NASA NTRS · 19790063949
A multiple objective optimization approach to aircraft control systems design
Abstract
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.
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Tabak, D., Schy, A. A., Johnson, K. G., Giesy, D. P.. 1979-01-01. A multiple objective optimization approach to aircraft control systems design. https://ntrs.nasa.gov/citations/19790063949
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