Modal Cost Analysis for Simple Continua

Author:

Hu A.,Skelton R. E.,Yang T. Y.

Publisher

Springer Berlin Heidelberg

Reference25 articles.

1. P. Likins 1977 Proceedings of the fourth Symposium of International Federation of Automatic Control on Multivariable Technological Systems, New Brunswick, N.B. Canada, July 1977. The Application of Multivariable Control Theory to Spacecraft Attitude Control.

2. M. Balas 1977 Symposium of American Institute of Aeronautics and Astronautics on Dynamics and Control of Large Flexible Spacecraft, Blacksburg, Virginia, U.S.A., June 1977. Active Control of Flexible Systems.

3. R. Skelton 1981 Theory and Applications of Optimal Control in Aerospace Systems (Chapter 8) ed. P. Kant, AGARD publication no. 251, KBN 92-835-1391-6, July 1981. Distributed in the United States, by NASA Langley Field, Virginia, 23365, attn: Report Distribution and Storage Unit. Control Design of Flexible Spacecraft.

4. R. Skelton, P. Hughes, and H. Hablani 1982 Journal of Guidance and Control 5(4) 351-357. Order Reduction for Models of Space Structures Using Modal Cost Analysis.

5. P. Hughes 1980 Journal of Applied Mechanics 47(1) 177-184. Modal Identities for Elastic Bodies with Application to Vehicle Dynamics and Control.

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1. Model reduction with weighted modal cost analysis;Guidance, Navigation and Control Conference;1990-08-17

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