Abstract
For unstable linear systems with actuator magnitude constraints, we present a method for designing smooth feedback control laws which yield maximal regions of attraction. The designed feedback control law produces a closed-loop region of attraction identical to the open-loop region of asymptotic null-controllability. We apply the result to the problem of stabilizing a statically unstable aircraft in the longitudinal direction.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 848-852 |
| Number of pages | 5 |
| Journal | Proceedings of the American Control Conference |
| Volume | 1 |
| State | Published - Jan 1 1997 |
| Event | Proceedings of the 1997 American Control Conference. Part 3 (of 6) - Albuquerque, NM, USA Duration: Jun 4 1997 → Jun 6 1997 |
ASJC Scopus subject areas
- Electrical and Electronic Engineering