Elsevier

Automatica

Volume 15, Issue 5, September 1979, Pages 595-600
Automatica

Brief paper
Application of multiobjective optimization in aircraft control systems design

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Abstract

Multiobjective optimization techniques are applied in the design of an aircraft lateral control system. A large manned reentry vehicle and a fighter aircraft are considered. An algorithm suggested by Lin's Proper Inequality Constraints method, is implemented in the numerical computation of Pareto-optimal solutions. Subsequently, a trade-off analysis of several Pareto-optimal solutions is conducted.

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The original version of this paper was not presented at any IFAC Meeting. This paper was recommended for publication in revised form by associate editor H. Kwakernaak.

Department of Electrical Engineering, Ben-Gurion University of the Negev, Beer-Sheva, Israel. (Work performed while at NASA Langley Research Center).

Vought Corporation, Hampton Technical Center.

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