On the Optimum Stabilization of a Satellite
- 1 October 1965
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Aerospace and Electronic Systems
- Vol. AES-1 (2), 82-83
- https://doi.org/10.1109/taes.1965.4501667
Abstract
The problem of stabilizing a tumbling satellite prior to attitude control is discussed. The method of Hamilton-Jacobi theory is used to derive an explicit closed-loop control law for the problem.Keywords
This publication has 2 references indexed in Scilit:
- Time-, fuel-, and energy-optimal control of nonlinear norm-invariant systemsIEEE Transactions on Automatic Control, 1963
- Applied Dynamic ProgrammingPublished by Walter de Gruyter GmbH ,1962