Stabilization of a Satellite via Specific Optimum Control
- 1 July 1966
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Aerospace and Electronic Systems
- Vol. AES-2 (4), 446-449
- https://doi.org/10.1109/taes.1966.4501795
Abstract
The Optimum Stabilization of a tumbling satellite via Hamilton-Jacobi theory has been reported by one of the authors before in ¿On the optimum stabilization of a satellite¿ [2]. This companion paper discusses the synthesis of a specific optimum control law for the same problem and compares the results with the optimum solution. It is shown that a specific optimum control law yields, acceptable performance while being much easier to instrument than the optimum control law.Keywords
This publication has 2 references indexed in Scilit:
- On the Optimum Stabilization of a SatelliteIEEE Transactions on Aerospace and Electronic Systems, 1965
- On the identification of control systems by the quasi-linearization methodIEEE Transactions on Automatic Control, 1964