Jitter Control for Optical Payload on Satellites
Publication: Journal of Aerospace Engineering
Volume 27, Issue 4
Abstract
The jitter control technique by using dual-stage vibration isolation system for optical payload on satellites is discussed, and it is applied on a satellite to improve the imaging performance. The dual-stage vibration isolation system includes two vibration isolation platforms. The first vibration isolation platform is at the actuator disturbance source, like control moment gyroscopes (CMGs). The second one is installed between the top of the satellite bus and the optical payload. In this paper, the first step constructs a general satellite dynamic model including a dual-stage vibration isolation system, a cluster of CMGs and solar arrays by Newton-Euler method and Kane equations, while the validity of this dynamic model is verified by a computer software program. The transmissibility matrices from CMGs motion to satellite motion and that to optical payload motion are then obtained according to the simplified satellite dynamic model. The parameters constraint conditions of the vibration isolation platform for the CMGs are described, with its influence on the attitude control system analyzed. The third part selects the reasonable parameters of the dual-stage vibration isolation system and those of the flexible solar arrays. Then the frequency domain characteristics of the dual-stage vibration isolation system are presented. Finally, using these reasonable parameters, the performance of this vibration isolation system on the satellite is testified by numerical simulations.
Get full access to this article
View all available purchase options and get full access to this article.
References
Agrawal, B. (2009). “Jitter control for imaging spacecraft.” 4th Recent Advances in Space Technologies Int. Conf., IEEE, Piscataway, NJ.
Anderson, E., Trubert, M., Fanson, J., and Davis, P. (1991). “Testing and application of a viscous passive damper for use in precision truss structures.” AIAA/ ASME/ ASCE/ AHS/ASC Structures, Structural Dynamics, and Materials Conf., 32nd, AIAA, 2796–2808.
Babuska, V., Erwin, R. S., and Sullivan, L. A. (2003). “System identification of the SUITE isolation platform: Comparison of ground and flight experiments.” 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf., AIAA.
Basdogan, I., Grogan, R., Kissil, A., Sigrist, N., and Sievers, L. (2000). “Preliminary optical performance analysis of the space interferometer mission using an integrated modeling methodology.” Control of vibration and noise: New millenium, 109–117.
Baudoin, A., Boussarie, E., Damilano, P., Rim, G., and Caltagirone, F. (2002). “Pleiades: A multi mission and multi cooperative program.” Acta Astronautica, 51(1), 317–327.
Blaurock, C., Liu, A., Dewell, L., and Alexander, J. (2005). “Passive isolator design for jitter reduction in the terrestrial planet finder coronagraph.” SPIE Paper No. 5867-34, Conf.: Optical Modeling and Performance Precisions II, National Aeronautics and Space Administration.
Bronowicki, A. J. (2006). “Vibration isolator for large space telescopes.” J. Spacecraft Rockets, 43(1), 45–53.
Cobb, R. G., Sullivan, J. M., and Das, A. (1999). “Vibration isolation and suppression system for precision payloads in space.” Smart Mater. Struct., 8(6), 798–812.
Davis, L. P., Carter, D. R., and Hyde, T. T. (1995). “Second generation hybrid D-strut.” Smart Structures and Materials 1995: Passive Damping; Proc., Conf., Society of Photo-Optical Instrumentation Engineers, 161–175.
Davis, L. P., Cunningham, D., Bicos, A., and Enright, M. (1994a). “Adaptable passive viscous damper(an adaptable D-StrutTM).” Smart structures and materials 1994: Passive damping; Proc., Conf., SPIE, 47–58.
Davis, L. P., Cunningham, D., and Harrell, J. (1994b). “Advanced 1.5 Hz passive viscous isolation system.” 35th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf., AIAA.
Davis, L. P., Wilson, J. F., and Jewell, R. E. (1986). “Hubble space telescope reaction wheel assembly vibration isolation system.”, Structural Dynamics and Control Interaction of Flexible Structures, National Aerospace and Space Administration, Washington, DC, 669–690.
Davis, L. P., and Workman, B. J. (1992). “Design of a D-StrutTM and its application results in the JPL, MIT, and LaRC test beds.” AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf. 33rd, AIAA, 1524–1530.
Jin, L. (2008). “Study on attitude dynamics and control of spacecraft using angular momentum exchange devices.” Ph.D. thesis, Beihang Univ., Beijing.
Liu, K. C., and Maghami, P. (2008). “Reaction wheel disturbance modeling, jitter analysis, and validation tests for solar dynamics observatory.” AIAA Guidance, Navigation and Control Conf. and Exhibit, AIAA.
Mahboubkhah, M., Nategh, M. J., and Khadem, S. E. (2009). “A comprehensive study on the free vibration of machine tools’ hexapod table.” Int. J. Adv. Manuf. Technol., 40(11–12), 1239–1251.
Masterson, R. A. (1999). “Development and validation of empirical and analytical reaction wheel disturbance models.” Doctoral dissertation, Massachusetts Institute of Technology.
MATLAB [Computer software]. MathWorks, Natick, MA.
Miller, S. E., Kirchman, P., and Sudey, J. (2007). “Reaction wheel operational impacts on the GOES-N jitter environment.” AIAA Guidance, Navigation and Control Conf. and Exhibit, AIAA.
Oh, C. S., Lee, W., and Bang, H. (2006). “Passive jitter isolation for reaction wheel of satellites.” SICE-ICASE Int. Joint Conf., IEEE Computer Society.
Orlandea, N., Calahan, D. A., and Chace, M. A. (1977). “A sparsity-oriented approach to the dynamic analysis and design of mechanical systems-part 2.” J. Manuf. Sci. Eng., 99(3), 780–784.
Stubstad, J. M., Shoemaker, J. R., and Brooks, P. (1999). “The space technology research vehicle (STRV)-2 program development.” AIAA Space Technology Conf. & Exposition, Society of Photo-Optical Instrumentation Engineers, 1–9.
Sullivan, L. A., Fuentes, R. J., and Babuska, V. (2003). “On-orbit active vibration isolation: The satellite ultraquiet isolation technologies experiment(SUITE).” Space 2003, AIAA.
Zhang, Y., and Xu, S. (2011). “Vibration isolation platform for control moment gyroscopes on satellites.” J. Aerosp. Eng., https://doi.org/10.1061/(ASCE)AS.1943-5525.0000156, 641–652.
Information & Authors
Information
Published In
Copyright
© 2014 American Society of Civil Engineers.
History
Received: Feb 14, 2012
Accepted: Nov 6, 2012
Published online: Nov 8, 2012
Published in print: Jul 1, 2014
Discussion open until: Sep 18, 2014
Authors
Metrics & Citations
Metrics
Citations
Download citation
If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.