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 con...Show MoreMetadata
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.
Published in: IEEE Transactions on Aerospace and Electronic Systems ( Volume: AES-1, Issue: 2, October 1965)
