Maximum likelihood estimation of translational acceleration derivatives from flight dataThis paper shows that translational acceleration derivatives, such as pitching moment due to rate of change of angle of attack, can be estimated from flight data with the use of appropriately designed maneuvers. No new development of estimation methodology is necessary to analyze these maneuvers. Flight data from a T-37B airplane were used to verify that rate of change of angle of attack could be estimated from rolling maneuvers.
Document ID
19780062630
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Maine, R. E. (NASA Flight Research Center Edwards, CA, United States)
Iliff, K. W. (NASA Flight Research Center Edwards, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 78-1342Report Number: AIAA PAPER 78-1342