AIAA Journal, Vol. 20, No. 9, September 1982.
5. Integrated Engineering Software, 46-1313 Border Place, Winnipeg, Manitoba, Canada R3H 0X4.
6. Bronowicki, A.J., Innis, J.W., Casteel, S., Dvorsky, G., Alvarez, O.S., Rohleen, E., TRW Space and Technology Div., presented at the SPIE Conference on Smart Structures and Intelligent Systems, February 1994.