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投稿时间:2021-11-15 修订日期:2022-03-29
投稿时间:2021-11-15 修订日期:2022-03-29
中文摘要: 针对无人机在失控肇事、干扰航管等方面的危害,本文提出一种基于逐点拉偏式卫星导航欺骗方法,通过重构错误的导航坐标系诱骗目标无人机飞离敏感区域保护地面安全。该方法将整个无人机欺骗过程看作是单步位置欺骗拉偏的时间迭代过程,首先,根据无人机的运动学模型以及外部量测信息估算出无人机的真实位置点以及真实控制输入量;然后,考虑无人机飞行控制器对欺骗效果的影响,在真实控制输入量中抵消掉预先设置的欺骗控制力矩效果,设计构造虚假卫星信号使得GNSS/INS组合导航模式下的滤波估计无人机位置点仍靠近原始期望目标点,但发生了偏差;最后,这种偏差产生的无人机轨迹跟踪控制输入量会导致无人机真实状态点往欺骗目标点偏移,实现单步卫星导航欺骗效果。单步欺骗过程在时间上的迭代运用,可实现无人机位置的逐点偏移式欺骗。仿真结果表明,利用逐点偏移式卫星导航欺骗方法能使得目标无人机慢慢偏离原始轨迹而跟踪欺骗轨迹,且组合导航滤波器估计轨迹仍跟踪原始参考轨迹,达到了卫星导航欺骗的目的。本文提出的基于逐点拉偏式卫星导航欺骗干扰技术可用于保障重点区域/人员的低空安全防护。
中文关键词: 无人机 单步位置偏移 逐点偏移 卫星导航欺骗 GNSS/INS组合导航
Abstract:Aiming at the harm of UAVs in the aspects of out-of-control accident and air traffic control interference, a GNSS navigation spoofing method based on point-by-point offset was proposed in this paper, which decoys target UAV to fly away from sensitive areas and protect ground security by reconstructing the wrong navigation coordinate system. It regards the entire UAV spoofing course as time-iterative process of one-step position spoofing bias. Firstly, the actual positions and actual control inputs were estimated according to the kinematica model of UAV and external measurement information; then, the pre-set fraudulent control effects were cancelled out from the actual control inputs, and the deceptive GNSS signals were designed and constructed so that the filter position estimates in GNSS/INS integrated navigation mode were still close to the original expected point, but had the offset; finally, the real state point of UAV was moved to the spoofed target point caused by the trajectory tracking control inputs generated by the offset , thereby achieving a one-step covert spoofing effect. Finally, the point-by-point position offset spoofing of UAV was completed by the iterative application of the one-step spoofing process over time. Simulation results verified the effectiveness of the proposed GNSS navigation spoofing method of UAV. The simulation results showed that the target UAV can slowly deviate from the original trajectory and track the deceptive trajectory by using the GNSS navigation spoofing method based on point-by-point offset, and the trajectory estimated by the integrated navigation filter still tracks the original reference trajectory, thus achieving the purpose of satellite navigation deception. The proposed spoof jamming technique based on point-by-point pull-biased satellite navigation can be used to protect key areas/personnel at low altitude.
keywords: UAV one-step position spoofing point-by-point offset GNSS navigation spoofing GNSS/INS integrated navigation
文章编号:202101139 中图分类号:U666.11 文献标志码:
基金项目:国家自然科学基金青年科学基金项目(62103424);国防科技大学智能科学学院青年教师创新研究项目(ZN2019-16)
作者 | 单位 | |
郭妍 | 国防科技大学 智能科学学院,湖南 长沙 410073 | guoyan010417@126.com |
唐康华 | 国防科技大学 智能科学学院,湖南 长沙 410073 | tt_kanghua@hotmail.com |
张鹭 | 电子信息系统复杂电磁环境效应国家重点实验室,河南 洛阳 471003 |
作者简介:第一作者:郭妍(1990—),女,讲师,博士. 研究方向:无人与反无人技术. E-mail:guoyan010417@126.com;通信作者:唐康华, E-mail:tt_kanghua@hotmail.com
引用文本:
郭妍,唐康华,张鹭.面向无人机的逐点偏移式卫星导航欺骗干扰方法[J].工程科学与技术,2023,55(2):275-284.
GUO Yan,TANG Kanghua,ZHANG Lu.GNSS Navigation Spoofing Method of UAV Based on Point-by-point Offset[J].Advanced Engineering Sciences,2023,55(2):275-284.
引用文本:
郭妍,唐康华,张鹭.面向无人机的逐点偏移式卫星导航欺骗干扰方法[J].工程科学与技术,2023,55(2):275-284.
GUO Yan,TANG Kanghua,ZHANG Lu.GNSS Navigation Spoofing Method of UAV Based on Point-by-point Offset[J].Advanced Engineering Sciences,2023,55(2):275-284.