Attitude Stability Criteria for Dual Spin Spacecraft von LIKINS, PETER W

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A study of attitude control concepts for precision-pointing nonrigid spacecraft / Peter W. Likins ; prepared by University of California, Los Angeles, Calif. for Marshall Space Fli... von Likins, Peter W

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Attitude stability criteria for dual spin spacecraft von LIKINS, PETER W

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Dynamics of flexible bodies in tree topology - A computer-oriented approach von SINGH, R. P, VANDERVOORT, R. J, LIKINS, P. W

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Dynamics of a multibody system with relative translation on curved, flexible tracks von LI, DECHANG, LIKINS, PETER W.

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Errata: Dynamics of a Multibody System with Relative Translation on Curved, Flexible Tracks von Li, Dechang, Likins, Peter W.

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Geometric stiffness characteristics of a rotating elastic appendage von Likins, Peter W

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Mathematical modeling of spinning elastic bodies for modal analysis von LIKINS, PETER W., BARBERA, FRANK J., BADDELEY, VICTOR

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Modal method for analysis of free rotations of spacecraft von LIKINS, PETER W

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Orthogonal Filters for Model Error Compensation in the Control of Nonrigid Spacecraft von Skelton, Robert E, Likins, Peter W

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Stability analysis of mechanical systems with constraint damping von LIKINS, PETER W

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Results of flexible spacecraft attitude control studies utilizing hybrid coordinates von LIKINS, PETER W, FLEISCHER, GERALD E

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Influence of flexible appendages on dual-spin spacecraft dynamics and control von GALE, AUSTIN H, LIKINS, PETER W

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Baffles to Suppress Energy Dissipation in Liquid-Filled Precessing Cavities von VANYO, JAMES P, LIKINS, PETER W

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Phase plane methods for toppling stability analysis of landing spacecraft von WILLIAMSON, DALE R, LIKINS, PETER W

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Erratum: "Comment on 'Equilibrium Orientations of Gravity-Gradient Satellites" von KANE, THOMAS R, LIKINS, PETER W

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Comment on "Equilibrium Orientations of Gravity-Gradient Satellites" von KANE, THOMAS R, LIKINS, PETER W

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Finite element appendage equations for hybrid coordinate dynamic analysis von Likins, Peter W.

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Effects of eddy-current damping on satellite attitude stability von LIKINS, PETER W, COLUMBUS, RICHARD L

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Stable Limit Cycles due to Nonlinear Damping in Dual-Spin Spacecraft von LIKINS, PETER W, TSENG, GAN-TAI, MINGORI, D. LEWIS

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