NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Performance comparison of five frequency domain system identification techniques for helicopter higher harmonic controlThis paper presents the results of a computer simulation comparing the performance of five system identification techniques currently proposed for use with helicopter, frequency domain, higher harmonic vibration control algorithms. The system identification techniques studied were: (1) the weighted least squares method in moving block format, (2) the classical Kalman filter, (3) a generalized Kalman filter, (4) the classical least mean square (LMS) filter, and (5) a generalized LMS filter. The generalized Kalman and LMS filters were derived by allowing for multistep operation, rather than the single-step update approach used by their classical versions. Both open-loop and closed-loop (vibration control mode) identification results are presented in the paper. The algorithms are evaluated in terms of their accuracy, stability, convergence properties, computation speeds, and the relative ease with which these techniques may be directly applied to the helicopter vibration control problem.
Document ID
19880064545
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jacklin, Stephen A.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: International Conference on Rotorcraft Basic Research
Location: College Park, MD
Country: United States
Start Date: February 16, 1988
End Date: February 18, 1988
Accession Number
88A51772
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available