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Attitude Dynamics and Control of Liquid Filled Spacecraft with Large Amplitude Fuel Slosh

Published online by Cambridge University Press:  15 July 2016

M.-L. Deng  and
B.-Z. Yue
M.-L. Deng
Affiliation:
Department of MechanicsSchool of Aerospace EngineeringBeijing Institute of TechnologyBeijing, China
B.-Z. Yue*
Affiliation:
Department of MechanicsSchool of Aerospace EngineeringBeijing Institute of TechnologyBeijing, China
*
*Corresponding author ([email protected])
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Abstract

This paper focuses on the attitude dynamics and control of liquid filled spacecraft, and the large amplitude fuel slosh dynamics is included by using an improved moving pulsating ball model. The moving pulsating ball model is an equivalent mechanical model that is capable of imitating the whole liquid reorientation process, specifically for the occurrence of large amplitude slosh. This model is improved by incorporating a static capillary force and an effective mass factor. The improvements on this model are validated with previously published experiment results. The spacecraft attitude maneuver is implemented by the momentum transfer technique, and the feedback control strategy is designed based on Lyapunov theory. The effects of liquid viscosity, tank location and desired steady time on sloshing torque and control torque are investigated. The attitude control strategy applied in this paper is proved to be applicable for the coupled liquid filled spacecraft system. The obtained conclusions are useful to aid in liquid filled spacecraft overall design.

Keywords

Liquid filled spacecraftAttitude maneuverLarge amplitude liquid sloshThe moving pulsating ball model
Type
Research Article
Information
Journal of Mechanics , Volume 33 , Issue 1 , February 2017 , pp. 125 - 136
Copyright
Copyright © The Society of Theoretical and Applied Mechanics 2017 

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References

1. Reyhanoglu, M., “Maneuvering Control Problems for a Spacecraft with Unactuated Fuel Slosh Dynamics,” IEEE Control Systems, 1, pp. 695–699 (2003).Google Scholar
2. Yue, B. Z. and Zhu, L. M., “Hybrid control of liquid filled spacecraft maneuver by dynamic inversion and input shaping,” AIAA Journal, 52, pp. 618–626 (2014).Google Scholar
3. Ahmad, S., Yue, B. Z., Shah, S. F. and Ahmad, S., “Hamilton Structure and Stability Analysis for a Partially Filled Container,” Journal of Mechanics, 29, pp. 79–83 (2012).CrossRefGoogle Scholar
4. Kang, J. Y. and Lee, S., “Attitude acquisition of a satellite with a partially filled liquid tank,” Journal of Guidance Control and Dynamics, 31, pp. 790–793 (2008).CrossRefGoogle Scholar
5. Thomas, S. S., Kang, J. Y. and Victoria, L. C., “Analytical control law for spacecraft reorientation via Lyapunov theory,” AIAA Guidance, Navigation and Control Conference, Canada (2010).Google Scholar
6. Yang, D. D., Yue, B. Z., Wu, W. J., Song, X. J. and Zhu, L. M., “Attitude maneuver of liquid-filled spacecraft with a flexible appendage by momentum wheel,” Acta Mechanica Sinica, 28, pp. 543–550 (2012).CrossRefGoogle Scholar
7. Berry, R. L. and Tegart, J. R., “Experimental study of transient liquid motion in orbiting spacecraft,” NASA Report, NASA-CR-144213 (1976).Google Scholar
8. Dodge, F. T., “The New Dynamic Behavior of Liquids in Moving Containers,” NASA Report, SP-106 (2000).Google Scholar
9. Vreeburg, J. P. B. and Chato, D. J., “Models for Liquid Impact Onboard Sloshsat FLEVO,” AIAA Space 2000 Conference and Exposition, U.S. (2000).Google Scholar
10. Vreeburg, J. P. B., “Dynamics and control of a spacecraft with a moving pulsating ball in a spherical cavity,” Acta Astronautics, 40, pp. 257–274 (1997).CrossRefGoogle Scholar
11. Monti, R., Physics of Fluids in Microgravity, Taylor and Francis Publishers, London, pp. 293–321 (2002).CrossRefGoogle Scholar
12. Vreeburg, J. P. B., “Acceleration measurements on Sloshsat FLEVO for liquid force and location determination,” Technic Report, NLR-TP-2000-062, National Aerospace Laboratory, Netherland (2000).Google Scholar
13. Vreeburg, J. P. B., “Measured States of Sloshsat FLEVO,” 56th International Astronautical Congress, Japan (2005).Google Scholar
14. Vreeburg, J. P. B., “Free Motion of an Unsupported Tanks that is Partially Filled with Liquid,” Microgravity Fluid Mechanics, 92, pp. 519–528 (1992).CrossRefGoogle Scholar
15. Ibrahim, R. A., Liquid sloshing dynamics theory and applications, Cambridge University Press, Cambridge, pp. 752–762 (2005).CrossRefGoogle Scholar
16. Veldman, A. E. P., Gerrits, J., Luppes, R., Helder, J. A. and Vreeburg, J. P. B., “The numerical simulation of liquid sloshing on board spacecraft,” Journal of computational physics, 224, pp. 82–99 (2007).CrossRefGoogle Scholar
17. Luppes, R., Helder, J. A. and Veldman, A. E. P., “Liquid Sloshing in Microgravity,” 56th International Astronautical Congress, Japan (2005).Google Scholar
18. Yang, D. D. and Yue, B., “Attitude manoeuver of spacecraft with long cantilever beam appendage by momentum wheel,” International Journal of control, 86, pp. 360–368 (2013).CrossRefGoogle Scholar