3D Parameters Estimation of Helicopter with Constant Speed Using Single Hydrophone

ZHANG Huaxia; WANG Huigang; SUN Weitao; GU Qingyue; RONG Shaowei

doi:10.11999/JEIT220693

Volume 45 Issue 6

Jun. 2023

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Article Navigation > Journal of Electronics & Information Technology > 2023 > 45(6): 2180-2187

ZHANG Huaxia, WANG Huigang, SUN Weitao, GU Qingyue, RONG Shaowei. 3D Parameters Estimation of Helicopter with Constant Speed Using Single Hydrophone[J]. Journal of Electronics & Information Technology, 2023, 45(6): 2180-2187. doi: 10.11999/JEIT220693

Citation:

ZHANG Huaxia, WANG Huigang, SUN Weitao, GU Qingyue, RONG Shaowei. 3D Parameters Estimation of Helicopter with Constant Speed Using Single Hydrophone[J]. Journal of Electronics & Information Technology, 2023, 45(6): 2180-2187. doi: 10.11999/JEIT220693

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3D Parameters Estimation of Helicopter with Constant Speed Using Single Hydrophone

doi: 10.11999/JEIT220693

1.
School of Marine Science & Technology, Northwestern Polytechnical University, Xi’an 710072, China
2.
Research & Development Institute in Shenzhen, Northwestern Polytechnical University, Shenzhen 518057, China
3.
School of Equipment Management and UAV, Air Force Engineering University, Xi’an 710072, China

Funds: The National Key Laboratory Project of Science and Technology on Underwater Acoustic Antagonizing (JZX7Y201911SY003401), The Science, Technology and Innovation Project of Shenzhen Municipality (CYJ20190806150003606), The Fundamental Research Funds for the Central Universities (D5000220158)

Received Date: 2022-05-30
Accepted Date: 2022-08-25
Rev Recd Date: 2022-08-24

Available Online: 2022-08-30

Publish Date: 2023-06-10

Abstract

Abstract

The three-dimensional parameter estimation algorithm of the helicopter with constant speed flight from the underwater acoustic data with single hydrophone, which extended the traditional two-dimension flight parameters estimation is proposed. Firstly, the helicopter line spectrum is used as the exciting sound source, and its three-dimensional Doppler propagation model in two-layer air-water medium, including altitude, speed and deviation distance of the helicopter, is established. The asymmetry of the Doppler frequency curve and its first- and second-order derivatives is related with the three-dimensional motion parameter of the helicopter, which can be estimated from the received data. Finally, with the measured data, the rationality of the three-dimensional Doppler shift flight model is verified and the result is compared with short-time Fourier instantaneous frequency estimation algorithm, APP-LMS algorithm can more accurately retrieve the flight parameters such as natural frequency, velocity, altitude and yaw distance of the helicopter.
- 3D parameters estimation of helicoper,
- Underwater acoustic detection,
- Doppler effect,
- Instantaneous frequency estimation

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References(18)

References

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