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) |
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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) |
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City | Seattle, WA, USA |
Period | 6/21/95 → 6/23/95 |
ASJC Scopus subject areas
- Control and Systems Engineering