By F. Lamnabhi-Lagarrigue, A. Lor´ıa, E. Panteley (Eds.)
"Advanced themes on top of things structures idea" includes chosen contributions written by way of academics on the moment (annual) Formation d’Automatique de Paris (FAP) (Graduate regulate tuition in Paris). it truly is addressed to graduate scholars and researchers on top of things concept with issues referring to various parts of curiosity to the keep watch over group corresponding to cascaded structures, flatness, optimum keep watch over, and Hamiltonian and infinite-dimensional platforms. The reader is supplied with a well-integrated synthesis of the newest considering in those topics with out the necessity for an exhaustive literature assessment. "Advanced subject matters up to the mark platforms conception" can be utilized to help both a one-term basic complex direction on nonlinear regulate idea, devoting a couple of lectures to every bankruptcy, or for extra concentrated and in depth classes at graduate point. The book’s concise yet pedagogical demeanour will supply a great begin to researchers wishing to expand their wisdom in facets of recent regulate concept outdoors their very own services.
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Additional info for Advanced Topics in Control Systems Theory: Lecture Notes from FAP 2004
Lor´ıa and E. Panteley 20. H. Khalil (2002) Nonlinear systems. , New York. 21. E. Koditschek (1987) Adaptive techniques for mechanical systems. In Proceedings 5th Yale Workshop on Adaptive Systems, pages 259–265, New Haven, CT. 22. I. Kolmanovsky and H. McClamroch (1995) Developments in nonholonomic control problems. Control systems magazine, pages 20–36. 23. M. Krsti´c, I. Kanellakopoulos, and P. Kokotovi´c (1995) Nonlinear and Adaptive control design. , New York. 24. J. Kurzweil (1956) On the inversion of Ljapunov’s second theorem on stability of motion.
P 47870, 21078 Dijon Cedex, France. org. The objective of this chapter is to describe geometric methods applied to aerospace systems: attitude control of a rigid spacecraft, orbital transfer, shuttle re-entry. We characterize the controllability of a rigid spacecraft controlled by one gas jet and the set of orbits reached in orbital transfer, depending upon the orientation of the thrust. Then we construct controls in orbital transfer and attitude control, using stabilization techniques and path planning.
Jabeur, and G. Janin • Shuttle re-entry: in this problem we are in the atmospheric part of the trajectory, the thrust is turned oﬀ and the shuttle behaves as a glider, the control being the lift force. There is also a drag force. The model is Kepler equation, with aerodynamic forces. The studied problems are not independent because: • The attitude control can be used to orientate the thrust in the orbital transfer. • In the re-entry problem, a preliminary part of the trajectory is an orbital transfer.
Advanced Topics in Control Systems Theory: Lecture Notes from FAP 2004 by F. Lamnabhi-Lagarrigue, A. Lor´ıa, E. Panteley (Eds.)