Abstract
A method for decomposition of unified state feedback singularly perturbed systems is presented. Based on the small gain theorem, a sufficient condition for robust stability is derived such that the composite state feedback renders the closed-loop singularly perturbed system asymptotically stable. With this method there is no need to consider two different (continuous/discrete) domains. An F-4 fighter aircraft example is given to illustrate the methodology.
| Original language | English (US) |
|---|---|
| Title of host publication | Guidance, Navigation, and Control Conference and Exhibit |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| Pages | 820-825 |
| Number of pages | 6 |
| State | Published - Jan 1 1999 |
| Event | Guidance, Navigation, and Control Conference and Exhibit, 1999 - Portland, United States Duration: Aug 9 1999 → Aug 11 1999 |
Other
| Other | Guidance, Navigation, and Control Conference and Exhibit, 1999 |
|---|---|
| Country/Territory | United States |
| City | Portland |
| Period | 8/9/99 → 8/11/99 |