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{"title":"Omni-Directional Antenna-Based Rotational Speed Measurement of High-Speed Rolling Carriers","authors":"Xiyan Sun, Ruoru Li, Yuanfa Ji, Yu Chen, Chenggan Wen","doi":"10.1002/tee.70232","DOIUrl":null,"url":null,"abstract":"<p>Accurate rotational speed measurement is essential for high-speed rolling carriers. Traditional rotational speed measurement techniques are often limited by low spin rate and harsh external environments, reducing their effectiveness in high-dynamic conditions. This paper proposes a Global Navigation Satellite System (GNSS)-based rotational speed measurement method utilizing an omni-directional antenna, which ensures continuous signal acquisition and tracking under high rotational speeds. A mathematical model is established to analyze the effect of missile spin on GNSS signals, enabling rotational speed estimation using in-phase (I) and quadrature-phase (Q) correlation values. To enhance tracking accuracy, we introduce a Frequency-Locked Loop (FLL)-assisted Phase-Locked Loop (PLL) algorithm, which enables real-time speed detection and improves system robustness against high-frequency disturbances. Furthermore, an adaptive coherent integration time adjustment mechanism and a filter parameter optimization strategy are proposed to mitigate high-frequency residual errors, ensuring high tracking accuracy and stability. Simulation results confirm that the omni-directional antenna-assisted system achieves higher frequency estimation accuracy and is significantly more stable than traditional PLL-based methods, particularly under low signal-to-noise ratio (SNR) conditions. The proposed approach meets the accuracy requirements for high-speed rolling carriers within the range 3 r/s ≤ r ≤ 300 r/s, making it suitable for real-time aircraft flight trajectory correction and aerospace applications. © 2025 Institute of Electrical Engineers of Japan and Wiley Periodicals LLC.</p>","PeriodicalId":13435,"journal":{"name":"IEEJ Transactions on Electrical and Electronic Engineering","volume":"21 8","pages":"1246-1255"},"PeriodicalIF":1.0000,"publicationDate":"2026-07-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEJ Transactions on Electrical and Electronic Engineering","FirstCategoryId":"5","ListUrlMain":"https://onlinelibrary.wiley.com/doi/10.1002/tee.70232","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"2025/12/29 0:00:00","PubModel":"Epub","JCR":"Q4","JCRName":"ENGINEERING, ELECTRICAL & ELECTRONIC","Score":null,"Total":0}
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Abstract
Accurate rotational speed measurement is essential for high-speed rolling carriers. Traditional rotational speed measurement techniques are often limited by low spin rate and harsh external environments, reducing their effectiveness in high-dynamic conditions. This paper proposes a Global Navigation Satellite System (GNSS)-based rotational speed measurement method utilizing an omni-directional antenna, which ensures continuous signal acquisition and tracking under high rotational speeds. A mathematical model is established to analyze the effect of missile spin on GNSS signals, enabling rotational speed estimation using in-phase (I) and quadrature-phase (Q) correlation values. To enhance tracking accuracy, we introduce a Frequency-Locked Loop (FLL)-assisted Phase-Locked Loop (PLL) algorithm, which enables real-time speed detection and improves system robustness against high-frequency disturbances. Furthermore, an adaptive coherent integration time adjustment mechanism and a filter parameter optimization strategy are proposed to mitigate high-frequency residual errors, ensuring high tracking accuracy and stability. Simulation results confirm that the omni-directional antenna-assisted system achieves higher frequency estimation accuracy and is significantly more stable than traditional PLL-based methods, particularly under low signal-to-noise ratio (SNR) conditions. The proposed approach meets the accuracy requirements for high-speed rolling carriers within the range 3 r/s ≤ r ≤ 300 r/s, making it suitable for real-time aircraft flight trajectory correction and aerospace applications. © 2025 Institute of Electrical Engineers of Japan and Wiley Periodicals LLC.
基于全向天线的高速滚动载体转速测量
准确的转速测量对高速滚动运输车至关重要。传统的转速测量技术往往受到低转速和恶劣外部环境的限制,降低了其在高动态条件下的有效性。提出了一种基于全球导航卫星系统(GNSS)的全向天线转速测量方法,以保证高转速下信号的连续采集和跟踪。建立了导弹自旋对GNSS信号影响的数学模型,实现了利用同相(I)和正交相(Q)相关值进行转速估计。为了提高跟踪精度,我们引入了锁频环(FLL)辅助锁相环(PLL)算法,该算法可以实现实时速度检测并提高系统对高频干扰的鲁棒性。此外,提出了一种自适应相干积分时间调整机制和滤波器参数优化策略,以减轻高频残留误差,保证高跟踪精度和稳定性。仿真结果表明,与传统的基于锁相环的方法相比,全向天线辅助系统具有更高的频率估计精度和显著的稳定性,特别是在低信噪比条件下。该方法满足3r /s≤r≤300r /s范围内高速滚转载体的精度要求,适用于飞机飞行轨迹实时修正和航空航天应用。©2025日本电气工程师协会和Wiley期刊有限责任公司。
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