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Stability robustness improvement of direct eigenspace assignment based feedback systems using singular value sensitivities
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Garg, Sanjay |
| Copyright Year | 1989 |
| Description | A methodology to improve the stability robustness of feedback control systems designed using direct eigenspace assignment techniques is presented. The method consists of considering the sensitivity of the minimum singular value of the return difference transfer matrix at the plant input to small changes in the desired closed-loop eigenvalues and the specified elements of the desired closed-loop eigenvectors. Closed-form expressions for the gradient of the minimum return difference singular value with respect to desired closed-loop eigenvalue and eigenvector parameters are derived. Closed-form expressions for the gradients of the control feedback gains with respect to the specified eigenspace parameters are obtained as an intermediate step. The use of the gradient information to improve the guaranteed gain and phase margins in eigenspace assignment based designs is demonstrated by application to an advanced fighter aircraft. |
| File Size | 1237373 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890018301 |
| Archival Resource Key | ark:/13960/t9867dr1s |
| Language | English |
| Publisher Date | 1989-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Robustness Mathematics Transient Response Systems Stability Control Systems Design Feedback Control Flight Control Siso Control Systems Sensitivity Algorithms Eigenvalues Control Stability Mathematical Models Eigenvectors Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |