State Estimation of Aircraft in Lateral Movement by Using Observers and Kalman Filter

被引：0

作者：

Kiyak, Emre ^{[1
]}

Iyibakanlar, Gulay ^{[1
]}

机构：

[1] Anadolu Univ, Sivil Havacilik Yuksekokulu, Havacilik Elk Elt Bolumu, TR-26470 Eskisehir, Turkey

来源：

PAMUKKALE UNIVERSITY JOURNAL OF ENGINEERING SCIENCES-PAMUKKALE UNIVERSITESI MUHENDISLIK BILIMLERI DERGISI | 2009年 / 15卷 / 02期

关键词：

Observers; Kalman Filter; Estimation of state;

D O I：

暂无

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Nowadays, lots of problems are simplified by modeling. Instead of working with real systems, response of a system may be examined and analyzed by using modeling. A fault tolerant scheme relies on the estimation of true states. Observers and Kalman Filters are widely used in such an estimation. In this study, an application is realized for states estimation of an aircraft in lateral movement by using observers and a Kalman Filter.

引用

页码：291 / 299

页数：9

共 18 条

[11] Cenan N., 1998, THESIS
[12] Gu Y., 2004, THESIS
[13] Sensor and control surface/actuator failure detection and isolation applied to F-16 flight dynamic
Hajiyev, C
Caliskan, F
[J]. AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2005, 77 (02) : 152 - 160
[14] Aircraft sensor fault detection based on unknown input observers
Kiyak, Emre
Cetin, Oemer
Kahvecioglu, Ayse
[J]. AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2008, 80 (05) : 545 - 548
[15] Krzeminski S., 2004, B POLISH ACAD SCI TE, V50
[16] McLean D, 1990, AUTOMATIC FLIGHT CON
[17] Siouris G. M., 1996, ENG APPROACH OPTIMAL
[18] Solak E., 2001, THESIS

← 1 2 →