Title :
Designing Autopilot by Nonlinear Servomechanism Theory
Author :
Huang, J. ; Lin, C.F.
Author_Institution :
American GNC Corporation, CA
Keywords :
Aerospace control; Eigenvalues and eigenfunctions; Equations; Error correction; Performance gain; Regulators; Servomechanisms; State feedback; Steady-state; Uncertainty;
Conference_Titel :
Aerospace Control Systems, 1993. Proceedings. The First IEEE Regional Conference on
DOI :
10.1109/AEROCS.1993.721028
