Hostname: page-component-cd9895bd7-p9bg8 Total loading time: 0 Render date: 2024-12-22T10:08:59.103Z Has data issue: false hasContentIssue false
  • English
  • Français

Constrained on-board attitude control using gas jet thrusters

Published online by Cambridge University Press:  04 July 2016

G. Radice  and
C. R. Mclnnes
G. Radice
Affiliation:
Department of Aerospace EngineeringUniversity of GlasgowGlasgow, UK
C. R. Mclnnes
Affiliation:
Department of Aerospace EngineeringUniversity of GlasgowGlasgow, UK
Get access Rights & Permissions [Opens in a new window]

Abstract

This paper analyses a new approach utilising potential functions to autonomously control constrained attitude slew manoeuvres using gas jet thrusters. The method hinges on defining a potential function from the geometric configuration of the satellite's current attitude, the final target attitude and any pointing constraint which may be present. It will be demonstrated that complex path shaping and planning can be achieved using little computational effort. The method is mathematically validated using Lyapunov's theorem, and so can be considered for safety critical applications.

Type
Research Article
Information
The Aeronautical Journal , Volume 103 , Issue 1030 , December 1999 , pp. 549 - 556
Copyright
Copyright © Royal Aeronautical Society 1999 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Barba, P.M. and Auburn, J.N. Satellite attitude acquisition by momentum transfer, AIAA J, October 1976, 14, pp 1382–1386.Google Scholar
2. Vadali, S.R. and Junkins, J.L. Spacecraft large angle rotational manoeuvres with optimal momentum transfer, J Astro Sci, April-June 1983, XXXI, (2), pp 217–235.Google Scholar
3. Olszweski, O.W.Automatedterminalguidanceforashuttle rendezvous to space station Freedom, AIAA Guidance, Navigation and Control Conference, AIAA, Washington DC, USA, 1990, pp 337-387.Google Scholar
4. Kumar, R.R. Artificial neural networks in space station optimal attitude control, IAF-92-0038, World Space Congress, Washington IX, USA, 1992.Google Scholar
5. McInnes, C.R. Potential function methods for autonomous spacecraft guidance and control, AAS/AIAA Astrodynamics Specialist Conference, Halifax, 1995.Google Scholar
6. McInnes, C.R. Large Angle slew manoeuvres with autonomous Sun vector avoidance, J Guid, Control and Dynamics, 1994,17, (4), pp 875–877.Google Scholar
7. McInnes, C.R. Autonomous control of constrained large angle attitude slews, Paper RAL.GS.58, 1st International Symposium on Reducing the Cost of Spacecraft Ground Systems and Operations, Rutherford Appleton Laboratory, Chilton, Oxfordshire, UK, 27-29 September 1995.Google Scholar
8. McInnes, C.R. Non-linear control for large angle attitude slew manoeu vres, ESA SP-381, 3rd ESA symposium on Guidance Navigation and Control system, ESTEC, Noordwijk, The Netherlands, 25-28 November 1996.Google Scholar
9. Borne, P. and Matrasov, V. The Lyapunov function methods and applications, IMACS Annals on Computing and Applied Mathematics, 1990.Google Scholar
10. Bertram, J.E. and Kalman, K.E. Control system analysis and design via the second method of Lyapunov, Trans ASME, 1960, pp 371–400.Google Scholar
11. Likins, P.W., Kane, T.R. and Levinson, D.A. Spacecraft Dynamics, McGraw-Hill Book Co, New York, 1983.Google Scholar
12. Wertz, J.R. and Larson, W.J. Space mission analysis and design, Dordrecht: Kluwer, 1991.Google Scholar