C. S. Bodley

发表

Literature Review : DYNAMIC STABILITY ANALYSIS BY THE CONJUGATE GRADIENT METHOD Rubinstein, M. F. and Roberts, T. A. J. Franklin Inst. 293 (3), 173-189 (Mar. 1972) 9 refs Refer to Abstract No. 72-1044

C. S. Bodley, 1973 .

Dynamic analysis of a flexible spacecraft with rotating components. Volume 2: Program guide and examples

C. S. Bodley, A. C. Park, A. D. Devers, 1975 .

Tethered satellite system dynamics and control

C. S. Bodley, B. Cibrario, B. Musetti, 1990 .

Dynamic analysis of a flexible spacecraft with rotating components. Volume 1: Analytical developments

C. S. Bodley, A. C. Park, A. D. Devers, 1975 .

Response of flexible space vehicles to docking impact. Volume 2 - Numerical investigation

C. S. Bodley, A. C. Park, 1970 .

Response of flexible space vehicles to docking impact. Volume 1 - Analytical investigation, 4 April 1968 - 3 March 1970

C. S. Bodley, A. C. Park, 1970 .

Dynamic analysis of a flexible spacecraft with rotating components. Volume 3: Program code

C. S. Bodley, A. C. Park, A. D. Devers, 1975 .

Dynamic response and stability analysis of flexible, multibody systems. [spacecraft]

C. S. Bodley, A. C. Park, H. P. Frisch, 1977 .

A digital computer program for the dynamic interaction simulation of controls and structure (DISCOS), volume 2

C. S. Bodley, A. C. Park, H. P. Frisch, 1978 .

Computer program system for dynamic simulation and stability analysis of passive and actively controlled spacecraft. Volume 2: Program user's guide

C. S. Bodley, D. A. Devers, C. A. Park, 1975 .