Digital Controller Design for the Pitch Axis of the F-14 Using an H_INFINTY Method.
| dc.contributor.author | Levine, William S. | en_US |
| dc.contributor.author | Yang, J.S. | en_US |
| dc.contributor.department | ISR | en_US |
| dc.date.accessioned | 2007-05-23T09:43:24Z | |
| dc.date.available | 2007-05-23T09:43:24Z | |
| dc.date.issued | 1989 | en_US |
| dc.description.abstract | A 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.extent | 744858 bytes | |
| dc.format.mimetype | application/pdf | |
| dc.identifier.uri | http://hdl.handle.net/1903/4875 | |
| dc.language.iso | en_US | en_US |
| dc.relation.ispartofseries | ISR; TR 1989-26 | en_US |
| dc.title | Digital Controller Design for the Pitch Axis of the F-14 Using an H_INFINTY Method. | en_US |
| dc.type | Technical Report | en_US |
Files
Original bundle
1 - 1 of 1