Title :
Design of a longitudinal ride control system for a STOL aircraft by using the modified optimal coordination approach
Author :
El-Singaby, M.I.
Author_Institution :
Dept. of Eng. Sci., Air Defense Coll., Alexandria, Egypt
Abstract :
A modified optimal coordination approach is proposed and applied to the design of a controller for short take-off and landing (STOL) aircraft. This approach exploits the precision and effectiveness of the second version of the method of inequalities together with a decomposition coordination technique to find a suboptimal solution for a set of control systems
Keywords :
aircraft control; STOL aircraft; decomposition coordination technique; longitudinal ride control system; modified optimal coordination approach; short take-off and landing aircraft; Acceleration; Aerospace control; Aircraft; Closed loop systems; Control systems; Error correction; Open loop systems; Open systems; Optimal control; Proportional control;
Conference_Titel :
Systems, Man and Cybernetics, 1989. Conference Proceedings., IEEE International Conference on
Conference_Location :
Cambridge, MA
DOI :
10.1109/ICSMC.1989.71297
