The design of an aircraft lateral control system, subject to several performance criteria and constraints, is considered. While in the previous studies of the same model a single criterion optimization, with other performance requirements expressed as constraints, has been pursued, the current approach involves a multiple criteria optimization. In particular, a Pareto optimal solution is sought.
A multiple objective optimization approach to aircraft control systems design
1978 Conference on Decision and Control ; 1979 ; San Diego, CA
01.01.1979
Sonstige
Keine Angabe
Englisch
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