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1980
DOI: 10.1016/0094-5765(80)90011-9
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General dynamics of a large class of flexible satellite systems

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Cited by 17 publications
(6 citation statements)
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“…1). The reason why the I model predicts such a "good" energy drift is because it contains the elastic configuration dependence in the mass matrix given in (15). Indeed, without these terms, the value of e^ R^S increases to 23.8 with no discernible difference in the simulation results.…”
Section: T I F> 15smentioning
confidence: 97%
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“…1). The reason why the I model predicts such a "good" energy drift is because it contains the elastic configuration dependence in the mass matrix given in (15). Indeed, without these terms, the value of e^ R^S increases to 23.8 with no discernible difference in the simulation results.…”
Section: T I F> 15smentioning
confidence: 97%
“…They are defined analogously to equations (13) and (14) with: 8c " = 2 P"a?"" a=l a=l 8H""= 2 v" "p^"p (15) We observe that the argument of the second summation in (15^) is a quadratic function of elastic variables q^^. Its inclusion is necessary to preserve the positive-definiteness of the augmented inertia matrix.…”
Section: (7)mentioning
confidence: 99%
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“…The writings of Bainum and Kumar (1982), Diarra and Bainum (1987), Dubowsky and Sunada (1982), Hale and Meirovitch (1982), Ho and Herber (1985), Hughes (1979), Huston (1980Huston ( , 1981, Ibrahim and Modi (1986), Kane, Ryan, and Banerjee (1987), Levinson (1982), Likins (1975), Lips and Modi (1980), Rajaram and Junkins (1985), Rosen, Loewy and Mathcw (1987), Shabana (1985), Wu, Haug, and Kim (1989), and of Yoo and Haug (1986) represent a sampling of this research.…”
Section: Flexible Multibody Systemsmentioning
confidence: 97%
“…Problems of the aerospace industry and robotics stimulate the development of new methods for mathematical modeling and control design for complex mechanical systems with elastic elements. In particular, it is a well-known fact that the vibrations of flexible parts of satellites influence significantly their dynamics, so that a rigid body model is not acceptable in stability and control investigations for such distributed parameter systems (see, e.g., [2,11,14]). This brings the motivation for studying the controllability and stabilization issues for infinite-dimensional mathematical models of flexible structures with strings, beams, and plates.…”
Section: Introductionmentioning
confidence: 99%