By D. Schaechter, K.R. Lorell
A big, winning sector for keep an eye on structures improvement is that of state of the art aeronautical and house comparable applied sciences. best researchers and practitioners inside of this box were given the chance to switch rules and speak about effects on the IFAC symposia on automated keep watch over in aerospace. the main learn papers awarded on the most recent within the sequence were prepare during this book to supply a close review of current and destiny advancements of those regulate method applied sciences
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Extra info for Automatic Control in Aerospace 1994 (Aerospace Control '94). A Postprint Volume from the IFAC Symposium, Palo Alto, California, USA, 12–16 September 1994
BUCHARLES** * AEROSPATIALE, Aircraft Division, 316 route de Bayonne, 31060 Toulouse, **ONERA-CERT, 2 avenue Edouard Belin, 31400 Toulouse, France France Abstract. This paper discusses the design of a flight control system for a flexible aircraft, with significant coupling between flight mechanics and structural dynamics modes. Based on a longitudinal model, a normal acceleration control law is designed with a new synthesis technique, which is in fact a mixing of optimal control and eigenstructure assignment by means of constrained optimization.
5 1 8 - 5 2 5 . Zhukov, A. N. and V. N. Lebedev ( 1 9 6 4 ) . Variational Problem of Transfer Between Heliocentric Circular Orbits by Means of a Solar Sail. Translated from Kosmicheskie Issledovaniya, Vol. 2, No. 1, J a n - F e b , pp. 4 5 - 5 0 . Breakwell, J . V. and Η. E . Rauch ( 1 9 6 6 ) . Optim u m Guidance for a Low T h r u s t Interplanetary Vehicle. AIAA Journal, April, pp. 6 9 3 704. Bryson, A. E . J r . and Y . C. Ho ( 1 9 7 5 ) . Applied Optimal Control, Hemisphere, Washington. D C .
T R (9) R c =c Η ( τ ) is multiplied by e" x. The impulse response Thus : Ί Γ ( Τ ) . Β - χ= 7 Γ . τ Τ · ~ H l( t ) . H ( t ) ) . d t ' Thus G Q ax (14) (15) (11) b) The shape o f the eigenvectors associated with these eigenvalues can be altered. A total of m or r (whichever is smaller) elements of each eigenvector that can be altered can be chosen arbitrarily. (12) If it is desired to move an eigenvalue, the procedure consists in determining a gain matrix Κ such that for all desired closed-loop eigenvalue \ and eigenvector vj pairs It follows that: R = ~ B " 1.