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.
On the Optimum Stabilization of a Satellite
IEEE Transactions on Aerospace and Electronic Systems ; AES-1 , 2 ; 82-83
1965-10-01
1092643 byte
Article (Journal)
Electronic Resource
English
Optimum Ship Steering-Stabilization Control
Online Contents | 2003
|On satellite electrodynamic attitude stabilization
Elsevier | 2014
|On satellite electrodynamic attitude stabilization
Online Contents | 2014
|