P. W. Likins

发表

Influence of Flexible Appendages on Dual-Spin Spacecraft Dynamics and Control

A. H. Gale, P. W. Likins, 1970 .

Determination of poles and zeros of transfer functions for flexible spacecraft attitude control

Y. Ohkami, P. W. Likins, P. Likins, 1976 .

Stability analysis of mechanical systems with constraint damping.

P. W. Likins, P. Likins, 1967 .

A definition of the degree of controllability - A criterion for actuator placement

Richard W. Longman, P. W. Likins, P. Likins, 1979 .

Kinematics of rigid bodies in spaceflight

T. R. Kane, P. W. Likins, P. Likins, 1971 .

A definition of the degree of disturbance rejection

R. A. Laskin, R. W. Longman, P. W. Likins, 1982 .

An application of modern control theory to an elastic spacecraft

V. Larson, P. W. Likins, 1976 .

Nutation dampers vs precession dampers for asymmetric spinning spacecraft.

P. W. Likins, C. Schneider, Peter W. Likins, 1973 .

Results of flexible spacecraft attitude control studies utilizing hybrid coordinates

G. E. Fleischer, P. W. Likins, P. W. Likins, 1970 .

Constant and variable amplitude limit cycles in dual-spin spacecraft.

G. T. Tseng, P. W. Likins, D. L. Mingori, 1972 .

Large-deformation modal coordinates for nonrigid vehicle dynamics

P. W. Likins, P. Likins, G. Fleischer, 1972 .

A degree of controllability definition - Fundamental concepts and application to modal systems

Richard W. Longman, P. W. Likins, P. Likins, 1984 .