A methodology for multi-objective design assessment and flight control synthesis tuning |
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| Institution: | 1. College of Internet of Things, Hohai University, Changzhou Campus, China;2. Department of Physics, University of Cape Coast, Cape Coast, Ghana;3. Central South University of Forestry and Technology, Changsha, China;4. Department of Mathematics and Computer Science, Brandon University, 270 18th Street, Brandon R7A 6A9, Canada;5. Research Center for Interneural Computing, China Medical University, Taichung 40402, Taiwan;1. College of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China;2. Science and Technology of UAV Laboratory, Northwestern Polytechnical University, Xi’an 710065, China;3. Ordance Engineering College, Shijiazhuang 050003, China |
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| Abstract: | Flight control law design is a multi-variable control problem where various strict requirements from multiple disciplines have to be satisfied. This paper describes quality function deployment and its use in multi-objective control synthesis tuning and design assessment, with application to flight control design. The main feature of this methodology is that the various kinds of design objectives can be taken into account in their most natural form and design alternatives can be assessed most visibly with respect to given requirements. Multi-objective synthesis tuning by min-max parameter optimisation allows interactive compromising in the set of what can be best-possibly achieved with a chosen control law structure. |
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