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Digital Controller Design for the Pitch Axis of the F-14 Using an H_INFINTY Method.

dc.contributor.authorLevine, William S.en_US
dc.contributor.authorYang, J.S.en_US
dc.date.accessioned2007-05-23T09:43:24Z
dc.date.available2007-05-23T09:43:24Z
dc.date.issued1989en_US
dc.identifier.urihttp://hdl.handle.net/1903/4875
dc.description.abstractA H_INFINITY based control system design procedure is developed. The basic idea is to produce a controller in which the closed- loop system is designed, via H_INFINITY methods similar to those of Kwakemaak, to be robust with respect to both disturbance rejection and insensitivity to parameter variations. This design algorithm is then applied to design a pitch axis controller for a digitized model of the F -14 aircraft. In this two-degree-of- freedom structure, the controller is designed via our H_INFINITY method. The pre-compensator is used to shape the output response so as to cause the entire system to achieve the desired performance. The robustness of the angle-of-attack step response under large parameter variations is also examined.en_US
dc.format.extent744858 bytes
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen_US
dc.relation.ispartofseriesISR; TR 1989-26en_US
dc.titleDigital Controller Design for the Pitch Axis of the F-14 Using an H_INFINTY Method.en_US
dc.typeTechnical Reporten_US
dc.contributor.departmentISRen_US


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