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Design of a longitudinal ride control system for a STOL aircraft by using the modified optimal coordination approach

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1 Author(s)
El-Singaby, M.I. ; Dept. of Eng. Sci., Air Defense Coll., Alexandria, Egypt

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

Published in:

Systems, Man and Cybernetics, 1989. Conference Proceedings., IEEE International Conference on

Date of Conference:

14-17 Nov 1989