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Qft multi-input, multi-output design with non-diagonal, non-square compensation matrices
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hess, R. A. Henderson, D. K. |
| Copyright Year | 1996 |
| Description | A technique for obtaining a non-diagonal compensator for the control of a multi-input, multi-output plant is presented. The technique, which uses Quantitative Feedback Theory, provides guaranteed stability and performance robustness in the presence of parametric uncertainty. An example is given involving the lateral-directional control of an uncertain model of a high-performance fighter aircraft in which redundant control effectors are in evidence, i.e. more control effectors than output variables are used. |
| File Size | 386756 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19980017310 |
| Archival Resource Key | ark:/13960/t8z945m6b |
| Language | English |
| Publisher Date | 1996-01-01 |
| Access Restriction | Open |
| Subject Keyword | Cybernetics Robustness Mathematics Stability Feedback Control Equipment Aircraft Performance Directional Control Flight Control Fighter Aircraft Lateral Control Matrices Mathematics Compensators Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
