LPV modeling of atmospheric re-entry demonstrator for guidance re-entry problem

Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05

Volumn 2005, Issue , 2005, Pages 7422-7427

  Zerar, M ^a   Cazaurang, F ^a   Zolghadri, A ^a  

^a UNIVERSITÉ BORDEAUX 1   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC RE-ENTRY DEMONSTRATOR (ARD); ENTRY GUIDANCE SCHEME; LONGITUDINAL DYNAMICS; TRAJECTORY TRACKING ERROR;

COMPUTER SIMULATION; CONTROL THEORY; LINEAR SYSTEMS; MATHEMATICAL MODELS; PROBLEM SOLVING;

REENTRY;

EID: 33847217322     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/CDC.2005.1583359     Document Type: Conference Paper

References (15)

1. J. Pignié, P. Clar, E. Ferreira, L. Bouaziz and J. Caillaud. "Navigation, Guidance and Control of the Atmospheric Re-entry Demonstrator", in Pproc. 3rd ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, November 1996.
2. J.P. Arrington and J.J. Jones, Shuttle Performance: Lessons Learned, NASA Langley Research Center, 1983.
3. J. C. Harpold and C. A. Graves Jr, "Shuttle Entry Guidance", The Journal of the Astronautical Sciences, vol. XXVII, No. 3, pp. 239-268, July-September, 1979.
4. M. Fliess, J. Lévine, Ph. Martin, and P. Rouchon, "Flatness and defect of non-linear systems: introduction theory and examples", International Journal of Control, vol. 61(6), pp. 1327-1361, 1995.
5. M. Van Nieuwstadt and Richard M. Murray. "Real time trajectory generation for differentially flat systems". In Proc. IEEE Control and Decision Conference, pp 4224-4230, Dec 1995.
6. J. S. Shamma and J. Cloutier, "Gain-scheduled Missile Autopilot Design using Linear parameter varying transformations", Journal of guidance, Control, and dynamics, vol. 16, no 2, pp. 256-263, 1993.
7. ∞ controllers", Automatic Control, IEEE Transactions on, Volume: 40, Issue: 5, pp. 853-864. May 1995.
8. F. Wu and A. Packard, "LQG Control Design for LPV Systems", in Proc. American Control Conference, Vol. 6, June 1995, pp. 4440-4444.
9. N. X. Vinh, A. Busemann and R. D. Culp, Hypersonic and Planetary Entry Flight Mechanics The university of Michigan Press, Ann Harbor, 1980.
10. J. T. Betts, Practical methods for optimal control using nonlinear programming, SIAM, 2001.
11. th Aerospace Sciences Meeting, AIAA paper 70-28 - New York, 19-21 janvier 1970.
12. P. Rouchon, M. Fliess, J. Levine and P. Martin, "Flatness, motion planning and trailer systems", In: Proc. of the 32nd IEEE Conference on Decision and Control. San Antonio, Texas, pp. 2700-2705, 1993.
13. T. Neckel, C. Talbot and N. Petit, "Collocation and inversion for a reentry optimal control problem", Proc. of the 5th Intern. Conference on Launcher Technology. Madrid, Spain, 2003.
14. P. Rouchon, "Necessary condition and genericity of dynamic feedback linearization", J. Math. Systems Estim. Control, 5 (1995), pp. 345-358.
15. M. Zerar, F. Cazaurang, A. Zolghadri, "Robust tracking of nonlinear MIMO uncertain flat systems", in Proc. IEEE International Conference on Systems Man & Cybernetics. The Hague, The Netherlands, 2004.