This study consisted of four parallel efforts: (1) modal analyses of elastic continua for Liapunov stability analysis of flexible spacecraft; (2) development of general purpose simulation equations for arbitrary spacecraft; (3) evaluation of alternative mathematical models for elastic components of spacecraft; and (4) examination of the influence of vehicle flexibility on spacecraft attitude control system performance. A complete record is given of achievements under tasks (1) and (3), in the form of technical appendices, and a summary description of progress under tasks two and four. (Author)
Modal Analysis for Liapunov Stability of Rotating Elastic Bodies
1973
220 pages
Report
Keine Angabe
Englisch
Interpretation of Liapunov stability regions.
AIAA | 1967
|Interpretation of Liapunov stability regions.
NTRS | 1967
|