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- W2726487989 abstract "Summary Optimal controller design constrained on the desired response characteristics and the available states for a VTOL aircraft is considered. The procedure is illustrated by considering the longitudinal flight control of a VTOL aircraft, Model S-58, during its hovering mode. Two cases of the desired response characteristics are considered. First, all of the desired characteristics of the plant are assumed to be specified. Secondly, only sane of the desired response characteristics are assumed to be given. In each case the synthesis procedure is based upon the available plant states. Computational results obtained for each case illustrate the characteristics of the design procedure." @default.
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- W2726487989 date "1976-05-01" @default.
- W2726487989 modified "2023-09-25" @default.
- W2726487989 title "On a Constrained Design of an Optimal Controller for VTOL Aircraft *" @default.
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- W2726487989 doi "https://doi.org/10.1016/s1474-6670(17)67147-7" @default.
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