Application of a Constant Gain Extended Kalman Filter for In-Flight Estimation of Aircraft Engine Performance Parameters.

Application of a Constant Gain Extended Kalman Filter for In-Flight Estimation of Aircraft Engine Performance Parameters.

Author(s):

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

2005

Pub. Year:

2005

No.:

GT2005-68494

Paper no.:

GT2005-68494

Pages:

12

Pub. info.:

New York, NY: American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00001650
Series ID:	PA00000136
Conf. info. (Name):	ASME Turbo Expo 2005
Conf. info. (Number):	2005
Conf. info. (Venue):	Reno-Tahoe, NV., USA
Conf. info. (Date):	2005.06.06-2005.06.09
Note for article:	ASME Turbo Expo 2005, Reno-Tahoe, NV., USA, June 6-9, 2005

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