Mathematical modeling and control of large space structures with multiple appendages-Reference-Cited by-同舟云学术

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Mathematical modeling and control of large space structures with multiple appendages

Published:1988 Issue:12 Volume:10 Page:891-900
ISSN:0895-7177
Container-title:Mathematical and Computer Modelling
language:en
Short-container-title:Mathematical and Computer Modelling

Author:

Ahmed N.U.,Biswas S.K.

Publisher

Elsevier BV

Subject

Computer Science Applications,Modelling and Simulation

Reference15 articles.

1. Equations of motion of flexible spacecraft;Grote;J. Spacecraft Rockets,1971

2. Influence of flexible appendages on dual spin spacecraft dynamics and control;Gale;J. Spacecraft Rockets,1970

3. The dynamical attitude equations for an n-body satellite;Hooker;J. astronaut Sci.,1965

4. Robust colocated control for large flexible space structures;Arbel;J. Guidance Control Dynam.,1981

5. Attitude control of flexible spacecraft;Martin;J. Guidance Control,1980

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3. Existence of solutions to strongly damped plate or beam equations;Boundary Value Problems;2012-07-20

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