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Comparison of Multisine Peak Factor Minimization Algorithms for Aircraft System Identification(Presentation)Two phase-optimized multisine peak factor minimization algorithms are presented and evaluated. The first algorithm minimizes peak factor by iteratively clipping the peaks of generated multisine signals. The second algorithm optimizes peak factor indirectly through minimization of an approximation of the infinity norm of the
multisine. Algorithm performance was evaluated as a function of different signal properties, including the number of harmonics, harmonic spacing, and number of snow harmonics (extra harmonics included for further reduction of the peak factor). The two algorithms are compared against results obtained by minimizing peak factor directly using a simplex algorithm, which has been a common approach when designing phase-optimized multisines for system identification flight tests. Sample results show that the clipping and infinity norm algorithms produced multisine signals with comparable peak factors that were lower than that of the simplex algorithm. However, the clipping algorithm runs an order of magnitude faster than the other two algorithms, which also makes it practical to repeat the algorithm multiple times to achieve even lower peak factors.
Document ID
20240013263
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Justin J Matt
(Langley Research Center Hampton, United States)
Date Acquired
October 18, 2024
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-TM-20240009677
Meeting Information
Meeting: LaRC Flight Dynamics Branch Internal Presentation
Location: Hampton, VA
Country: US
Start Date: October 18, 2024
Sponsors: NASA Langley Research Center (LaRC)
Funding Number(s)
WBS: 340428.02.40.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
flight test
peak factor
multisine
system identification
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