CN117439698B - Dynamic monitoring and adjustment method and system for operating status of UAV interference equipment - Google Patents

Dynamic monitoring and adjustment method and system for operating status of UAV interference equipment Download PDF

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CN117439698B
CN117439698B CN202311708849.XA CN202311708849A CN117439698B CN 117439698 B CN117439698 B CN 117439698B CN 202311708849 A CN202311708849 A CN 202311708849A CN 117439698 B CN117439698 B CN 117439698B
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interference
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uav
equipment
operation control
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CN117439698A (en
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宋林海
王大军
杨猛
王昊
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Yixun Technology Co ltd
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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04KSECRET COMMUNICATION; JAMMING OF COMMUNICATION
    • H04K3/00Jamming of communication; Counter-measures
    • H04K3/40Jamming having variable characteristics
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04KSECRET COMMUNICATION; JAMMING OF COMMUNICATION
    • H04K3/00Jamming of communication; Counter-measures
    • H04K3/60Jamming involving special techniques
    • H04K3/62Jamming involving special techniques by exposing communication, processing or storing systems to electromagnetic wave radiation, e.g. causing disturbance, disruption or damage of electronic circuits, or causing external injection of faults in the information

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  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
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  • Physics & Mathematics (AREA)
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  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

The invention discloses a method and a system for dynamically monitoring and adjusting the running state of unmanned aerial vehicle interference equipment, which relate to the technical field of signal detection and are used for constructing a space domain based on the unmanned aerial vehicle interference equipment; generating an identification response, synchronously activating an interference operation control module along with the receiving of the identification response, and configuring an interference scheme based on an interference mode; tracking and positioning a target unmanned aerial vehicle, performing radio countering of the target unmanned aerial vehicle based on the interference scheme, and determining a target interference live condition; extracting an echo feedback signal, performing running state evaluation, and determining the brake off-axis degree; if the brake off-axis degree does not meet the threshold value standard, determining an operation disturbance factor marked with disturbance degree; the adaptive operation regulation and control of the unmanned aerial vehicle interference equipment are carried out, the problem that the unmanned aerial vehicle interference equipment in the prior art cannot be dynamically regulated according to the operation state due to insufficient rigor and insufficient completeness is solved, and the stability of the unmanned aerial vehicle interference equipment is improved.

Description

无人机干扰设备的运行状态动态监测调节方法及系统Dynamic monitoring and adjustment method and system for operating status of UAV interference equipment

技术领域Technical field

本发明涉及信号探测技术领域,具体涉及无人机干扰设备的运行状态动态监测调节方法及系统。The present invention relates to the technical field of signal detection, and in particular to a method and system for dynamic monitoring and adjustment of the operating status of UAV interference equipment.

背景技术Background technique

随着无人机技术的不断发展,无人机干扰设备在军事、安全、航空摄影等诸多领域的需求日益增长。无人机干扰设备的主要作用是通过发射特定频段的信号来干扰无人机的正常飞行,从而防止无人机进入禁飞区域或执行危险任务。然而,在实际使用过程中,无人机干扰设备常常会受到各种因素的影响,导致其干扰效果和稳定性不佳,因此,对无人机干扰设备的运行状态进行实时监测和调节,以保证干扰效果和稳定性,同时具有较低的成本和较高的可扩展性,并且能够适应各种复杂环境和任务需求具有重要意义。With the continuous development of drone technology, the demand for drone interference equipment is growing in many fields such as military, security, aerial photography and so on. The main function of drone jamming equipment is to interfere with the normal flight of drones by emitting signals in specific frequency bands, thereby preventing drones from entering no-fly areas or performing dangerous tasks. However, in actual use, UAV interference equipment is often affected by various factors, resulting in poor interference effect and stability. Therefore, the operating status of UAV interference equipment must be monitored and adjusted in real time to ensure It is of great significance to ensure the interference effect and stability, while having lower cost and higher scalability, and being able to adapt to various complex environments and mission requirements.

现有技术中存在的无人机干扰设备由于不够严谨且完备性不足而导致无法根据运行状态进行动态调整的问题,使得最终无法保证无人机干扰设备的干扰效果和稳定性。The UAV interference equipment in the existing technology cannot be dynamically adjusted according to the operating status due to insufficient rigor and completeness, which ultimately makes it impossible to guarantee the interference effect and stability of the UAV interference equipment.

发明内容Contents of the invention

本申请提供了无人机干扰设备的运行状态动态监测调节方法及系统,解决了现有技术中存在的无人机干扰设备由于不够严谨且完备性不足而导致无法根据运行状态进行动态调整的问题,实现了提高无人机干扰设备的稳定性。This application provides a dynamic monitoring and adjustment method and system for the operating status of UAV interference equipment, which solves the problem in the existing technology that UAV interference equipment cannot be dynamically adjusted according to the operating status due to insufficient rigor and completeness. , achieving improved stability of UAV jamming equipment.

鉴于上述问题,本申请提供了无人机干扰设备的运行状态动态监测调节方法。In view of the above problems, this application provides a dynamic monitoring and adjustment method for the operating status of UAV interference equipment.

第一方面,本申请提供了无人机干扰设备的运行状态动态监测调节方法,方法包括:通过搭建基于无人机干扰设备的空间域,所述空间域基于设备射频范围进行配置;基于空间域的探测空间约束,结合探测运控模块,通过无人机干扰设备的无线电探测进行目标识别,生成识别响应,其中,所述探测运控模块用于控制无人机干扰设备进行无线电探测;随着所述识别响应的接收,同步激活干扰运控模块,并配置基于干扰模式的干扰方案,其中,所述干扰模式包括迫降模式、返航模式与飞控干扰模式,所述干扰运控模块用于接收识别相应,并对当前干扰方式进行判断和干扰方案配置;对目标无人机进行追踪定位,结合空间域的干扰空间约束,基于所述干扰方案进行所述目标无人机的无线电反制,确定目标干扰实况;基于所述识别响应与所述目标干扰实况,提取回波反馈信号并进行运行状态评估,确定制动离轴度,所述制动离轴度为预期控制效果与实际控制效果之间的差值;若所述制动离轴度不满足阈值标准,针对所述制动离轴度进行溯源,确定标识有扰动度的运行扰动因素;基于所述运行扰动因素,对所述无人机干扰设备进行适应性运行调控。In the first aspect, this application provides a method for dynamic monitoring and adjustment of the operating status of UAV interference equipment. The method includes: building a space domain based on UAV interference equipment, and the space domain is configured based on the radio frequency range of the equipment; based on the spatial domain The detection space constraint, combined with the detection operation and control module, carries out target recognition through radio detection of UAV jamming equipment, and generates a recognition response, wherein the detection operation and control module is used to control the UAV interference equipment to perform radio detection; as The reception of the identification response activates the interference operation and control module synchronously, and configures an interference scheme based on interference modes. The interference modes include forced landing mode, return mode and flight control interference mode. The interference operation control module is used to receive Identify the corresponding, judge the current interference method and configure the interference plan; track and locate the target UAV, combined with the interference space constraints in the space domain, conduct radio countermeasures for the target UAV based on the interference plan, and determine Target interference real situation; based on the recognition response and the target interference real situation, extract the echo feedback signal and conduct operating status evaluation to determine the braking off-axis degree, which is the combination of the expected control effect and the actual control effect. The difference between Human-machine interference equipment performs adaptive operation control.

第二方面,本申请提供了无人机干扰设备的运行状态动态监测调节系统,系统包括:空间域搭建模块:搭建基于无人机干扰设备的空间域,所述空间域基于设备射频范围进行配置;识别响应模块:基于空间域的探测空间约束,结合探测运控模块,通过无人机干扰设备的无线电探测进行目标识别,生成识别响应,其中,所述探测运控模块用于控制无人机干扰设备进行无线电探测;干扰方案模块:随着所述识别响应的接收,同步激活干扰运控模块,并配置基于干扰模式的干扰方案,其中,所述干扰模式包括迫降模式、返航模式与飞控干扰模式,所述干扰运控模块用于接收识别相应,并对当前干扰方式进行判断和干扰方案配置;追踪定位模块:对目标无人机进行追踪定位,结合空间域的干扰空间约束,基于所述干扰方案进行所述目标无人机的无线电反制,确定目标干扰实况;状态评估模块:基于所述识别响应与所述目标干扰实况,提取回波反馈信号并进行运行状态评估,确定制动离轴度,所述制动离轴度为预期控制效果与实际控制效果之间的差值;扰动因素模块:若所述制动离轴度不满足阈值标准,针对所述制动离轴度进行溯源,确定标识有扰动度的运行扰动因素;运行调控模块:基于所述运行扰动因素,对所述无人机干扰设备进行适应性运行调控。In the second aspect, this application provides a dynamic monitoring and adjustment system for the operating status of drone interference equipment. The system includes: a space domain construction module: builds a space domain based on drone interference equipment, and the space domain is configured based on the radio frequency range of the equipment. ; Identification response module: Based on the detection space constraints of the space domain, combined with the detection operation control module, target recognition is performed through radio detection of the UAV jamming equipment, and an identification response is generated, where the detection operation control module is used to control the UAV The interference equipment performs radio detection; the interference solution module: with the reception of the identification response, the interference operation control module is synchronously activated, and an interference solution based on the interference mode is configured, where the interference mode includes forced landing mode, return mode and flight control Interference mode, the interference operation control module is used to receive and identify responses, judge the current interference mode and configure the interference plan; the tracking and positioning module: track and position the target UAV, combined with the interference space constraints in the space domain, based on the The interference plan is used to perform radio countermeasures on the target UAV and determine the actual target interference situation; the state evaluation module: based on the identification response and the actual target interference situation, extract the echo feedback signal and perform operating status evaluation to determine the braking Off-axis degree, the braking off-axis degree is the difference between the expected control effect and the actual control effect; Disturbance factor module: If the braking off-axis degree does not meet the threshold standard, for the braking off-axis degree Trace the source and determine the operating disturbance factors with a degree of disturbance; the operation control module: based on the operation disturbance factors, perform adaptive operation control of the UAV interference equipment.

本申请中提供的一个或多个技术方案,至少具有如下技术效果或优点:One or more technical solutions provided in this application have at least the following technical effects or advantages:

本申请实施例提供的无人机干扰设备的运行状态动态监测调节方法及系统,通过搭建基于无人机干扰设备的空间域,空间域基于设备射频范围进行配置,基于空间域的探测空间约束,结合探测运控模块,通过无人机干扰设备的无线电探测进行目标识别,生成识别响应,其中,所述探测运控模块用于控制无人机干扰设备进行无线电探测,再随着识别响应的接收,同步激活干扰运控模块,并配置基于干扰模式的干扰方案,再对目标无人机进行追踪定位,结合空间域的干扰空间约束,基于干扰方案进行目标无人机的无线电反制,确定目标干扰实况,并基于识别响应与目标干扰实况,提取回波反馈信号并进行运行状态评估,确定制动离轴度,然后若制动离轴度不满足阈值标准,针对制动离轴度进行溯源,确定标识有扰动度的运行扰动因素,最后基于运行扰动因素,进行无人机干扰设备的适应性运行调控,解决了现有技术中存在的无人机干扰设备由于不够严谨且完备性不足而导致无法根据运行状态进行动态调整的问题,实现了提高无人机干扰设备的稳定性。The method and system for dynamic monitoring and adjustment of the operating status of UAV interference equipment provided by the embodiments of this application build a space domain based on UAV interference equipment, the space domain is configured based on the radio frequency range of the equipment, and based on the detection space constraints of the space domain, Combined with the detection operation and control module, the target is identified through radio detection of the UAV interference equipment, and an identification response is generated. The detection operation control module is used to control the UAV interference equipment to perform radio detection, and then as the identification response is received , synchronously activate the interference operation control module, configure the interference scheme based on the interference mode, and then track and locate the target UAV. Combined with the interference space constraints in the space domain, the radio countermeasures of the target UAV are carried out based on the interference scheme to determine the target. Interference real-time, and based on the recognition response and target interference real-time, extract the echo feedback signal and conduct operating status evaluation to determine the braking off-axis degree. Then, if the braking off-axis degree does not meet the threshold standard, trace the braking off-axis degree. , determine the operational disturbance factors that indicate the degree of disturbance, and finally conduct adaptive operation regulation of UAV interference equipment based on the operational disturbance factors, solving the problem of UAV interference equipment existing in the existing technology due to insufficient rigor and incompleteness. This leads to the problem of being unable to dynamically adjust according to the operating status, thereby improving the stability of drone interference equipment.

附图说明Description of drawings

图1为本申请提供了无人机干扰设备的运行状态动态监测调节方法流程示意图;Figure 1 is a schematic flow chart of the dynamic monitoring and adjustment method for the operating status of UAV interference equipment provided in this application;

图2为本申请提供了无人机干扰设备的运行状态动态监测调节系统结构示意图。Figure 2 is a schematic structural diagram of the dynamic monitoring and adjustment system for operating status of UAV interference equipment provided in this application.

附图标记说明:空间域搭建模块11,识别响应模块12,干扰方案模块13,追踪定位模块14,状态评估模块15,扰动因素模块16,运行调控模块17。Explanation of reference signs: spatial domain construction module 11, identification response module 12, interference solution module 13, tracking and positioning module 14, status assessment module 15, disturbance factor module 16, operation control module 17.

具体实施方式Detailed ways

本申请通过提供无人机干扰设备的运行状态动态监测调节方法及系统,通过搭建基于无人机干扰设备的空间域,空间域基于设备射频范围进行配置,基于空间域的探测空间约束,结合探测运控模块,通过无人机干扰设备的无线电探测进行目标识别,生成识别响应,其中,所述探测运控模块用于控制无人机干扰设备进行无线电探测,再随着识别响应的接收,同步激活干扰运控模块,并配置基于干扰模式的干扰方案,再对目标无人机进行追踪定位,结合空间域的干扰空间约束,基于干扰方案进行目标无人机的无线电反制,确定目标干扰实况,并基于识别响应与目标干扰实况,提取回波反馈信号并进行运行状态评估,确定制动离轴度,然后若制动离轴度不满足阈值标准,针对制动离轴度进行溯源,确定标识有扰动度的运行扰动因素,最后基于运行扰动因素,进行无人机干扰设备的适应性运行调控。解决了现有技术中存在的无人机干扰设备由于不够严谨且完备性不足而导致无法根据运行状态进行动态调整的问题,实现了提高无人机干扰设备的稳定性。This application provides a method and system for dynamic monitoring and adjustment of the operating status of UAV interference equipment, and builds a space domain based on UAV interference equipment. The space domain is configured based on the radio frequency range of the equipment. Based on the detection space constraints of the space domain, combined with detection The operation control module performs target identification through radio detection of UAV interference equipment and generates an identification response. The detection operation control module is used to control the UAV interference equipment to perform radio detection, and then synchronizes with the reception of the identification response. Activate the interference operation control module and configure the interference scheme based on the interference mode, and then track and locate the target UAV. Combined with the interference space constraints in the space domain, carry out radio countermeasures for the target UAV based on the interference scheme to determine the actual situation of target interference. , and based on the recognition response and the target interference situation, the echo feedback signal is extracted and the operating status is evaluated to determine the braking off-axis degree. Then, if the braking off-axis degree does not meet the threshold standard, the source of the braking off-axis degree is traced and determined. Identify operational disturbance factors with a degree of disturbance, and finally conduct adaptive operation control of UAV interference equipment based on the operational disturbance factors. This solves the problem in the existing technology that the UAV interference equipment cannot be dynamically adjusted according to the operating status due to insufficient rigor and completeness, thereby improving the stability of the UAV interference equipment.

实施例一,如图1所示,本申请提供了无人机干扰设备的运行状态动态监测调节方法及系统,方法包括:Embodiment 1, as shown in Figure 1, this application provides a method and system for dynamic monitoring and adjustment of the operating status of drone interference equipment. The method includes:

搭建基于无人机干扰设备的空间域,所述空间域基于设备射频范围进行配置;Build a space domain based on drone interference equipment, which is configured based on the radio frequency range of the equipment;

无人机干扰设备的空间域是指无人机干扰设备的工作范围,根据无人机干扰设备的射频范围进行设置。其中,射频范围是无人机干扰设备干扰能力的重要指标,在对空间域进行搭建时,需保证射频范围能够覆盖无人机的干扰范围确保能够对无人机进行干扰。对无人机干扰设备的射频范围进行获取,并根据无人机的设备范围进行无人机干扰设备的空间范围进行设定,得到无人机干扰设备的空间域。无人机干扰设备的空间域可以根据设备射频范围进行任意划分,并根据实际情况进行相应的无人机干扰设备的空间域搭建,在确定坐标系后,得到空间坐标系,根据空间坐标系生成对应的坐标空间,将坐标空间输出得到无人机干扰设备的空间域。空间域的获取为后续基于空间域的探测空间约束,结合探测运控模块,通过无人机干扰设备的无线电探测进行目标识别,生成识别响应提供数据基础。The spatial domain of the UAV interference device refers to the working range of the UAV interference device, which is set according to the radio frequency range of the UAV interference device. Among them, the radio frequency range is an important indicator of the interference capability of UAV interference equipment. When building the space domain, it is necessary to ensure that the radio frequency range can cover the interference range of the UAV to ensure that the UAV can be interfered. The radio frequency range of the UAV interference equipment is obtained, and the spatial range of the UAV interference equipment is set according to the equipment range of the UAV to obtain the spatial domain of the UAV interference equipment. The spatial domain of the UAV interference equipment can be arbitrarily divided according to the radio frequency range of the equipment, and the corresponding spatial domain of the UAV interference equipment can be constructed according to the actual situation. After determining the coordinate system, the spatial coordinate system is obtained and generated according to the spatial coordinate system. Corresponding coordinate space, output the coordinate space to obtain the spatial domain of the drone interference device. The acquisition of the spatial domain provides a data basis for subsequent detection space constraints based on the spatial domain. Combined with the detection operation control module, target identification is performed through radio detection of UAV jamming equipment, and identification responses are generated.

基于空间域的探测空间约束,结合探测运控模块,通过无人机干扰设备的无线电探测进行目标识别,生成识别响应,其中,所述探测运控模块用于控制无人机干扰设备进行无线电探测;Based on the detection space constraints in the spatial domain, combined with the detection operation and control module, target identification is performed through radio detection of UAV jamming equipment, and an identification response is generated. The detection operation and control module is used to control the UAV interference equipment to perform radio detection. ;

基于空间域的探测空间约束是一种利用物理空间的信息来约束探测和识别的约束,无人机干扰设备在对无人机进行干扰时不能对所有空间域中的物体进行干扰,这样效率过低,对干扰加以限制,将对无人机的干扰按照设定的方式进行,并结合探测运控模块与无人机干扰设备的无线电探测,可以实现更高效和准确的目标识别。其中,探测运控模块用于控制无人机干扰设备进行无线电探测,并通过无人机干扰设备的无线电探测进行目标识别,在无线电探测完成目标识别后,获取目标识别结果,将目标识别结果进行获取,并根据目标识别结果生成相应的识别响应,表示目标为无人机,并对后续随着识别响应的接收,同步激活干扰运控模块,并配置基于干扰模式的干扰方案,其中,干扰模式包括迫降模式、返航模式与飞控干扰模式提供数据基础。The detection space constraint based on the spatial domain is a constraint that uses physical space information to constrain detection and identification. When the UAV jamming equipment interferes with the UAV, it cannot interfere with all objects in the spatial domain. This is too efficient. Low, the interference is limited, the interference of the drone is carried out in a set way, and the radio detection of the detection operation control module and the drone jamming equipment can be combined to achieve more efficient and accurate target identification. Among them, the detection operation control module is used to control the UAV jamming equipment to conduct radio detection, and perform target identification through the radio detection of the UAV interference equipment. After the radio detection completes the target identification, the target identification result is obtained, and the target identification result is Obtain and generate a corresponding recognition response based on the target recognition result, indicating that the target is a UAV, and with the subsequent receipt of the recognition response, the interference operation control module is activated synchronously, and an interference scheme based on the interference mode is configured, where the interference mode Including forced landing mode, return mode and flight control interference mode to provide data basis.

随着所述识别响应的接收,同步激活干扰运控模块,并配置基于干扰模式的干扰方案,其中,所述干扰模式包括迫降模式、返航模式与飞控干扰模式,所述干扰运控模块用于接收识别相应,并对当前干扰方式进行判断和干扰方案配置;With the reception of the identification response, the interference operation control module is activated synchronously and an interference scheme based on interference modes is configured. The interference modes include forced landing mode, return mode and flight control interference mode. The interference operation control module uses Correspond to the receiving identification, judge the current interference mode and configure the interference plan;

在对识别相应进行接收后,对干扰运控模块进行激活,干扰运控模块用于接收识别相应,并对当前干扰方式进行判断,获取判断结果,并根据判断结果进行干扰方案配置。构建干扰方案数据库,干扰方案数据库中存在多种干扰方案,用户可根据实际情况对干扰模式进行选择,并对当前干扰模式进行确认,并根据干扰模式对干扰方案进行相应的选取,完成对干扰方案的配置。干扰模式分为三种,迫降模式、返航模式与飞控干扰模式,迫降模式为对无人机进行信号干扰,并使无人机进行急速降落;返航模式为对无人机进行方向干扰,对无人机进行驱离,离开无人机干扰设备的空间域;飞控干扰模式为对无人机的飞控进行干扰,导致无人机在飞行过程中无法稳定,出现坠机等情况。干扰方案的确定,为后续对目标无人机进行追踪定位,结合空间域的干扰空间约束,基于干扰方案进行目标无人机的无线电反制,确定目标干扰实况提供数据基础。After receiving the identification response, the interference operation control module is activated. The interference operation control module is used to receive the identification response, judge the current interference method, obtain the judgment result, and configure the interference plan according to the judgment result. Construct an interference scheme database. There are multiple interference schemes in the interference scheme database. Users can select the interference mode according to the actual situation, confirm the current interference mode, and select the interference scheme accordingly according to the interference mode to complete the interference scheme. Configuration. There are three interference modes: forced landing mode, return mode and flight control interference mode. The forced landing mode interferes with the signal of the UAV and makes the UAV land rapidly; the return mode interferes with the direction of the UAV and causes it to land rapidly. The drone is driven away and leaves the space domain of the drone interference device; the flight control interference mode is to interfere with the flight control of the drone, causing the drone to become unstable during flight and crash. The determination of the interference plan provides a data basis for subsequent tracking and positioning of the target UAV, combined with the interference space constraints in the space domain, radio countermeasures for the target UAV based on the interference plan, and determining the actual situation of target interference.

对目标无人机进行追踪定位,结合空间域的干扰空间约束,基于所述干扰方案进行所述目标无人机的无线电反制,确定目标干扰实况;Track and locate the target UAV, combine the interference space constraints in the space domain, conduct radio countermeasures for the target UAV based on the interference plan, and determine the actual situation of target interference;

对目标无人机进行追踪定位,需要采集目标无人机的位置信息,并获取目标无人机的速度和方向信息,通过GPS对无人机位置进行确定,并获取无人机位置信息,通过位置信息对目标无人机的速度进行计算,得到目标无人机的速度信息,并根据速度信息进行目标无人机的方向信息确定,得到方向信息,根据目标无人机的位置信息、速度信息和方向信息对目标无人机进行追踪定位。将空间域的干扰空间约束进行获取,并根据空间域的干扰空间约束对目标无人机发射干扰信号,根据空间域的干扰空间约束对信号发射方向和信号剂量进行控制,使发射方向和发射剂量达到预设的干扰效果,并对干扰过程进行监控,确定目标干扰实况,对后续基于识别响应与目标干扰实况,提取回波反馈信号并进行运行状态评估,确定制动离轴度提供数据基础。To track and locate the target UAV, it is necessary to collect the position information of the target UAV, obtain the speed and direction information of the target UAV, determine the position of the UAV through GPS, and obtain the UAV position information through The position information calculates the speed of the target UAV to obtain the speed information of the target UAV, and determines the direction information of the target UAV based on the speed information to obtain the direction information. Based on the position information and speed information of the target UAV, and direction information to track and locate the target drone. The interference space constraints in the space domain are obtained, and the interference signal is emitted to the target UAV according to the interference space constraints in the space domain. The signal emission direction and signal dose are controlled according to the interference space constraints in the space domain, so that the emission direction and emission dose are Achieve the preset interference effect, monitor the interference process, determine the actual target interference, and provide a data basis for subsequent extraction of echo feedback signals and operating status evaluation based on the recognition response and the actual target interference, and determine the braking off-axis degree.

基于所述识别响应与所述目标干扰实况,提取回波反馈信号并进行运行状态评估,确定制动离轴度,所述制动离轴度为预期控制效果与实际控制效果之间的差值;Based on the recognition response and the target interference situation, the echo feedback signal is extracted and the operating status is evaluated to determine the braking off-axis degree, which is the difference between the expected control effect and the actual control effect. ;

对被干扰的无人机进行运行状态评估,判断被干扰无人机的干扰情况,对回波反馈信号进行提取,回波反馈信号包括被干扰无人机的反射信号和无人机干扰设备的发射信号的混合信号。通过识别响应与目标干扰实况分析结果,对回波反馈信号进行提取,获取回波反馈信号,并对回波反馈信号进行信号处理,获取信号处理结果,并对信号处理结果的回波反馈信号进行特征提取,得到回波反馈信号的信号特征。对反馈信号的信号特征进行评估,其中,评估指标包括干扰效果、功耗、稳定性等,基于运行状态评估效果,对制动离轴度进行确定,其中制动离轴度是指预期控制效果与实际控制效果之间的差值。制动离轴度的确定为后续若制动离轴度不满足阈值标准,针对制动离轴度进行溯源,确定标识有扰动度的运行扰动因素提供数据基础。Evaluate the operating status of the interfered UAV, determine the interference situation of the interfered UAV, and extract the echo feedback signal. The echo feedback signal includes the reflected signal of the interfered UAV and the interference signal of the UAV jamming equipment. A mixed signal that emits a signal. By identifying the response and target interference live analysis results, the echo feedback signal is extracted, the echo feedback signal is obtained, the echo feedback signal is signal processed, the signal processing result is obtained, and the echo feedback signal of the signal processing result is processed Feature extraction to obtain the signal characteristics of the echo feedback signal. Evaluate the signal characteristics of the feedback signal. The evaluation indicators include interference effects, power consumption, stability, etc. Based on the operating status evaluation effect, the braking off-axis degree is determined, where the braking off-axis degree refers to the expected control effect. The difference between the actual control effect. The determination of the braking off-axis degree provides a data basis for tracing the source of the braking off-axis degree and determining the operating disturbance factors that indicate the degree of disturbance if the braking off-axis degree does not meet the threshold standard.

若所述制动离轴度不满足阈值标准,针对所述制动离轴度进行溯源,确定标识有扰动度的运行扰动因素;If the braking off-axis degree does not meet the threshold standard, trace the source of the braking off-axis degree and determine the operating disturbance factors marked with the degree of disturbance;

设置制动离轴度阈值,制动离轴度阈值为制动离轴度最低合格标准,低于制动离轴度阈值则表示当前无人机干扰设备对无人机干扰效果较差,需要对该无人机干扰设备进行调整。当制动离轴度不满足制动离轴度阈值时,对制动离轴度进行溯源,即对制动离轴度中的回波反馈信号进行获取,并对造成回波反馈信号的无人机干扰设备的参数进行获取,并对原因进行分析,获取造成回波反馈信号的原因,即运行扰动因素,并根据运行扰动因素对扰动因素进行特征提取,获取扰动因素的特征,对扰动因素的特征进行扰动度判断,获取扰动因素的扰动度,得到带有扰动度标识的运行扰动因素。运行扰动因素的获取,为后续基于运行扰动因素,进行无人机干扰设备的适应性运行调控提供数据基础。Set the braking off-axis threshold. The braking off-axis threshold is the minimum qualifying standard for braking off-axis. If it is lower than the braking off-axis threshold, it means that the current UAV interference device has poor interference effect on the UAV. It is necessary to Make adjustments to the drone jamming equipment. When the braking off-axis degree does not meet the braking off-axis degree threshold, the source of the braking off-axis degree is traced, that is, the echo feedback signal in the braking off-axis degree is obtained, and the error that causes the echo feedback signal is detected. Obtain the parameters of the human-machine interference equipment and analyze the causes to obtain the causes of the echo feedback signals, that is, operating disturbance factors, and extract features of the disturbance factors based on the operating disturbance factors to obtain the characteristics of the disturbance factors and analyze the disturbance factors The characteristics of the system are used to judge the degree of disturbance, obtain the degree of disturbance of the disturbance factors, and obtain the operating disturbance factors with disturbance degree identification. The acquisition of operational disturbance factors provides a data basis for subsequent adaptive operation control of UAV interference equipment based on operational disturbance factors.

基于所述运行扰动因素,对所述无人机干扰设备进行适应性运行调控。Based on the operation disturbance factors, adaptive operation control of the UAV interference equipment is performed.

根据运行扰动因素,对无人机干扰设备进行相应的调控,其中运行扰动因素具有多种,如环境温度、风速、气压、无人机类型等,举例而言,在风速较大的场景中,无人机会出现摇摆不定,无法维持在稳定位置的情况,导致无人机干扰设备无法对目标无人机进行稳定和准确的干扰,当无人机是抗干扰能力较强类型的无人机时,所需要无人机干扰设备的功耗也要增加,且干扰效果也会相对应的下降。针对不同的运行扰动因素需要的不同的运行调控方法,运行调控方法包括但不限于调整信号频率,不同的无人机使用的通信信号频率不同,通过对干扰设备进行信号频率的调整,可以实现对不同无人机的有效干扰;控制信号功率:信号功率过大可能会对其他电子设备造成干扰,过小则可能无法对无人机产生有效影响,需要根据实际情况对信号功率进行灵活调整;调整干扰模式:根据无人机的类型和数量,选择合适的干扰模式。例如,对于群体无人机,可以使用协同干扰模式,对于单个无人机,可以使用定向干扰模式。对运行扰动因素进行分析,获取与运行扰动因素相对应的运行调控方法,完成对无人机干扰设备的适应性运行调控,能够进一步提高对无人机干扰设备的干扰效果,提高无人机的干扰效率。UAV interference equipment is regulated accordingly based on operational disturbance factors. There are many operational disturbance factors, such as ambient temperature, wind speed, air pressure, UAV type, etc. For example, in a scene with high wind speed, The drone will be unstable and unable to maintain a stable position, causing the drone jamming equipment to be unable to stably and accurately interfere with the target drone. When the drone is a type of drone with strong anti-interference ability , the power consumption of the required drone interference equipment will also increase, and the interference effect will decrease accordingly. Different operation control methods are required for different operation disturbance factors. The operation control methods include but are not limited to adjusting the signal frequency. Different UAVs use different communication signal frequencies. By adjusting the signal frequency of the interference equipment, the control method can be achieved. Effective interference of different drones; control signal power: too large a signal power may cause interference to other electronic equipment, while too small a signal power may not have an effective impact on the drone. The signal power needs to be flexibly adjusted according to the actual situation; adjustment Interference mode: Select the appropriate interference mode according to the type and number of drones. For example, for a group of UAVs, the cooperative interference mode can be used, and for a single UAV, the directional interference mode can be used. Analyze the operating disturbance factors, obtain the operation control methods corresponding to the operation disturbance factors, and complete the adaptive operation control of the UAV interference equipment, which can further improve the interference effect of the UAV interference equipment and improve the UAV's interference efficiency.

进一步而言,所述方法还包括:Furthermore, the method further includes:

以所述无人机干扰设备的布设空间为基准,以设备布设位置为原点,确定空间轴向;Use the layout space of the drone interference equipment as the benchmark and the equipment layout position as the origin to determine the spatial axis;

基于所述空间轴向搭建空间坐标系,对所述空间坐标系进行经纬度定位拟合,确定拟合坐标系;Build a spatial coordinate system based on the spatial axis, perform longitude and latitude positioning fitting on the spatial coordinate system, and determine the fitting coordinate system;

读取所述无人机干扰设备的探测范围与干扰范围,对所述拟合坐标系进行空间约束,生成所述空间域。Read the detection range and interference range of the UAV interference device, perform spatial constraints on the fitting coordinate system, and generate the spatial domain.

在生成空间域时,需要先建立坐标系,并根据坐标系对空间域进行生成,根据坐标系对空间域进行生成,能够对空间域中的无人机进行定位,为后续对无人机进行定位跟踪提供数据基础。将无人机干扰设备的布设位置设为坐标原点,并以无人机干扰设备所在平面为水平面,将水平面作为基准进行空间轴向确认,垂直于水平面进行Z轴构建,并基于Z轴进行相应的X轴和Y轴构建,且X轴和Y轴在水平面中,将空间坐标系的X轴和Y轴与地球经纬度进行重合,完成空间坐标系的经纬度定位重合,获取重合结果,对你和坐标系进行确定。再将无人机干扰设备的探测范围进行获取,在拟合坐标系中以原点为圆心,以无人机干扰设备的探测范围为半径,在拟合空间坐标系中进行球体构建,获取地面上的半球体,该半球体的内部范围即为实际探测范围;同理可得,再将无人机干扰设备的干扰范围进行获取,在拟合坐标系中以原点为圆心,以无人机干扰设备的干扰范围为半径,在拟合空间坐标系中进行球体构建,获取地面上的半球体,该半球体的内部范围为实际干扰范围,即完成对你和坐标系进行空间约束,得到空间域,空间域包括实际探测范围和实际干扰范围。空间域的生成为后续基于空间域的探测空间约束,结合探测运控模块,通过无人机干扰设备的无线电探测进行目标识别,生成识别响应提供数据基础。When generating a spatial domain, it is necessary to first establish a coordinate system and generate the spatial domain according to the coordinate system. Generating the spatial domain according to the coordinate system can position the UAV in the spatial domain and provide a basis for subsequent operations on the UAV. Location tracking provides the data foundation. Set the layout position of the UAV interference equipment as the origin of the coordinates, take the plane where the UAV interference equipment is located as the horizontal plane, use the horizontal plane as the benchmark to confirm the spatial axis, construct the Z-axis perpendicular to the horizontal plane, and perform corresponding operations based on the Z-axis The X-axis and Y-axis are constructed, and the X-axis and Y-axis are in the horizontal plane. Coinciding the X-axis and Y-axis of the spatial coordinate system with the longitude and latitude of the earth, complete the positioning coincidence of the longitude and latitude of the spatial coordinate system, and obtain the coincidence result, which is useful for you and The coordinate system is determined. Then obtain the detection range of the UAV jamming equipment, take the origin as the center of the circle in the fitting coordinate system, take the detection range of the UAV interference equipment as the radius, construct a sphere in the fitting space coordinate system, and obtain the is a hemisphere, and the internal range of the hemisphere is the actual detection range; in the same way, the interference range of the UAV interference device is obtained. In the fitting coordinate system, the origin is the center of the circle, and the interference range of the UAV is The interference range of the device is the radius. Construct a sphere in the fitting space coordinate system to obtain the hemisphere on the ground. The internal range of the hemisphere is the actual interference range. That is, the spatial constraints on you and the coordinate system are completed, and the spatial domain is obtained. , the spatial domain includes the actual detection range and the actual interference range. The generation of the spatial domain provides a data basis for subsequent detection space constraints based on the spatial domain. Combined with the detection operation and control module, target identification is performed through radio detection of UAV jamming equipment, and identification responses are generated.

进一步而言,所述方法还包括:Furthermore, the method further includes:

配置干扰数据库,其中,所述干扰数据库包括存在一对多关系的表征为干扰模式-预干扰方案多个序列;Configure an interference database, wherein the interference database includes multiple sequences characterized by interference patterns-pre-interference schemes that have a one-to-many relationship;

以所述识别响应为约束,以干扰模式为需求,遍历所述干扰数据库进行匹配,确定所述干扰方案。With the identification response as a constraint and the interference pattern as a requirement, the interference database is traversed for matching to determine the interference plan.

在对干扰方案进行确定时,需对干扰方案进行整理,建立干扰方案数据库,并建立干扰数据库中各数据方案的对应关系,根据识别响应,在干扰方案数据库中进行遍历,获取相应的干扰方案,提高干扰方案的确定效率,进一步提高整体系统的效率。将干扰模式与干扰方案进行对应关系构建由于干扰方案还未执行,所以将干扰方案作为预干扰方案,获取干扰模式-预干扰方案序列。举例而言,干扰模式分为迫降模式、返航模式与飞控干扰模式,其中返航模式对应的干扰方式包括GPS压制式干扰,即对发射与GPS卫星同频率的大功率信号,使无人机GPS接收机模块饱和,使无人机进行迫降;也同样对应阻塞式干扰,阻塞式干扰是利用噪声信号对对方接收机进行扰乱,在时域、频域、变换域上实现对回波的完全覆盖,使对方雷达无法捕获有效的回波信息,完成对无人机的迫降。获取多个干扰模式-预干扰方案序列,并将多个干扰模式-预干扰方案序列组合为干扰数据库。根据对识别响应进行特征提取,根据识别相应特征对干扰模式进行特征匹配,获取匹配结果,根据匹配结果在干扰数据库中进行遍历,获取匹配的干扰模式,并根据干扰模式对应的多个序列,获取干扰方案,能够提高干扰方案的确定效率,进一步提高整体系统的效率。When determining the interference scheme, it is necessary to organize the interference scheme, establish an interference scheme database, and establish the corresponding relationship between each data scheme in the interference database. According to the identification response, traverse the interference scheme database to obtain the corresponding interference scheme. Improve the efficiency of determining interference plans and further improve the efficiency of the overall system. Construct a corresponding relationship between the interference mode and the interference plan. Since the interference plan has not yet been executed, the interference plan is used as the pre-interference plan to obtain the interference mode-pre-interference plan sequence. For example, the interference modes are divided into forced landing mode, return mode and flight control interference mode. Among them, the interference methods corresponding to the return mode include GPS suppressive interference, that is, transmitting high-power signals with the same frequency as GPS satellites, making the UAV GPS The receiver module is saturated, causing the UAV to make an emergency landing; it also corresponds to blocking interference. Blocking interference uses noise signals to disrupt the other party's receiver, achieving complete coverage of the echo in the time domain, frequency domain, and transform domain. , so that the other party's radar cannot capture effective echo information and complete the emergency landing of the UAV. Multiple interference pattern-pre-interference scheme sequences are obtained, and the multiple interference pattern-pre-interference scheme sequences are combined into an interference database. Extract features based on the recognition response, perform feature matching on the interference pattern based on the identified corresponding features, obtain the matching results, traverse the interference database based on the matching results, obtain the matching interference patterns, and obtain the matching interference patterns based on the multiple sequences corresponding to the interference patterns. The interference plan can improve the efficiency of determining the interference plan and further improve the efficiency of the overall system.

进一步而言,所述方法还包括:Furthermore, the method further includes:

配置运控偏离溯源模组,所述运控偏离溯源模组包括抗干扰分析模块、运控偏差分析模块与环境场域干扰分析模块,其中,所述抗干扰分析模块、所述运控偏差分析模块与所述环境场域干扰分析模块分别用于分析无人机自身的抗干扰能力、无人机干扰设备自身的控制偏差,无人机干扰设备工作环境受到的磁场干扰;Configure an operation control deviation traceability module. The operation control deviation traceability module includes an anti-interference analysis module, an operation control deviation analysis module and an environmental field interference analysis module. The anti-interference analysis module, the operation control deviation analysis module The module and the environmental field interference analysis module are respectively used to analyze the anti-interference ability of the drone itself, the control deviation of the drone interference equipment itself, and the magnetic field interference in the working environment of the drone interference equipment;

将所述回波反馈信号传输至所述运控偏离溯源模组中,进行模块独立分析确定单项溯源结果,其中,所述单项溯源结果与各分析模块一一对应;The echo feedback signal is transmitted to the operation control deviation traceability module, and the module is independently analyzed to determine the single traceability result, where the single traceability result corresponds to each analysis module one-to-one;

对所述单项溯源结果进行同向拟合,确定所述运行扰动因素。Perform in-line fitting on the single traceability results to determine the operating disturbance factors.

导致无人机干扰设备的制动离轴度有很多原因,包括无人机自身具有一定的抗干扰能力,无人机干扰设备自身的控制偏差,与无人机干扰设备的工作环境受到的磁场干扰,针对无人机干扰设备的制动离轴度原因,分别生成相应的解决该对应问题的解决模块,即抗干扰分析模块、运控偏差分析模块与环境场域干扰分析模块。将抗干扰分析模块、运控偏差分析模块与环境场域干扰分析模块进行组合构建运控偏离溯源模组,运控偏离溯源模组根据接收到的回波反馈信号进行制动离轴度分析,将回波反馈信号发送至运控偏离溯源模组中的三个分析模块中,三个分析模块分别对回波反馈信号进行原因分析,判断导致无人机干扰设备的制动离轴度的原因,并获得分析结果,分别将分析结果进行获取,并对三个分析结果进行结果拟合,抗干扰分析模块、运控偏差分析模块与环境场域干扰分析模块得到的对应分析结果为单项溯源结果,且单项溯源结果与对其分析的分析模块具有一一对应的关系。将各分析模块的单项溯源结果进行拟合,即将三个模块得到的分析结果进行整合,对各个模块额单项溯源结果进行特征提取,获取各单项溯源结果的同偏离方向特征,即针对相同的问题进行分析获得的分析结果的特征,根据同偏离方向特征将相同偏离方向特征的单项溯源结果进行整合,得到运行扰动因素,完成对单项溯源结果的同向拟合,通过构建多个分析模块对制动离轴度进行分析,能够极大地提高分析的精确度和效率。There are many reasons for the off-axis braking of UAV interference equipment, including the UAV itself having a certain anti-interference ability, the control deviation of the UAV interference equipment itself, and the magnetic field in the working environment of the UAV interference equipment. Interference, in view of the reasons for the braking off-axis degree of the UAV interference equipment, corresponding solution modules are generated to solve the corresponding problems, namely the anti-interference analysis module, the operation control deviation analysis module and the environmental field interference analysis module. The anti-interference analysis module, operation control deviation analysis module and environmental field interference analysis module are combined to build an operation control deviation traceability module. The operation control deviation traceability module performs braking off-axis analysis based on the received echo feedback signal. The echo feedback signal is sent to the three analysis modules in the operation control deviation traceability module. The three analysis modules perform cause analysis on the echo feedback signal respectively to determine the cause of the UAV interfering with the braking off-axis of the equipment. , and obtain the analysis results, obtain the analysis results respectively, and perform result fitting on the three analysis results. The corresponding analysis results obtained by the anti-interference analysis module, operation control deviation analysis module and environmental field interference analysis module are single traceability results. , and there is a one-to-one correspondence between the single traceability result and the analysis module that analyzes it. Fit the single traceability results of each analysis module, that is, integrate the analysis results obtained by the three modules, perform feature extraction on the single traceability results of each module, and obtain the same deviation direction characteristics of each single traceability result, that is, for the same problem Analyze the characteristics of the analysis results obtained, integrate the single traceability results of the same deviation direction characteristics according to the same deviation direction characteristics, obtain the operating disturbance factors, complete the same direction fitting of the single traceability results, and build multiple analysis modules to control the system Analyzing off-axis motion can greatly improve the accuracy and efficiency of analysis.

进一步而言,所述方法还包括:Furthermore, the method further includes:

进行工业互联网检索,确定无人机干扰日志;Conduct an industrial Internet search to determine drone interference logs;

基于所述无人机干扰日志,提取映射对应的样本无线电射频信号、样本回波反馈信号与样本抗干扰数据;Based on the UAV interference log, extract and map the corresponding sample radio frequency signals, sample echo feedback signals and sample anti-interference data;

基于所述样本无线电射频信号与所述样本回波反馈信号随机提取一项,作为决策数据并搭建第一决策层;Randomly extract one item based on the sample radio frequency signal and the sample echo feedback signal as decision-making data and build the first decision-making layer;

重复迭代,完成第N决策层的搭建,并进行所述第一决策层直至所述第N决策层的层级连接,基于所述样本抗干扰数据进行匹配标识,生成抗干扰决策树;Repeat the iteration to complete the construction of the Nth decision-making layer, and perform hierarchical connections from the first decision-making layer to the Nth decision-making layer, perform matching identification based on the sample anti-interference data, and generate an anti-interference decision tree;

基于所述抗干扰决策树,生成所述抗干扰分析模块。Based on the anti-interference decision tree, the anti-interference analysis module is generated.

在工业互联网中进行搜索,获取大量样本数据,对无人机干扰日志进行搜索,获取无人机干扰日志,无人机干扰日志中包括大量无线电射频信号、回波反馈信号和抗干扰数据,其中样本抗干扰数据为对无人机进行干扰时所生成的总体数据,不同干扰情况对应的抗干扰数据不同,根据不同的抗干扰数据可进行构建不同的分析模块,将无人机干扰日志中的无线电射频信号、回波反馈信号和抗干扰数据进行提取,得到样本无线电射频信号、样本回波反馈信号与样本抗干扰数据。从样本无线电射频信号与样本回波反馈信号中随机进行提取,得到任意一项数据,并将该数据最为决策数据进行第一决策层的构建,并继续从样本无线电射频信号与样本回波反馈信号中随机进行提取,得到任意一项数据,并将该数据最为决策数据进行第二决策层的构建,并将第一决策层与第二决策层进行连接,同理可得,将决策层进行多层构建,且在每层之间构建层级连接,建立每层决策层之间的联系,并将样本抗干扰数据与决策层进行匹配,获取匹配结果,并按照匹配结果进行标识,根据样本抗干扰数据和多个决策层进行决策树构建,将样本干扰数据按照匹配标识作为决策结果,得到抗干扰决策树。将抗干扰决策树作为抗干扰分析模块,生成抗干扰分析模块。抗干扰分析模块的生成,为后续配置运控偏离溯源模组,将回波反馈信号传输至运控偏离溯源模组中,进行模块独立分析确定单项溯源结果,其中,单项溯源结果与各分析模块一一对应提供数据基础。Search in the industrial Internet to obtain a large amount of sample data. Search the UAV interference log to obtain the UAV interference log. The UAV interference log includes a large number of radio frequency signals, echo feedback signals and anti-interference data, among which The sample anti-interference data is the overall data generated when interfering with the drone. Different interference situations correspond to different anti-interference data. Different analysis modules can be constructed based on different anti-interference data to combine the data in the drone interference log. Radio frequency signals, echo feedback signals and anti-interference data are extracted to obtain sample radio frequency signals, sample echo feedback signals and sample anti-interference data. Randomly extract any data from the sample radio frequency signal and sample echo feedback signal, and use this data as decision-making data to construct the first decision-making layer, and continue to extract the sample radio frequency signal and sample echo feedback signal Extract randomly to obtain any item of data, use this data as decision-making data to construct the second decision-making layer, and connect the first decision-making layer with the second decision-making layer. In the same way, the decision-making layer can be Layer construction, and build hierarchical connections between each layer, establish the connection between each layer of decision-making layers, match the sample anti-interference data with the decision-making layer, obtain the matching results, and identify them according to the matching results, and anti-interference based on the samples The data and multiple decision-making layers are used to construct a decision tree, and the sample interference data is used as the decision result according to the matching identification to obtain an anti-interference decision tree. Use the anti-interference decision tree as the anti-interference analysis module to generate an anti-interference analysis module. The generation of the anti-interference analysis module is for subsequent configuration of the operation control deviation traceability module. The echo feedback signal is transmitted to the operation control deviation traceability module, and the module is independently analyzed to determine the single traceability result. Among them, the single traceability result is consistent with each analysis module. One-to-one correspondence provides data basis.

进一步而言,所述方法还包括:Furthermore, the method further includes:

确定所述无人机干扰设备的底层运控逻辑与操作规则,确定调控约束;Determine the underlying operation control logic and operating rules of the drone interference equipment, and determine regulatory constraints;

读取所述无人机干扰设备的运控自由度,确定调控范围;Read the degree of freedom of operation and control of the drone interference equipment and determine the control range;

基于所述调控约束与所述调控范围,针对所述运行扰动因素进行运控调整寻优,确定目标调控方案。Based on the control constraints and the control range, the operation control adjustment and optimization is performed according to the operation disturbance factors to determine the target control plan.

针对无人机干扰设备的底层运控逻辑与操作规则,需要确定相应的调控约束和调控范围,调控约束通常包括设备的最大输出功率、最小干扰距离、干扰模式的选择等。而调控范围则可以根据无人机干扰设备的运控自由度进行设定,无人机干扰设备的运控自由度是指无人机干扰设备可以进行干扰参数设置的允许范围,在允许范围内选择合适的信号频率和信号功率等。根据调控约束和调控范围进行相应的调整空间构建,并在调整空间中对运行扰动因素进行调整方案生成,并对调整方案进行筛选和优化,得到目标调控方案,针对运行扰动因素且在调控约束和运控自由度的限制内,所得到的目标调控该方案具有合理性和可行性,减少因调整方案超出可实现范围而导致的无人机干扰设备干扰效果差的问题,进一步提高无人机干扰设备的可靠性。For the underlying operation control logic and operating rules of UAV interference equipment, it is necessary to determine the corresponding control constraints and control scope. Control constraints usually include the maximum output power of the equipment, the minimum interference distance, the selection of interference mode, etc. The control range can be set according to the freedom of operation and control of the UAV interference equipment. The freedom of operation and control of the UAV interference equipment refers to the allowable range within which the UAV interference equipment can set interference parameters. Within the allowable range Choose appropriate signal frequency and signal power, etc. According to the control constraints and control scope, the corresponding adjustment space is constructed, and the adjustment plan for the operating disturbance factors is generated in the adjustment space, and the adjustment plan is screened and optimized to obtain the target control plan. Within the limits of the degree of freedom of operation and control, the obtained target control scheme is reasonable and feasible, reducing the problem of poor interference effect of UAV interference equipment caused by adjusting the scheme beyond the achievable range, and further improving UAV interference. Equipment reliability.

进一步而言,所述方法还包括:Furthermore, the method further includes:

基于所述调控约束与所述调控范围,搭建寻优空间;Based on the control constraints and the control range, build an optimization space;

在所述寻优空间中,以所述运行扰动因素为基准,进行随机扰动,确定多个运行调控方案;In the optimization space, random disturbance is performed based on the operation disturbance factors to determine multiple operation control plans;

以调控能耗与操作难度为约束,以所述扰动度为响应目标搭建适应度函数,对所述运行调控方案进行适应度计量,择取最大适应度映射的目标调控方案。With the regulation energy consumption and operation difficulty as constraints, a fitness function is built with the disturbance degree as the response target, the fitness of the operation regulation scheme is measured, and the target regulation scheme with the maximum fitness mapping is selected.

根据调控约束与调控范围,进行空间域搭建得到搭建结果,搭建结果为寻优空间,在寻优空间中设置运行扰动因素,并将运行扰动因素设为随机触发,通过运行扰动因素对无人机干扰设备进行扰动,并根据扰动结果进行相应的调整,调整方法不唯一,即获得多个调整方法,将多个调整方法进行输出,得到多个运行调控方案。对多个调控方案进行筛选,制定筛选标准,筛选标准包括调控能耗和操作难度,其中调控能耗是指在对无人机干扰设备进行调控时所产生的能量消耗,而操作难度为对无人机干扰设备进行操作时的复杂程度。构建函数,将调控能耗操作难度与扰动度作为自变量,适应度作为因变量进行适应度函数搭建,适应度为该运行调控方案的可行性,构建调控能耗操作难度、扰动度与适应度之间的对应关系,对运行调控方案进行适应度判断,根据输入的调控能耗与操作难度择取最大适应度所对应的目标调控方案,根据适应度函数计算得到对应所述目标调控方案,能够最大限度的保证调控能耗与操作难度在合理的范围之内,且扰动度不会造成较为严重的影响,提高了整体系统的稳定性和效率。According to the control constraints and control scope, the space domain is constructed to obtain the construction result. The construction result is the optimization space. Operation disturbance factors are set in the optimization space, and the operation disturbance factors are set to random triggers. The UAV is affected by the operation disturbance factors. The interference equipment performs disturbance and makes corresponding adjustments according to the disturbance results. The adjustment method is not unique, that is, multiple adjustment methods are obtained, and multiple adjustment methods are output to obtain multiple operation control plans. Screen multiple control schemes and formulate screening criteria. The screening criteria include control energy consumption and operation difficulty. The control energy consumption refers to the energy consumption generated when controlling drone interference equipment, and the operation difficulty refers to the energy consumption for unmanned aerial vehicle interference equipment. The complexity of operating the human-machine interference device. Construct a function, using the difficulty of regulating energy consumption operations and the degree of disturbance as independent variables, and the fitness as the dependent variable to build a fitness function. The fitness degree is the feasibility of the operation control plan. Construct the difficulty of regulating energy consumption operations, degree of disturbance and degree of fitness. According to the corresponding relationship between each other, the fitness of the operation control scheme is judged, the target control scheme corresponding to the maximum fitness is selected according to the input control energy consumption and operation difficulty, and the corresponding target control scheme is calculated according to the fitness function, which can It ensures that the control energy consumption and operation difficulty are within a reasonable range to the greatest extent, and the degree of disturbance will not cause serious impacts, improving the stability and efficiency of the overall system.

实施例二,基于与前述实施例中无人机干扰设备的运行状态动态监测调节方法相同的发明构思,如图2所示,本申请提供了无人机干扰设备的运行状态动态监测调节系统,所述系统包括:Embodiment 2 is based on the same inventive concept as the method for dynamic monitoring and adjustment of the operating status of UAV interference equipment in the previous embodiment. As shown in Figure 2, this application provides a system for dynamic monitoring and adjustment of the operating status of UAV interference equipment. The system includes:

空间域搭建模块11:所述空间域搭建模块11用于搭建基于无人机干扰设备的空间域,所述空间域基于设备射频范围进行配置;Space domain construction module 11: The space domain construction module 11 is used to build a space domain based on UAV interference equipment, and the space domain is configured based on the radio frequency range of the equipment;

识别响应模块12:所述识别响应模块12用于基于空间域的探测空间约束,结合探测运控模块,通过无人机干扰设备的无线电探测进行目标识别,生成识别响应,其中,所述探测运控模块用于控制无人机干扰设备进行无线电探测;Identification response module 12: The identification response module 12 is used to detect space constraints based on the spatial domain. Combined with the detection operation control module, it performs target identification through radio detection of UAV jamming equipment and generates an identification response, wherein the detection operation The control module is used to control UAV jamming equipment for radio detection;

干扰方案模块13:所述干扰方案模块13用于随着所述识别响应的接收,同步激活干扰运控模块,并配置基于干扰模式的干扰方案,其中,所述干扰模式包括迫降模式、返航模式与飞控干扰模式,所述干扰运控模块用于接收识别相应,并对当前干扰方式进行判断和干扰方案配置;Interference scheme module 13: The interference scheme module 13 is used to activate the interference operation control module synchronously with the reception of the identification response, and configure an interference scheme based on interference modes, where the interference modes include forced landing mode and return mode. In accordance with the flight control interference mode, the interference operation control module is used to receive and identify the response, judge the current interference mode and configure the interference plan;

追踪定位模块14:所述追踪定位模块14用于对目标无人机进行追踪定位,结合空间域的干扰空间约束,基于所述干扰方案进行所述目标无人机的无线电反制,确定目标干扰实况;Tracking and positioning module 14: The tracking and positioning module 14 is used to track and position the target UAV. Combined with the interference space constraints in the space domain, it performs radio countermeasures for the target UAV based on the interference plan to determine the target interference. live;

状态评估模块15:所述状态评估模块15用于基于所述识别响应与所述目标干扰实况,提取回波反馈信号并进行运行状态评估,确定制动离轴度,所述制动离轴度为预期控制效果与实际控制效果之间的差值;State evaluation module 15: The state evaluation module 15 is used to extract the echo feedback signal and perform operating state evaluation based on the identification response and the target interference situation, and determine the braking off-axis degree. is the difference between the expected control effect and the actual control effect;

扰动因素模块16:所述扰动因素模块16用于若所述制动离轴度不满足阈值标准,针对所述制动离轴度进行溯源,确定标识有扰动度的运行扰动因素;Disturbance factor module 16: The disturbance factor module 16 is used to trace the source of the braking off-axis degree if the braking off-axis degree does not meet the threshold standard, and determine the operating disturbance factor with the disturbance degree marked;

运行调控模块17:所述运行调控模块17用于基于所述运行扰动因素,对所述无人机干扰设备进行适应性运行调控。Operation control module 17: The operation control module 17 is used to perform adaptive operation control of the UAV interference equipment based on the operation disturbance factors.

进一步的,空间域搭建模块11包括以下执行步骤:Further, the spatial domain building module 11 includes the following execution steps:

以所述无人机干扰设备的布设空间为基准,以设备布设位置为原点,确定空间轴向;Use the layout space of the drone interference equipment as the benchmark and the equipment layout position as the origin to determine the spatial axis;

基于所述空间轴向搭建空间坐标系,对所述空间坐标系进行经纬度定位拟合,确定拟合坐标系;Build a spatial coordinate system based on the spatial axis, perform longitude and latitude positioning fitting on the spatial coordinate system, and determine the fitting coordinate system;

读取所述无人机干扰设备的探测范围与干扰范围,对所述拟合坐标系进行空间约束,生成所述空间域。Read the detection range and interference range of the UAV interference device, perform spatial constraints on the fitting coordinate system, and generate the spatial domain.

进一步的,干扰方案模块13包括以下执行步骤:Further, the interference solution module 13 includes the following execution steps:

配置干扰数据库,其中,所述干扰数据库包括存在一对多关系的表征为干扰模式-预干扰方案多个序列;Configure an interference database, wherein the interference database includes multiple sequences characterized by interference patterns-pre-interference schemes that have a one-to-many relationship;

以所述识别响应为约束,以干扰模式为需求,遍历所述干扰数据库进行匹配,确定所述干扰方案。With the identification response as a constraint and the interference pattern as a requirement, the interference database is traversed for matching to determine the interference plan.

进一步的,扰动因素模块16包括以下执行步骤:Further, the disturbance factor module 16 includes the following execution steps:

配置运控偏离溯源模组,所述运控偏离溯源模组包括抗干扰分析模块、运控偏差分析模块与环境场域干扰分析模块,其中,所述抗干扰分析模块、所述运控偏差分析模块与所述环境场域干扰分析模块分别用于分析无人机自身的抗干扰能力、无人机干扰设备自身的控制偏差,无人机干扰设备工作环境受到的磁场干扰;Configure an operation control deviation traceability module. The operation control deviation traceability module includes an anti-interference analysis module, an operation control deviation analysis module and an environmental field interference analysis module. The anti-interference analysis module, the operation control deviation analysis module The module and the environmental field interference analysis module are respectively used to analyze the anti-interference ability of the drone itself, the control deviation of the drone interference equipment itself, and the magnetic field interference in the working environment of the drone interference equipment;

将所述回波反馈信号传输至所述运控偏离溯源模组中,进行模块独立分析确定单项溯源结果,其中,所述单项溯源结果与各分析模块一一对应;The echo feedback signal is transmitted to the operation control deviation traceability module, and the module is independently analyzed to determine the single traceability result, where the single traceability result corresponds to each analysis module one-to-one;

对所述单项溯源结果进行同向拟合,确定所述运行扰动因素。Perform in-line fitting on the single traceability results to determine the operating disturbance factors.

进一步的,扰动因素模块16包括以下执行步骤:Further, the disturbance factor module 16 includes the following execution steps:

进行工业互联网检索,确定无人机干扰日志;Conduct an industrial Internet search to determine drone interference logs;

基于所述无人机干扰日志,提取映射对应的样本无线电射频信号、样本回波反馈信号与样本抗干扰数据;Based on the UAV interference log, extract and map the corresponding sample radio frequency signals, sample echo feedback signals and sample anti-interference data;

基于所述样本无线电射频信号与所述样本回波反馈信号随机提取一项,作为决策数据并搭建第一决策层;Randomly extract one item based on the sample radio frequency signal and the sample echo feedback signal as decision-making data and build the first decision-making layer;

重复迭代,完成第N决策层的搭建,并进行所述第一决策层直至所述第N决策层的层级连接,基于所述样本抗干扰数据进行匹配标识,生成抗干扰决策树;Repeat the iteration to complete the construction of the Nth decision-making layer, and perform hierarchical connections from the first decision-making layer to the Nth decision-making layer, perform matching identification based on the sample anti-interference data, and generate an anti-interference decision tree;

基于所述抗干扰决策树,生成所述抗干扰分析模块。Based on the anti-interference decision tree, the anti-interference analysis module is generated.

进一步的,运行调控模块17包括以下执行步骤:Further, the operation control module 17 includes the following execution steps:

确定所述无人机干扰设备的底层运控逻辑与操作规则,确定调控约束;Determine the underlying operation control logic and operating rules of the drone interference equipment, and determine regulatory constraints;

读取所述无人机干扰设备的运控自由度,确定调控范围;Read the degree of freedom of operation and control of the drone interference equipment and determine the control range;

基于所述调控约束与所述调控范围,针对所述运行扰动因素进行运控调整寻优,确定目标调控方案。Based on the control constraints and the control range, the operation control adjustment and optimization is performed according to the operation disturbance factors, and the target control plan is determined.

进一步的,运行调控模块17包括以下执行步骤:Further, the operation control module 17 includes the following execution steps:

基于所述调控约束与所述调控范围,搭建寻优空间;Based on the control constraints and the control range, build an optimization space;

在所述寻优空间中,以所述运行扰动因素为基准,进行随机扰动,确定多个运行调控方案;In the optimization space, random disturbance is performed based on the operation disturbance factors to determine multiple operation control plans;

以调控能耗与操作难度为约束,以所述扰动度为响应目标搭建适应度函数,对所述运行调控方案进行适应度计量,择取最大适应度映射的目标调控方案。With the regulation energy consumption and operation difficulty as constraints, a fitness function is built with the disturbance degree as the response target, the fitness of the operation regulation scheme is measured, and the target regulation scheme with the maximum fitness mapping is selected.

本说明书通过前述对无人机干扰设备的运行状态动态监测调节方法的详细描述,本领域技术人员可以清楚的知道本实施例中无人机干扰设备的运行状态动态监测调节方法,对于实施例公开的装置而言,由于其与实施例公开的方法相对应,所以描述的比较简单,相关之处参见方法部分说明即可。Through the foregoing detailed description of the dynamic monitoring and adjustment method of the operating status of the UAV interference equipment in this specification, those skilled in the art can clearly understand the dynamic monitoring and adjustment method of the operating status of the UAV interference equipment in this embodiment. Disclosure of the embodiments As for the device, since it corresponds to the method disclosed in the embodiment, the description is relatively simple. For relevant details, please refer to the description of the method part.

对所公开的实施例的上述说明,使本领域专业技术人员能够实现或使用本申请。对这些实施例的多种修改对本领域的专业技术人员来说将是显而易见的,本文中所定义的一般原理可以在不脱离本申请的精神或范围的情况下,在其它实施例中实现。因此,本申请将不会被限制于本文所示的这些实施例,而是要符合与本文所公开的原理和新颖特点相一致的最宽的范围。The above description of the disclosed embodiments enables those skilled in the art to implement or use the present application. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be practiced in other embodiments without departing from the spirit or scope of the application. Therefore, the present application is not to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.

Claims (7)

1.无人机干扰设备的运行状态动态监测调节方法,其特征在于,所述方法包括:1. A dynamic monitoring and adjustment method for the operating status of UAV interference equipment, characterized in that the method includes: 搭建基于无人机干扰设备的空间域,所述空间域基于设备射频范围进行配置;Build a space domain based on drone interference equipment, which is configured based on the radio frequency range of the equipment; 基于空间域的探测空间约束,结合探测运控模块,通过无人机干扰设备的无线电探测进行目标识别,生成识别响应,其中,所述探测运控模块用于控制无人机干扰设备进行无线电探测;Based on the detection space constraints in the spatial domain, combined with the detection operation and control module, target identification is performed through radio detection of UAV jamming equipment, and an identification response is generated. The detection operation and control module is used to control the UAV interference equipment to perform radio detection. ; 随着所述识别响应的接收,同步激活干扰运控模块,并配置基于干扰模式的干扰方案,其中,所述干扰模式包括迫降模式、返航模式与飞控干扰模式,所述干扰运控模块用于接收识别响应,并对当前干扰方式进行判断和干扰方案配置;With the reception of the identification response, the interference operation control module is activated synchronously and an interference scheme based on interference modes is configured. The interference modes include forced landing mode, return mode and flight control interference mode. The interference operation control module uses To receive the identification response, judge the current interference method and configure the interference plan; 对目标无人机进行追踪定位,结合空间域的干扰空间约束,基于所述干扰方案进行所述目标无人机的无线电反制,确定目标干扰实况;Track and locate the target UAV, combine the interference space constraints in the space domain, conduct radio countermeasures for the target UAV based on the interference plan, and determine the actual situation of target interference; 基于所述识别响应与所述目标干扰实况,提取回波反馈信号并进行运行状态评估,确定制动离轴度,所述制动离轴度为预期控制效果与实际控制效果之间的差值;Based on the recognition response and the target interference situation, the echo feedback signal is extracted and the operating status is evaluated to determine the braking off-axis degree, which is the difference between the expected control effect and the actual control effect. ; 若所述制动离轴度不满足阈值标准,针对所述制动离轴度进行溯源,确定标识有扰动度的运行扰动因素;If the braking off-axis degree does not meet the threshold standard, trace the source of the braking off-axis degree and determine the operating disturbance factors marked with the degree of disturbance; 其中,所述针对所述制动离轴度进行溯源,包括:Wherein, the tracing of the brake off-axis degree includes: 配置运控偏离溯源模组,所述运控偏离溯源模组包括抗干扰分析模块、运控偏差分析模块与环境场域干扰分析模块,其中,所述抗干扰分析模块、所述运控偏差分析模块与所述环境场域干扰分析模块分别用于分析无人机自身的抗干扰能力、无人机干扰设备自身的控制偏差和无人机干扰设备工作环境受到的磁场干扰;Configure an operation control deviation traceability module. The operation control deviation traceability module includes an anti-interference analysis module, an operation control deviation analysis module and an environmental field interference analysis module. The anti-interference analysis module, the operation control deviation analysis module The module and the environmental field interference analysis module are respectively used to analyze the anti-interference ability of the drone itself, the control deviation of the drone interference equipment itself, and the magnetic field interference in the working environment of the drone interference equipment; 将所述回波反馈信号传输至所述运控偏离溯源模组中,进行模块独立分析确定单项溯源结果,其中,所述单项溯源结果与各分析模块一一对应;The echo feedback signal is transmitted to the operation control deviation traceability module, and the module is independently analyzed to determine the single traceability result, where the single traceability result corresponds to each analysis module one-to-one; 对所述单项溯源结果进行同向拟合,确定所述运行扰动因素;Perform in-line fitting on the single traceability results to determine the operating disturbance factors; 基于所述运行扰动因素,对所述无人机干扰设备进行适应性运行调控。Based on the operation disturbance factors, adaptive operation control of the UAV interference equipment is performed. 2.如权利要求1所述的方法,其特征在于,所述搭建基于无人机干扰设备的空间域,包括:2. The method according to claim 1, characterized in that said building a space domain based on UAV interference equipment includes: 以无人机干扰设备的布设空间为基准,以设备布设位置为原点,确定空间轴向;Use the layout space of the UAV interference equipment as the benchmark and the equipment layout position as the origin to determine the spatial axis; 基于所述空间轴向搭建空间坐标系,对所述空间坐标系进行经纬度定位拟合,确定拟合坐标系;Build a spatial coordinate system based on the spatial axis, perform longitude and latitude positioning fitting on the spatial coordinate system, and determine the fitting coordinate system; 读取所述无人机干扰设备的探测范围与干扰范围,对所述拟合坐标系进行空间约束,生成空间域。Read the detection range and interference range of the UAV interference device, perform spatial constraints on the fitting coordinate system, and generate a spatial domain. 3.如权利要求1所述的方法,其特征在于,所述配置基于干扰模式的干扰方案,包括:3. The method of claim 1, wherein the configuring an interference scheme based on an interference mode includes: 配置干扰数据库,其中,所述干扰数据库包括存在一对多关系的表征为干扰模式-预干扰方案的多个序列;Configuring an interference database, wherein the interference database includes multiple sequences characterized by interference patterns-pre-interference schemes that have a one-to-many relationship; 以所述识别响应为约束,以干扰模式为需求,遍历所述干扰数据库进行匹配,确定所述干扰方案。With the identification response as a constraint and the interference pattern as a requirement, the interference database is traversed for matching to determine the interference plan. 4.如权利要求1所述的方法,其特征在于,所述抗干扰分析模块的配置包括:4. The method of claim 1, wherein the configuration of the anti-interference analysis module includes: 进行工业互联网检索,确定无人机干扰日志;Conduct an industrial Internet search to determine drone interference logs; 基于所述无人机干扰日志,提取映射的样本无线电射频信号、样本回波反馈信号与样本抗干扰数据;Based on the UAV interference log, extract the mapped sample radio frequency signal, sample echo feedback signal and sample anti-interference data; 基于所述样本无线电射频信号与所述样本回波反馈信号随机提取一项,作为决策数据并搭建第一决策层;Randomly extract one item based on the sample radio frequency signal and the sample echo feedback signal as decision-making data and build the first decision-making layer; 重复迭代,完成第N决策层的搭建,并进行所述第一决策层直至所述第N决策层的层级连接,基于所述样本抗干扰数据进行匹配标识,生成抗干扰决策树;Repeat the iteration to complete the construction of the Nth decision-making layer, and perform hierarchical connections from the first decision-making layer to the Nth decision-making layer, perform matching identification based on the sample anti-interference data, and generate an anti-interference decision tree; 基于所述抗干扰决策树,生成所述抗干扰分析模块。Based on the anti-interference decision tree, the anti-interference analysis module is generated. 5.如权利要求1所述的方法,其特征在于,所述基于所述运行扰动因素,对所述无人机干扰设备进行适应性运行调控,包括:5. The method of claim 1, wherein the adaptive operation control of the UAV interference equipment based on the operation disturbance factors includes: 确定所述无人机干扰设备的底层运控逻辑与操作规则,确定调控约束;Determine the underlying operation control logic and operating rules of the drone interference equipment, and determine regulatory constraints; 读取所述无人机干扰设备的运控自由度,确定调控范围;Read the degree of freedom of operation and control of the drone interference equipment and determine the control range; 基于所述调控约束与所述调控范围,针对所述运行扰动因素进行运控调整寻优,确定目标调控方案。Based on the control constraints and the control range, the operation control adjustment and optimization is performed according to the operation disturbance factors to determine the target control plan. 6.如权利要求5所述的方法,其特征在于,所述针对所述运行扰动因素进行运控调整寻优,包括:6. The method of claim 5, wherein the operation control adjustment and optimization for the operation disturbance factors includes: 基于所述调控约束与所述调控范围,搭建寻优空间;Based on the control constraints and the control range, build an optimization space; 在所述寻优空间中,以所述运行扰动因素为基准,进行随机扰动,确定多个运行调控方案;In the optimization space, random disturbance is performed based on the operation disturbance factors to determine multiple operation control plans; 以调控能耗与操作难度为约束,以所述扰动度为响应目标搭建适应度函数,对所述运行调控方案进行适应度计量,择取最大适应度映射的目标调控方案。With the regulation energy consumption and operation difficulty as constraints, a fitness function is built with the disturbance degree as the response target, the fitness of the operation regulation scheme is measured, and the target regulation scheme with the maximum fitness mapping is selected. 7.无人机干扰设备的运行状态动态监测调节系统,其特征在于,所述系统包括:7. Dynamic monitoring and adjustment system for the operating status of UAV interference equipment, characterized in that the system includes: 空间域搭建模块,用于搭建基于无人机干扰设备的空间域,所述空间域基于设备射频范围进行配置;The space domain construction module is used to build a space domain based on UAV interference equipment, and the space domain is configured based on the radio frequency range of the equipment; 识别响应模块,用于基于空间域的探测空间约束,结合探测运控模块,通过无人机干扰设备的无线电探测进行目标识别,生成识别响应,其中,所述探测运控模块用于控制无人机干扰设备进行无线电探测;The recognition response module is used to detect space constraints based on the space domain. Combined with the detection operation control module, it performs target recognition through radio detection of UAV jamming equipment and generates an identification response. The detection operation control module is used to control the unmanned aerial vehicle. jamming equipment for radio detection; 干扰方案模块,用于随着所述识别响应的接收,同步激活干扰运控模块,并配置基于干扰模式的干扰方案,其中,所述干扰模式包括迫降模式、返航模式与飞控干扰模式,所述干扰运控模块用于接收识别响应,并对当前干扰方式进行判断和干扰方案配置;The interference scheme module is used to activate the interference operation control module synchronously with the reception of the identification response, and configure the interference scheme based on the interference mode, wherein the interference mode includes the forced landing mode, the return mode and the flight control interference mode, so The interference operation control module is used to receive the identification response, judge the current interference mode and configure the interference plan; 追踪定位模块,用于对目标无人机进行追踪定位,结合空间域的干扰空间约束,基于所述干扰方案进行所述目标无人机的无线电反制,确定目标干扰实况;The tracking and positioning module is used to track and position the target UAV, combine the interference space constraints in the spatial domain, perform radio countermeasures for the target UAV based on the interference plan, and determine the actual situation of target interference; 状态评估模块,用于基于所述识别响应与所述目标干扰实况,提取回波反馈信号并进行运行状态评估,确定制动离轴度,所述制动离轴度为预期控制效果与实际控制效果之间的差值;A state evaluation module, configured to extract echo feedback signals and perform operating state evaluation based on the identification response and the target interference situation, and determine the braking off-axis degree, which is a combination of the expected control effect and the actual control The difference between effects; 扰动因素模块,用于若所述制动离轴度不满足阈值标准,针对所述制动离轴度进行溯源,确定标识有扰动度的运行扰动因素;A disturbance factor module, used to trace the source of the braking off-axis degree if the braking off-axis degree does not meet the threshold standard, and determine the operating disturbance factors with the disturbance degree marked; 其中,所述扰动因素模块包括以下执行步骤:Among them, the disturbance factor module includes the following execution steps: 配置运控偏离溯源模组,所述运控偏离溯源模组包括抗干扰分析模块、运控偏差分析模块与环境场域干扰分析模块,其中,所述抗干扰分析模块、所述运控偏差分析模块与所述环境场域干扰分析模块分别用于分析无人机自身的抗干扰能力、无人机干扰设备自身的控制偏差和无人机干扰设备工作环境受到的磁场干扰;Configure an operation control deviation traceability module. The operation control deviation traceability module includes an anti-interference analysis module, an operation control deviation analysis module and an environmental field interference analysis module. The anti-interference analysis module, the operation control deviation analysis module The module and the environmental field interference analysis module are respectively used to analyze the anti-interference ability of the drone itself, the control deviation of the drone interference equipment itself, and the magnetic field interference in the working environment of the drone interference equipment; 将所述回波反馈信号传输至所述运控偏离溯源模组中,进行模块独立分析确定单项溯源结果,其中,所述单项溯源结果与各分析模块一一对应;The echo feedback signal is transmitted to the operation control deviation traceability module, and the module is independently analyzed to determine the single traceability result, where the single traceability result corresponds to each analysis module one-to-one; 对所述单项溯源结果进行同向拟合,确定所述运行扰动因素;Perform in-line fitting on the single traceability results to determine the operating disturbance factors; 运行调控模块,用于基于所述运行扰动因素,对所述无人机干扰设备进行适应性运行调控。An operation control module is used to perform adaptive operation control of the UAV interference equipment based on the operation disturbance factors.
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