Doppler-based motion compensation algorithm for focusing the signature of a rotorcraft.
A computationally efficient algorithm was developed and tested to compensate for the effects of motion on the acoustic signature of a rotorcraft. For target signatures with large spectral peaks that vary slowly in amplitude and have near constant frequency, the time-varying Doppler shift can be tracked and then removed from the data. The algorithm can be used to preprocess data for classification, tracking, and nulling algorithms. The algorithm was tested on rotorcraft data. The average instantaneous frequency of the first harmonic of a rotorcraft was tracked with a fixed-lag smoother. Then, state space estimates of the frequency were used to calculate a time warping that removed the effect of a time-varying Doppler shift from the data. The algorithm was evaluated by analyzing the increase in the amplitude of the harmonics in the spectrum of a rotorcraft. The results depended upon the frequency of the harmonics and the processing interval duration. Under good conditions, the results for the fundamental frequency of the target (~11 Hz) almost achieved an estimated upper bound. The results for higher frequency harmonics had larger increases in the amplitude of the peaks, but significantly lower than the estimated upper bounds.
U.S. Army Research Laboratory, ATTN: RDRL-SES-P, 2800 Powder Mill Road, Adelphi, Maryland 20783-1197, USA. geoffrey.h.goldman.civ@mail.mil
Geoffrey H
GH
Goldman
D000162:Acoustics / Q000295:instrumentation; D000401:Aircraft; D000465:Algorithms; D004301:Doppler Effect; D005583:Fourier Analysis; D008962:Models, Theoretical; D015203:Reproducibility of Results; D012399:Rotation; D012815:Signal Processing, Computer-Assisted; D013018:Sound Spectrography; D013997:Time Factors; D014159:Transducers