Abstract
In this paper, a method is presented for enhancing the performance of an unstable missile system in the presence of multiple saturating actuators. The method involves the design of a saturation detection system which modifies a nominal autopilot via on-line optimization and maintains, to the extent possible, the multivariable properties of the nominal design. The method relies on missile state estimates.
| Original language | English (US) |
|---|---|
| Title of host publication | Proceedings of the American Control Conference |
| Pages | 2143-2147 |
| Number of pages | 5 |
| Volume | 3 |
| State | Published - 1995 |
| Event | Proceedings of the 1995 American Control Conference. Part 1 (of 6) - Seattle, WA, USA Duration: Jun 21 1995 → Jun 23 1995 |
Other
| Other | Proceedings of the 1995 American Control Conference. Part 1 (of 6) |
|---|---|
| City | Seattle, WA, USA |
| Period | 6/21/95 → 6/23/95 |
ASJC Scopus subject areas
- Control and Systems Engineering