Title :
An H∞ design for aircraft longitudinal flight control
Author :
Li, X.P. ; Chang, B.C.
Author_Institution :
Dept. of Mech. Eng. & Mech., Drexel Univ., Philadelphia, PA, USA
Abstract :
Step-by-step procedures for applying H∞ control theory to systems design are given. An actual aircraft longitudinal flight control design problem is used to illustrate this process. With the robust controller obtained, simulations and analyses are performed on the closed-loop system
Keywords :
aircraft control; closed loop systems; control system synthesis; optimal control; H∞ control; aircraft control; closed-loop system; longitudinal flight control; robust controller; systems design; Aerospace control; Aircraft; Control systems; Control theory; H infinity control; Linear feedback control systems; Robust control; Robust stability; State-space methods; Transfer functions;
Conference_Titel :
Control Applications, 1992., First IEEE Conference on
Conference_Location :
Dayton, OH
Print_ISBN :
0-7803-0047-5
DOI :
10.1109/CCA.1992.269782
