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 |
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ASJC Scopus subject areas
- Control and Systems Engineering
Cite this
Saturation prevention strategies for unstable bank-to-turn (BTT) missiles : partial information. / Rodriguez, Armando; Wang, Yanzhuo.
Proceedings of the American Control Conference. Vol. 3 1995. p. 2143-2147.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Saturation prevention strategies for unstable bank-to-turn (BTT) missiles
T2 - partial information
AU - Rodriguez, Armando
AU - Wang, Yanzhuo
PY - 1995
Y1 - 1995
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=0029180315&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0029180315&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:0029180315
VL - 3
SP - 2143
EP - 2147
BT - Proceedings of the American Control Conference
ER -