Optimal tuner selection for Kalman filter-based aircraft engine performance estimation /

Bibliographic Details

Main Author:	Simon, Donald L.
Corporate Authors:	NASA Glenn Research Center, ASME Turbo Expo
Other Authors:	Garg, Sanjay
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:	NASA technical memorandum ; 216076.
Subjects:	Error analysis. Kalman filters. Gas turbine engines. Steady state. On-line systems. Performance prediction. Mean square values.
Online Access:	https://purl.fdlp.gov/GPO/gpo991