Title :
Nonlinear H∞ control of aerospace plane ascent
Author :
McEneaney, William M. ; Mease, Kenneth D.
Author_Institution :
Dept. of Math., Carnegie Mellon Univ., Pittsburgh, PA, USA
Abstract :
Nonlinear H∞ theory is applied to design the fast part of a composite control for guiding the ascent of an aerospace plane to orbit. The viscosity solution of the corresponding Isaacs equation is obtained at any point by a generalized method of characteristics
Keywords :
H∞ control; aerospace control; attitude control; fuel optimal control; game theory; nonlinear control systems; state-space methods; Isaacs equation; aerospace plane; ascent guidance; game theory; minimum fuel control; nonlinear H∞ control; space vehicles; state space method; viscosity solution; Additives; Aerodynamics; Aerospace control; Argon; Attenuation; Equations; H infinity control; Optimal control; State-space methods; Viscosity;
Conference_Titel :
Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
Conference_Location :
New Orleans, LA
Print_ISBN :
0-7803-2685-7
DOI :
10.1109/CDC.1995.479229
