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Publishing Language: Chinese

Design of tracking telemetry and command signal based on prolate spheroidal wave functions waveform forming

Zhichao XU1,2,3Faping LU2,3Jiafang KANG2,3Qi AN2,3Zhilin ZHANG2,3Dongkai YANG1( )
School of Electronic and Information Engineering,Beihang University,Beijing 100191,China
Naval Aviation University,Yantai 264001,China
Key Laboratory on Signal & Information Processing of Shandong Province,Yantai 264001,China
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Abstract

Enhancing the signal waveform's power efficiency and information transmission efficiency is one of the issues in tracking, telemetry, and command (TT&C) system waveform design. It is found that the basic characteristics such as biorthogonal, optimal time-frequency energy aggregate, and spectral controllable of prolate spheroidal wave functions (PSWFs) make it be a reliable candidate for TT&C signal waveform design. In this paper, PSWF are introduced into TT&C signal waveform design, and a four-dimensional unified spread spectrum TT&C signal waveform design method based on PSWF waveform shaping is proposed. This new idea, by using high-energy aggregation PSWF as waveform shaping functions, can obtain higher power efficiency and information transmission rate, better anti-interference and anti-interception capabilities. It provides a better waveform scheme for the design of TT&C signal waveforms. For instance, the suggested approach can boost the spread spectrum gain by 3.44 dB and the information transmission rate by one when compared to conventional TT&C signals based on rectangular pulse functions under the same system error performance.

CLC number: V443.1;TN975 Document code: A Article ID: 1001-5965(2026)04-1160-10

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Journal of Beijing University of Aeronautics and Astronautics
Pages 1160-1169

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Cite this article:
XU Z, LU F, KANG J, et al. Design of tracking telemetry and command signal based on prolate spheroidal wave functions waveform forming. Journal of Beijing University of Aeronautics and Astronautics, 2026, 52(4): 1160-1169. https://doi.org/10.13700/j.bh.1001-5965.2024.0068

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Received: 30 January 2024
Published: 10 April 2024
© Journal of Beijing University of Aeronautics and Astronautics