Brief paper: Application of multiobjective optimization in aircraft control systems design

Authors:
D. Tabak;A. A. Schy;D. P. Giesy;K. G. Johnson
Affiliations:
-;Assistant Head, Stability and Control Branch, Flight Dynamics and Control Division, NASA-Langley Research Center, MS 478, Hampton, VA 23665, U.S.A.;NASA-Langley Research Center, MS' 478, Hampton, VA 23665, U.S.A.;NASA-Langley Research Center, MS' 478, Hampton, VA 23665, U.S.A.
Venue:
Automatica (Journal of IFAC)
Year:
1979

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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.