| contributor author | N. Sugiyama | |
| date accessioned | 2017-05-09T00:02:27Z | |
| date available | 2017-05-09T00:02:27Z | |
| date copyright | January, 2000 | |
| date issued | 2000 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26793#19_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/123707 | |
| description abstract | System identification plays an important role in advanced control systems for jet engines, in which controls are performed adaptively using data from the actual engine and the identified engine. An identification technique for jet engine using the Constant Gain Extended Kalman Filter (CGEKF) is described. The filter is constructed for a two-spool turbofan engine. The CGEKF filter developed here can recognize parameter change in engine components and estimate unmeasurable variables over whole flight conditions. These capabilities are useful for an advanced Full Authority Digital Electric Control (FADEC). Effects of measurement noise and bias, effects of operating point and unpredicted performance change are discussed. Some experimental results using the actual engine are shown to evaluate the effectiveness of CGEKF filter. [S0742-4795(00)00401-4] | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | System Identification of Jet Engines | |
| type | Journal Paper | |
| journal volume | 122 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.483172 | |
| journal fristpage | 19 | |
| journal lastpage | 26 | |
| identifier eissn | 0742-4795 | |
| keywords | Engines | |
| keywords | Jet engines | |
| keywords | Kalman filters | |
| keywords | Compressors AND Turbofans | |
| tree | Journal of Engineering for Gas Turbines and Power:;2000:;volume( 122 ):;issue: 001 | |
| contenttype | Fulltext | |
