Direct path method for flexible multibody spacecraft dynamics

Journal of Spacecraft and Rockets

Volumn 14, Issue 2, 1977, Pages 102-110

  Ho, J Y L ^a  

^a LOCKHEED MARTIN SPACE SYSTEMS COMPANY   (United States)

Author keywords

Spacecraft attitude dynamics and control

Indexed keywords

SPACECRAFT;

EID: 0017453675     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.57167     Document Type: Article

References (17)

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3. Hooker, W.W., "A Set of r Dynamical Attitude Equations for an Arbitrary n-Body Satellite Having r Rotational Degrees of Freedom," AIAA Journal, Vol. 8, July 1970, pp. 1205-1207.
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8. Likins, P.W., "Dynamics and Control of Flexible Space Vehicles," Tech. Rept. 32-1329 (Rev. I), 1970, Jet Propulsion Lab., Pasadena, Calif.
9. Likins, P.W. and Fleischer, G.E., "Results of Flexible Spacecraft Attitude Control Studies Utilizing Hybrid Coordinates," AIAA Paper 70-20, N.Y., 1970.
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11. Meirovitch, L., "Stability of Spinning Body Containing Elastic Parts via Liapunov’s Direct Method," AIAA Journal, Vol. 8, July 1970, pp. 1193-1200.
12. Seltzer, S., "Stabilizing a Spinning Skylab," 5th World Congress of IFAC, Paris, France, June 1972.
13. Kane, T.R. and Wang, C.F., "On the Derivation of Equations of Motion," Journal of the Society of Industrial and Applied Mathematics, Vol. 13, 1965.
14. Ho, J.Y.L., "The Direct Path Method for Deriving the Dynamic Equations of Motion of a Multibody Flexible Spacecraft with Topological Tree Configuration," LMSC Tech. Rept. D35-6977, June, 1973; also AIAA Paper 74-786, Aug. 1974.
15. Hooker, W.W., "Equations of Attitude Motion of a Topological Tree of Bodies, the Terminal Members of Which May Be Flexible," Technical Rept. LMSC-D354938, Nov. 1973, Lockheed Missiles and Space Company, Palo Alto, Calif.
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