Case Study #7: Satellite Reorientation Control

Robinett, Rush D.; Wilson, David G.

doi:10.1007/978-0-85729-823-2_12

Rush D. Robinett III³ &
David G. Wilson³

Part of the book series: Understanding Complex Systems ((UCS))

2144 Accesses

Abstract

Chapter 12 presents HSSPFC applied to a slewing spacecraft problem. The specific slewing spacecraft problem is a Multi-Input-Multi-Output (MIMO) three-axis spacecraft that employs Proportional-Integral-Derivative (PID) tracking control with numerical simulation results. This problem provides an interesting complication due to the three-axis rigid body rotation sequence.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Log in via an institution

Chapter: USD 29.95; Price excludes VAT (USA)

eBook: USD 129.00; Price excludes VAT (USA)

Softcover Book: USD 169.99; Price excludes VAT (USA)

Hardcover Book: USD 169.99; Price excludes VAT (USA)

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

References

Robinett III, R.D., Wilson, D.G.: Exergy and irreversible entropy production thermodynamic concepts for nonlinear control design. Int. J. Exergy 6(3), 357–387 (2009)
Google Scholar
Robinett III, R.D., Wilson, D.G.: Exergy and entropy thermodynamic concepts for control system design: slewing single axis. In: AIAA Guidance, Navigation, and Control Conference and Exhibit, Keystone, CO, August 2006
Google Scholar
Robinett III, R.D., Wilson, D.G.: Nonlinear slewing spacecraft control based on exergy, power flow, and static and dynamic stability. Journal of the Astronautical Sciences 57(4) (2009)
Google Scholar
Slotine, J.-J.E., Li, W.: Applied Nonlinear Control. Prentice Hall, Englewood Cliffs (1991)
MATH Google Scholar
Hughes, P.C.: Spacecraft Attitude Dynamics. Dover, New York (2004)
Google Scholar
Srivener, S.L., Thompson, R.C.: Survey of time-optimal attitude maneuvers. J. Guid. Control Dyn. 17(2), 225–233 (1994)
Article Google Scholar
Tsiotras, P.: Stabilization and optimality results for attitude control problem. J. Guid. Control Dyn. 9(4), 772–779 (1996)
Article Google Scholar
Subbarao, K.: Nonlinear PID-like controllers for rigid-body attitude stabilization. J. Astronaut. Sci. 52(1 and 2), 61–74 (2004)
MathSciNet Google Scholar
Tsiotras, P.: Further passivity results for the attitude control problems. IEEE Trans. Autom. Control 43(11), 1597–1600 (1998)
Article MathSciNet MATH Google Scholar
Cavallo, A., DeMaria, G.: Attitude control of large angle maneuvers. In: Proceedings of the IEEE Workshop Variable Structure Control, pp. 232–236 (1996)
Chapter Google Scholar
Vadali, S.R.: Variable-structure control of spacecraft large-angle maneuvers. AIAA Journal of Guidance, Control, and Dynamics 235–239 (1986)
Google Scholar
Robinett III, R.D., Parker, G.G.: Spacecraft Euler parameter tracking of large angle maneuvers via sliding mode control. J. Guid. Control Dyn. 19, 702–703 (1996)
Article MATH Google Scholar
Robinett III, R.D., Parker, G.G.: Least squares sliding mode control tracking of spacecraft large angle maneuvers. J. Astronaut. Sci. 45(4), 433–450 (1997)
Google Scholar
Singh, S.N.: Nonlinear attitude control of spacecraft. IEEE Trans. Aerosp. Electron. Syst. 23, 371–379 (1987)
Article Google Scholar
Tandale, M.D., Valasek, J.: Adaptive dynamic inversion control with actuator saturation constraints applied to tracking spacecraft maneuvers. J. Astronaut. Sci. 52(4), 517–530 (2004)
MathSciNet Google Scholar
Tewari, A.: Optimal nonlinear spacecraft attitude control through Hamiltonian–Jacobi formulation. J. Astronaut. Sci. 50(1), 99–112 (2002)
MathSciNet Google Scholar
Joshi, S.M., Kelkar, A.G., Wen, J.T.Y.: Robust attitude stabilization of spacecraft using nonlinear quaternion feedback. IEEE Trans. Autom. Control 40, 1800–1803 (1995)
Article MathSciNet MATH Google Scholar
Wie, B., Barba, P.M.: Quaternion feedback for spacecraft large angle maneuvers. J. Guid. Control Dyn. 3(3), 360–365 (1985)
Article Google Scholar
Dalsmo, M., Egeland, O.: State feedback H _∞-suboptimal control of a rigid spacecraft. IEEE Trans. Autom. Control 42, 1186–1189 (1997)
Article MathSciNet MATH Google Scholar
Kang, W.: Nonlinear control and its applications to rigid spacecraft. IEEE Trans. Autom. Control 40, 1281–1285 (1995)
Article MATH Google Scholar
Kristic, M., Tsiotras, P.: Inverse optimal stabilization of rigid spacecraft. IEEE Trans. Autom. Control 44, 1042–1049 (1999)
Article Google Scholar
Yang, C.D., Kung, C.C.: Nonlinear H _∞ flight control of general six degree-of-freedom motions. J. Guid. Control Dyn. 23(2), 278–288 (2000)
Article Google Scholar
Show, L.-L., Juang, J.-C., Jan, Y.-W.: An LMI-based nonlinear attitude control approach. IEEE Trans. Control Syst. Technol. 11(1), 73–83 (2003)
Article Google Scholar
Pacheco, R.P., Steffen, V. Jr.: Orthogonal function techniques for the identification of nonlinear mechanical systems. Mater. Sci. Forum 440–441, 59–68 (2003). Trans Tech Pubs, Switzerland
Article Google Scholar

Download references

Author information

Authors and Affiliations

Sandia National Laboratories, PO Box 5800, Albuquerque, NM, 87185, USA
Dr. Rush D. Robinett III & Dr. David G. Wilson

Authors

Dr. Rush D. Robinett III
View author publications
You can also search for this author in PubMed Google Scholar
Dr. David G. Wilson
View author publications
You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to David G. Wilson .

Rights and permissions

Reprints and permissions

Copyright information

About this chapter

Cite this chapter

Robinett, R.D., Wilson, D.G. (2011). Case Study #7: Satellite Reorientation Control. In: Nonlinear Power Flow Control Design. Understanding Complex Systems. Springer, London. https://doi.org/10.1007/978-0-85729-823-2_12

Download citation

DOI: https://doi.org/10.1007/978-0-85729-823-2_12
Publisher Name: Springer, London
Print ISBN: 978-0-85729-822-5
Online ISBN: 978-0-85729-823-2
eBook Packages: Physics and AstronomyPhysics and Astronomy (R0)

Publish with us

Policies and ethics