基于DME/DME的GNSS干扰缓解导航:仿真,算法

Mustafa Tekin, Mehmet Karakas
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引用次数: 4

摘要

全球导航卫星系统是最精确的导航手段,但它依赖于可用的卫星,而且由于接收信号功率低,这些信号容易受到干扰。为了应对可能出现的无意/有意的信号丢失或退化漏洞和欺骗线程,并保持系统的准确性和完整性,提出了一种备用的基于DME/DME的导航系统。本文描述了基于DME/ DME的系统解决方案的实现和性能,以及模拟和真实的测试数据/结果。将飞行试验的共享记录数据与GNSS信号进行比较,验证了所提议的减缓算法的有效性。我们首先给出了所提出的DME/DME联合缓解算法的细节。然后,我们给出了模拟结果,并展示了精度优于0.1海里的备用导航能力。最后,我们分享了在土耳其安卡拉的TAI/TUSAS设施进行的真实飞行活动测量,以展示算法的性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
DME/DME Based Navigation for GNSS Interference Mitigation: Simulation, Algorithms
GNSS is the most accurate mean of navigation but it relies on satellite being available, and these signals are susceptible to interference due to their low received signal power. To deal with possible unintentional/intentional signal loss or degradation vulnerabilities and spoofing threads, and to maintain system accuracy and integrity an alternative backup DME/DME based navigation system is proposed. The article describes the implementation and performance of purposed DME/ DME based system solution together with simulated and real test data/results. Shared recorded data from the flight tests compared with GNSS signals verify the effectiveness of the proposed mitigation algorithm. We first give details of proposed DME/DME joint mitigation algorithm. We then present the simulated results and show backup navigation capability with accuracies better than 0.1 nautical miles. Finally, we share real flights campaign measurements performed at TAI/TUSAS facilities in Ankara, Turkey to show performance of algorithm.
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