| Title:
|
Robust quasi NID aircraft 3D flight control under sensor noise (English) |
| Author:
|
Błachuta, Marian J. |
| Author:
|
Yurkevich, Valery D. |
| Author:
|
Wojciechowski, Konrad |
| Language:
|
English |
| Journal:
|
Kybernetika |
| ISSN:
|
0023-5954 |
| Volume:
|
35 |
| Issue:
|
5 |
| Year:
|
1999 |
| Pages:
|
[637]-650 |
| Summary lang:
|
English |
| . |
| Category:
|
math |
| . |
| Summary:
|
In the paper the design of an aircraft motion controller based on the Dynamic Contraction Method is presented. The control task is formulated as a tracking problem for Euler angles, where the desired decoupled output transients are accomplished under assumption of high-level, high-frequency sensor noise and incomplete information about varying parameters of the system and external disturbances. The resulting controller has a simple form of a combination of a low-order linear dynamical system and a matrix whose entries depend nonlinearly on certain measurable flight variables. (English) |
| Keyword:
|
dynamic contraction method |
| Keyword:
|
tracking problem |
| Keyword:
|
aircraft motion controller |
| Keyword:
|
low-order linear dynamical system |
| Keyword:
|
decoupled output transients |
| Keyword:
|
sensor noise |
| MSC:
|
93B35 |
| MSC:
|
93B51 |
| MSC:
|
93C73 |
| MSC:
|
93C95 |
| idZBL:
|
Zbl 1274.93094 |
| idMR:
|
MR1728472 |
| . |
| Date available:
|
2009-09-24T19:28:33Z |
| Last updated:
|
2015-03-27 |
| Stable URL:
|
http://hdl.handle.net/10338.dmlcz/135312 |
| . |
| Reference:
|
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| . |
