Singular perturbation equations for flexible satellites

Author:

Huang T.C.,Das A.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials

Reference17 articles.

1. Thermoelastic flutter models for elements of flexible satellites;Huang;ACTA Astronautica,1975

2. Attitude dynamics of dual-spin satellites;Velman;Space Systems Division Research Report, Hughes Aircraft Co., SSD 60419R,1966

3. Attitude stability of dual-spin systems;Likins;Space Systems Research Report. Hughes Aircraft Co., SSD 60377R,1966

4. Use of synthetic modes in hybrid coordinate dynamic analysis;Likins;AIAA J.,1968

5. The analysis of interactions between attitude control systems and flexible appendages;Likins;Paper IAF AD29, 19th International Aeronautical Congress, New York,1968

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