Bifurcation Control of Nonlinear Systems
| dc.contributor.author | Abed, Eyad H. | en_US |
| dc.contributor.author | Fu, Jyun-Horng | en_US |
| dc.contributor.author | Lee, Hsien-Chiarn | en_US |
| dc.contributor.author | Liaw, Der-Cherng | en_US |
| dc.contributor.department | ISR | en_US |
| dc.date.accessioned | 2007-05-23T09:46:19Z | |
| dc.date.available | 2007-05-23T09:46:19Z | |
| dc.date.issued | 1990 | en_US |
| dc.description.abstract | Bifurcation control is discussed in the context of the stabilization of high angle-of-attach flight dynamics. Two classes of stabilization problems for which bifurcation control is useful are discussed. In the first class, which is emphasized in this presentation, a nonlinear control system operates at an equilibrium point which persists only under very small perturbations of a parameter. Such a system will tend to exhibit a jump, or divergence, instability in the absence of appropriate control action. In the second class of systems, an instance of which arises in a tethered satellite system model [14], eigenvalues of the system linearization appear on (or near) the imaginary axis in the complex plane, regardless of the values of system parameters or admissible linear feedback gains. | en_US |
| dc.format.extent | 381409 bytes | |
| dc.format.mimetype | application/pdf | |
| dc.identifier.uri | http://hdl.handle.net/1903/5011 | |
| dc.language.iso | en_US | en_US |
| dc.relation.ispartofseries | ISR; TR 1990-63 | en_US |
| dc.subject | aircraft | en_US |
| dc.subject | nonlinear systems | en_US |
| dc.subject | stability | en_US |
| dc.subject | Intelligent Servomechanisms | en_US |
| dc.title | Bifurcation Control of Nonlinear Systems | en_US |
| dc.type | Technical Report | en_US |
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