Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters [[electronic resource] / Takahisa Kobayashi, Donald L. Simon and Jonathan S. Litt]
Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine pe...
(Visualizza in formato marc)
(Visualizza in BIBFRAME)
| Autore: |
Kobayashi Takahisa
|
| Titolo: |
Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters [[electronic resource] / Takahisa Kobayashi, Donald L. Simon and Jonathan S. Litt]
|
| Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005] |
| Descrizione fisica: | 1 online resource (12 pages) : color illustrations |
| Soggetto topico: | Kalman filters |
| Aircraft engines | |
| Gas turbine engines | |
| Aircraft performance | |
| Amplification | |
| Altri autori: |
SimonDonald L
LittJonathan S
|
| Note generali: | Title from title screen (viewed on Mar. 12, 2012). |
| "Prepared for the Turbo Expo 2005 sponsored by the American Society of Mechanical Engineers, Reno, Nevada, June 6-9, 2005." | |
| "September 2005." | |
| "ARL-TR-3489." | |
| "GT2005-68494." | |
| Nota di bibliografia: | Includes bibliographical references (pages 11-12). |
| Titolo autorizzato: | Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910701473503321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |