CN1262846C - Track Data Fusion Processing Method - Google Patents
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Abstract
本发明是一种航迹资料融合处理方法,应用在联合雷达/自动回报装置监视环境中;本发明在融合航迹位置信号时定义了航迹状态、航迹类别及航迹类别转换的规则;本发明可以协助航管系统在联合雷达/自动回报装置监视环境中做航迹追踪,并针对不同机载设备的航迹提供最大的飞航服务。
The present invention is a track data fusion processing method, which is applied in a joint radar/automatic reporting device monitoring environment; the present invention defines the track status, track category and track category conversion rules when fusing track position signals; the present invention can assist the air traffic control system in tracking tracks in a joint radar/automatic reporting device monitoring environment, and provide the best flight service for the tracks of different airborne equipment.
Description
技术领域technical field
本发明属飞航管理技术领域,尤指在联合雷达/自动回报监视环境中,一种航迹资料融合处理方法。The invention belongs to the technical field of flight management, in particular to a flight track data fusion processing method in a combined radar/automatic return monitoring environment.
背景技术Background technique
由于航空交通量成长快速(约每年成长10%),目前的飞航管理系统无法做有效率的交通管理。为了解决伴随而来的问题例如:运作成本提高、飞机抵达时间延迟,国际民航组织(ICAO)组成FANS委员会针对此情况提出改善方案。FANS在1991年针对通讯(COMMUNICATION)、导航(NAVIGATION)及监视(SURVEILLANCE)提出了新的技术以用于未来2010年的飞航管理系统。在监视部分,FANS提出了定址自动回报装置(ADS-A)、广播自动回报装置(ADS-B),用来辅助目前的雷达监视设备。Due to the rapid growth of air traffic volume (about 10% per year), the current flight management system cannot manage traffic efficiently. In order to solve the accompanying problems such as increased operating costs and delays in aircraft arrival time, the International Civil Aviation Organization (ICAO) formed the FANS Committee to propose an improvement plan for this situation. In 1991, FANS proposed new technologies for communication (COMMUNICATION), navigation (NAVIGATION) and surveillance (SURVEILLANCE) to be used in the future flight management system in 2010. In the monitoring part, FANS proposed the addressing automatic reporting device (ADS-A) and the broadcasting automatic reporting device (ADS-B), which are used to assist the current radar monitoring equipment.
在未来同时使用雷达、定址自动回报和广播自动回报的监视环境下,目前只使用雷达做航迹追踪的航管系统必须做适度的修改,以便能在未来新的监视环境下,融合多重信号做航迹追踪。本发明便是要满足这样的需求。In the future surveillance environment where radar, addressing automatic reporting and broadcasting automatic reporting are used simultaneously, the current air traffic control system that only uses radar for track tracking must be modified appropriately so that it can integrate multiple signals in the new surveillance environment in the future. track tracking. The present invention is to meet such needs.
发明内容Contents of the invention
本发明的目的在于提供一种航迹资料融合处理方法,利用资料融合,本发明可在复杂监视环境中使用多重信号做航迹追踪。The purpose of the present invention is to provide a track data fusion processing method. By using data fusion, the present invention can use multiple signals for track tracking in a complex monitoring environment.
本发明的方法包括:一种航迹资料融合处理方法,应用在联合雷达和自动回报装置的监视环境,其特征在于,该方法包括:The method of the present invention comprises: a kind of track data fusion processing method, is applied in the monitoring environment of joint radar and automatic reporting device, it is characterized in that, this method comprises:
航迹状态定义,是定义可能的航迹状态为航迹初始状态、航迹建立状态、航迹追踪状态、航迹失踪状态、航迹结束状态,其中,当航迹状态为航迹初始状态时,航管系统根据不同回报设备各自的回报频率来初始化不同类别的航迹;当航迹状态为航迹追踪状态时,航管系统会对监视环境内的所有飞机的位置及速度做预测,以便显示相对应的航迹,并据此做危险预警;当航迹状态为航迹失踪状态时,航管系统会根据既有的信息计算航迹可能的位置及速度以便显示相对应的航迹,并据此做危险预警处理;当航迹状态为航迹结束状态时,航管系统不会再对此航迹做追踪,但记录航迹的相关信息;The definition of the track state is to define the possible track states as track initial state, track establishment state, track tracking state, track missing state, and track end state, among them, when the track state is the track initial state , the air traffic management system initializes different types of tracks according to the respective reporting frequencies of different reporting devices; when the track state is the track tracking state, the air traffic management system will predict the positions and speeds of all aircraft in the monitoring environment, so that Display the corresponding track, and make danger warning accordingly; when the track status is track missing, the air traffic control system will calculate the possible position and speed of the track based on the existing information in order to display the corresponding track, And do danger warning processing accordingly; when the track status is the track end state, the air traffic control system will no longer track the track, but record the relevant information of the track;
航迹类别定义,是定义可能的航迹类别为搜寻、电码、精确、ADS精确、ADS电码、ADS搜寻、及ADS,其中,航管系统对于一飞机只接到主雷达信号,且未关联到航管系统中的任何一个航迹时,初始航迹类别为搜寻;当航管系统对于一飞机只接到二次雷达信号,且未关联到航管系统中的任何一个航迹时,初始航迹类别为电码;当航管系统对于一飞机只接到广播自动回报信号,且未关联到航管系统中的任何一个航迹时,初始航迹类别为精确;当航管系统允许飞机登入ADS-A服务时,初始航迹类别为ADS;当航管系统收到主雷达的位置回报信号及定址自动回报信号,航迹类别为ADS搜寻;当航管系统同时收到二次雷达的位置回报信号及定址自动回报信号,航迹类别为ADS电码;当航管系统收到定址自动回报及广播自动回报信号,则航迹类别为ADS精确;以及The track category definition is to define possible track categories as search, code, precision, ADS precision, ADS code, ADS search, and ADS, where the air traffic management system only receives the main radar signal for an aircraft and is not associated with When the air traffic management system receives any track in the air traffic management system, the initial track type is search; The track type is code; when the air traffic management system only receives the broadcast automatic report signal for an aircraft and is not associated with any track in the air traffic management system, the initial track type is precise; when the air traffic management system allows the aircraft to log in to ADS In -A service, the initial track type is ADS; when the air traffic management system receives the position return signal from the primary radar and the automatic addressing return signal, the track type is ADS search; when the air traffic control system receives the position report from the secondary radar at the same time Signal and addressing automatic return signal, track type is ADS code; when the air traffic control system receives addressing automatic return signal and broadcast automatic return signal, the track type is ADS precise; and
航迹类别转换规则定义,是定义航迹类别转换的条件,其中,The track category conversion rule definition is to define the conditions for track category conversion, where,
当航迹类别初始为搜寻或电码时,进入建立状态的条件为连续3次收到位置回报;When the track type is initially search or code, the condition for entering the establishment state is to receive position reports for 3 consecutive times;
当航迹类别初始为精确时,进入建立状态的条件是直接建立;When the track category is initially precise, the condition for entering the establishment state is direct establishment;
当航迹类别初始为ADS时,进入建立状态的条件为收到第一笔ADS-A信息;When the track type is initially ADS, the condition for entering the establishment state is to receive the first ADS-A message;
当航迹类别为搜寻或电码时,进入失踪状态的条件为连续三个批次时间航迹未关联到任何目标物回报,进入结束状态的条件为连续八个批次时间航迹未关联到任何目标物回报或管制员直接移除该航迹,其中,一个批次时间为一段由航管系统所预先设定的固定时间;When the track type is search or code, the condition for entering the missing state is that three consecutive batches of time tracks are not associated with any target report, and the condition for entering the end state is that eight consecutive batches of time tracks are not associated with any The target reports or the controller directly removes the track, where a batch time is a fixed time preset by the air traffic control system;
当航迹类别为ADS时,进入失踪状态的条件为连续两次未在预定时间收到位置回报,进入结束状态的条件为登出ADS-A服务、航迹交管给其他中心或管制员直接移除该航迹;When the track type is ADS, the condition of entering the missing state is that the location report is not received twice in a row at the scheduled time, and the condition of entering the end state is that the ADS-A service is logged out, the track is handed over to other centers or the controller directly transfers remove the track;
当航迹类别为ADS搜寻、ADS电码、ADS精确时,管制员可直接输入指令删除该航迹;When the track type is ADS Search, ADS Code, or ADS Accurate, the controller can directly input commands to delete the track;
当航迹类别为搜寻时,航迹类别在管制员手动输入指令之下,转换为电码或ADS搜寻;When the track type is search, the track type is converted to code or ADS search under the manual input command of the controller;
当航迹类别为电码时:(1)于管制员手动输入指令的条件下,航迹类别可转换为搜寻;(2)在该航迹关联到广播自动回报的目标物的条件下,航迹类别转换为精确;(3)于飞机登入ADS-A服务,且飞机编号相符的条件下,航迹类别转换为ADS电码;When the track type is code: (1) under the condition that the controller manually inputs the command, the track type can be converted into search; (2) under the condition that the track is related to the target object automatically reported by the broadcast, the track type The category is converted to precise; (3) under the condition that the aircraft logs into the ADS-A service and the aircraft number matches, the track category is converted into an ADS code;
当航迹类别为精确时:(1)在该航迹未关联到广播自动回报的目标物,只关联到二次雷达回报的目标物的条件下,航迹类别转换为电码;(2)于飞机登入ADS-A服务,且飞机编号相符的条件下,航迹类别转换为ADS精确;When the track category is accurate: (1) under the condition that the track is not associated with the target object reported automatically by broadcasting, but only with the target object reported by the secondary radar, the track category is converted into code; (2) at If the aircraft is logged into the ADS-A service and the aircraft number matches, the track type will be converted to ADS-accurate;
当航迹类别为ADS时:(1)在该航迹关联到主雷达回报的目标物的条件下,航迹类别转换为ADS搜寻;(2)在该航迹关联到二次雷达回报的目标物的条件下,航迹类别转换为ADS电码;(3)在该航迹关联到广播自动回报的目标物,且飞机编号相符的条件下,航迹类别转换为ADS精确;When the track type is ADS: (1) under the condition that the track is associated with the target reported by the primary radar, the track type is converted to ADS search; (2) the track is associated with the target reported by the secondary radar (3) Under the condition that the track is associated with the broadcast automatic report target and the aircraft number matches, the track type is converted to ADS precision;
当航迹类别为ADS搜寻时:(1)于飞机登出ADS-A服务时,航迹类别转换为搜寻;(2)在该航迹连续一段时间未关联到主雷达目标物回报的条件下,航迹类别转换为ADS;(3)在该航迹关联到二次雷达回报的目标物的条件下,航迹类别转换为ADS电码;(4)在该航迹关联到广播自动回报的目标物,且飞机编号相符的条件下,航迹类别转换为ADS精确;When the track type is ADS search: (1) when the aircraft logs out of the ADS-A service, the track type is converted to search; (2) under the condition that the track is not associated with the main radar target report for a continuous period of time , the track type is converted to ADS; (3) under the condition that the track is associated with the target object reported by the secondary radar, the track type is converted into an ADS code; (4) the track is associated with the broadcast automatic report target Objects, and under the condition that the aircraft numbers match, the track category is converted to ADS accurately;
当航迹类别为ADS电码时:(1)于飞机登出ADS-A服务的条件下,航迹类别转换为电码;(2)在该航迹连续一段时间未关联到二次雷达回报的目标物的条件下,航迹类别转换为ADS;(3)在该航迹关联到广播自动回报的目标物的条件下,航迹类别转换为ADS精确;When the track type is ADS code: (1) Under the condition that the aircraft logs out of the ADS-A service, the track type is converted into a code; (2) the track is not associated with the target reported by the secondary radar for a continuous period of time (3) Under the condition that the track is associated with the broadcast automatic report target, the track category is converted to ADS precision;
当航迹类别为ADS精确时:(1)于飞机登出ADS-A服务的条件下,航迹类别转换为精确;(2)于连续一段时间未关联到广播自动回报的目标物的条件下,航迹类别转换为ADS;(3)在该航迹关联到二次雷达回报的目标物,且无关联到广播自动回报的目标物的条件下,航迹类别转换为ADS电码。When the track category is ADS precise: (1) under the condition that the aircraft logs out of the ADS-A service, the track category is converted to precise; (2) under the condition that there is no target object that broadcasts automatic reporting for a continuous period of time , the track category is converted to ADS; (3) under the condition that the track is related to the target object reported by the secondary radar and not related to the target object reported automatically by the broadcast, the track category is converted to ADS code.
附图说明Description of drawings
为进一步说明本发明的结构特征,以下结合附图对本发明作进一步的详细描述,其中:For further illustrating structural feature of the present invention, below in conjunction with accompanying drawing, the present invention is described in further detail, wherein:
图1是本发明的系统环境示意图。FIG. 1 is a schematic diagram of the system environment of the present invention.
具体实施方式Detailed ways
有关本发明的联合雷达/自动回报监视环境请参照图1。其中,在地面有:主雷达站11:可将航迹位置信号传送到航管中心10;Please refer to FIG. 1 for the combined radar/automatic return surveillance environment of the present invention. Among them, there are on the ground: the main radar station 11: can transmit the track position signal to the air
次雷达站12:除可接收航迹位置及高度信号,另可接收航迹收发器所发出的航迹电码,并将信号传送到航管中心10;注意,主雷达和次雷达通常会架设在一起;Secondary radar station 12: In addition to receiving track position and altitude signals, it can also receive track codes sent by track transceivers, and transmit the signals to the
航管中心10:整合多重信号做航迹追踪及飞航服务;Air Traffic Management Center 10: Integrate multiple signals for track tracking and flight services;
广播自动回报信号接收站13:可接收航迹广播的位置、高度、航迹编号等信息,并传送信号回航管中心10;Broadcast automatic return signal receiving station 13: can receive information such as the position, altitude, and track number of the track broadcast, and send the signal back to the
卫星信号接收站14:接收航迹20利用通讯卫星30传来的定址自动回报信号。Satellite signal receiving station 14: receiving track 20 utilizes the addressing automatic return signal transmitted by
在此联合监视环境中,航迹20依其等级可能配有下述不同的设备:In this joint surveillance environment, track 20 may have the following equipment depending on its class:
电码收发器21:传送航迹的电码;Code transceiver 21: transmit the code of the track;
定址自动回报设备22:由导航卫星40定出航迹位置,在向航管中心10登入ADS-A服务之后,航迹20透过卫星30传送定址自动回报信号给航管中心10;Addressing and automatic reporting equipment 22: the track position is determined by the
广播自动回报设备23:藉由导航卫星定出航迹位置,广播航迹的位置、高度、航迹编号等信息。Broadcast automatic reporting device 23: determine the location of the track by means of navigation satellites, and broadcast information such as the position, altitude, and track number of the track.
于上述的联合雷达/自动回报监视环境架构中,本发明在航迹资料融合处理时,定义了航迹状态、航迹类别及航迹类别转换的规则,以针对不同机载设备的航迹提供最大的飞航服务,如表一所示。In the above-mentioned joint radar/automatic report monitoring environment framework, the present invention defines the rules of track state, track category and track category conversion during track data fusion processing, so as to provide track information for different airborne equipment. The largest airline services are shown in Table 1.
表一:不同机载设备航迹所得的飞航服务
本发明所定义的航迹状态如下:The track state defined by the present invention is as follows:
1.航迹初始:当系统接收到的航迹位置回报并未关联到系统中任何一个航迹时,此时系统认为有新的目标物出现,因此会初始化一个新的航迹,以对此目标物做追踪。因为不同回报设备的回报频率不同,因此系统会根据不同的回报设备初始化不同类别的航迹。1. Track initialization: When the track position report received by the system is not associated with any track in the system, the system thinks that there is a new target at this time, so it will initialize a new track for this purpose. The target is tracked. Because the reporting frequency of different reporting devices is different, the system will initialize different types of tracks according to different reporting devices.
2.航迹建立:在经过几次航迹位置资料更新之后,系统确认这不是偶发的杂讯,因此会建立航迹,对此航迹做追踪。2. Track establishment: After several track position data updates, the system confirms that this is not an occasional noise, so it will create a track and track it.
3.航迹追踪:系统定期由监视设备接收航迹位置回报,并更新航迹位置。此外,系统会对所有航迹的位置及速度做预测,以便航管系统显示航迹,并且做危险预警或飞航资料处理等等。3. Track tracking: The system regularly receives the track position report from the monitoring equipment and updates the track position. In addition, the system will predict the position and speed of all tracks, so that the air traffic management system can display the tracks, and do danger warning or flight data processing, etc.
4.航迹失踪:若某一航迹有一段时间未关联到任何的位置回报,此航迹会进入失踪状态。此时,系统会根据既有的信息计算航迹可能的位置及速度以便航管系统显示航迹,并且做危险预警处理。4. Missing track: If a track has not been associated with any position report for a period of time, the track will enter the missing state. At this time, the system will calculate the possible position and speed of the track based on the existing information so that the air traffic control system can display the track and perform risk warning processing.
5.航迹结束:当航迹在失踪状态且持续一段时间系统仍未收到任何的位置回报,此航迹会进入结束状态。系统不再对此航迹做追踪,但航迹的一些相关信息会被纪录下来。5. Track end: When the track is in the missing state and the system has not received any position report for a period of time, the track will enter the end state. The system will no longer track this track, but some relevant information of the track will be recorded.
表二和表三显示了不同类别航迹进入初始、建立、失踪、结束状态的条件。Tables 2 and 3 show the conditions for different types of tracks to enter the initial, establishment, missing, and end states.
表二:不同航迹其初始及建立的条件
表三:不同航迹进入失踪及结束状态的条件
其中,表二及表三的航迹类别与机载回报装置有关。在联合雷达/自动回报装置监视环境中,可能的航迹位置回报装置有:主雷达、二次雷达、定址自动回报装置、广播自动回报装置。若航管系统对于同一架飞机只接到一种信号来源,例如:主雷达信号源,则将初始的新航迹类别为“搜寻”;同理,若信号源为二次雷达、广播自动回报或定址自动回报,则初始的航迹类别依次为“电码”、“精确”及“ADS”。除了上述基本的航迹类别(“搜寻”、“电码”、“精确”及“ADS”)之外,本发明同时定义了“ADS搜寻”、“ADS电码”和“ADS精确”类别。当航迹类别为“ADS”且同时收到主雷达对该航迹位置回报的信号,此时航迹类别会由“ADS”变为“ADS搜寻”;同理,若同时收到的是次雷达信号或广播自动回报信号则航迹会由“ADS”变为“ADS电码”或“ADS精确”。不同航迹类别彼此间转换的条件详列在表四。在本发明中,航迹类别转换的原则是:当一架飞机同时有两种或两种以上的位置信号回报时,本发明所定义的航迹类别变化必须协助系统有效运用所有位置回报信号,以便任何时候都能使用目前最好的信号来追踪航迹。Among them, the track types in Table 2 and Table 3 are related to the airborne reporting device. In the joint radar/automatic reporting device surveillance environment, possible track position reporting devices include: primary radar, secondary radar, addressing automatic reporting device, and broadcast automatic reporting device. If the air traffic management system only receives one signal source for the same aircraft, for example: the main radar signal source, the initial new track type is "search"; similarly, if the signal source is secondary radar, broadcast automatic report or Addressing automatic reporting, the initial track category is "code", "accurate" and "ADS". In addition to the basic track categories described above ("Search", "Code", "Precise" and "ADS"), the present invention also defines the categories "ADS Search", "ADS Code" and "ADS Precise". When the track type is "ADS" and the signal reported by the main radar on the track position is received at the same time, the track type will change from "ADS" to "ADS search" at this time; The track will change from "ADS" to "ADS Code" or "ADS Accurate" if the radar signal or broadcast automatic return signal. The conditions for switching between different track categories are listed in Table 4. In the present invention, the principle of track type conversion is: when an aircraft has two or more position signal reports at the same time, the change of track type defined in the present invention must assist the system to effectively use all position return signals, So that the best available signal can be used to track the track at any time.
表四:航迹类别转换条件
以前述本发明的方法,假设目前有一航迹20同时配备“电码收发器”21及“自动定址回报设备”22,并在图1的监视环境中飞行。当航迹20向航管中心10登入ADS-A服务时,本发明的方法会为航管系统初始一个“ADS”类别的航迹。当航迹20不断用定址自动回报设备22透过卫星30传送航迹位置、高度、航迹编号等信息时,航管中心10会透过卫星信号地面接收站13接收这些信息,并且利用这些信息建立及追踪此“ADS”航迹,并提供航迹20适当的飞航服务。当航迹20飞入次雷达12的涵盖范围时,航迹20的电码收发器21会收到次雷达12的电码询问信号,此时收发器21会发出飞机的电码,当次雷达12接收到电码时,它会将航迹20的电码、位置、高度等信息传至航管中心10,此时航管中心会改变此“ADS”航迹类别为“ADS电码”,并且同时使用次雷达12及定址自动回报信号来追踪航迹。With the aforementioned method of the present invention, it is assumed that a flight track 20 is equipped with "code transceiver" 21 and "automatic addressing return device" 22 at the same time, and is flying in the monitoring environment of FIG. 1 . When the track 20 registers the ADS-A service to the air
当飞行一段时间之后,可能因为气候因素或机载的电码收发器21故障,造成地面端的次雷达12无法收到电码,若此状况持续一段时间,此时航迹类别会由“ADS电码”变为“ADS”,本发明改以定址自动回报来追踪航迹(因为收不到次雷达的信号)。若再经过一段时间,主雷达11发现此航迹,并将位置信号传回航管中心10,此时航迹类别会由“ADS”变成“ADS搜寻”,代表系统目前同时使用主雷违11及定址自动回报来追踪航迹。After flying for a period of time, the sub-radar 12 on the ground may not be able to receive the code due to weather factors or the failure of the
当飞机再飞行一段时间之后,飞行员可能向航管中心10要求登出ADS-A服务。在登出ADS-A服务之后,系统会只收到主雷达11的位置信号回报,因此航迹类别将由“ADS搜寻”变成“搜寻”,同时系统改以主雷达11追踪航迹。当航迹20飞行一段时间之后,飞机可能飞出主雷达11的涵盖范围,因此系统会有一段时间收不到航迹20的主雷达位置信号回报,此时这航迹会由追踪状态变为失踪状态,当再经过一段时间仍未收到主雷达11的位置信号回报,此时系统会将航迹由失踪状态改成结束状态并删掉此航迹,停止追踪此航迹。After the aircraft has been flying for a period of time, the pilot may request the air
上例说明了本发明可以协助系统随时使用目前可用的追踪信号来追踪航迹20。而由于不同监视设备其回报频率大不相同,例如:广播自动回报可达到一秒钟一次,定址自动回报5到15分钟一次,本发明同时考虑了这些特性,协助系统使用最高的回报率来追踪航迹,使航迹得到最佳的飞航服务。The above example illustrates that the present invention can assist the system to track the track 20 at any time using currently available tracking signals. And because the reporting frequency of different monitoring devices is quite different, for example: the automatic reporting of broadcasting can reach once a second, and the automatic reporting of addressing can be done once every 5 to 15 minutes. track, so that the track can get the best flight service.
综上所述,本发明无论就目的、手段及功效,均不同于现有技术的特征,实为一极具实用价值的发明。惟应注意的是,上述诸多实施例仅是为了便于说明而举例而已,本发明所主张的权利范围自应以申请专利范围所述为准,而非仅限于上述实施例。To sum up, the present invention is different from the features of the prior art in terms of purpose, means and efficacy, and is actually an invention of great practical value. However, it should be noted that the above-mentioned embodiments are examples for convenience of description only, and the scope of rights claimed by the present invention should be determined by the scope of the patent application, rather than limited to the above-mentioned embodiments.
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CN101571591B (en) * | 2009-06-01 | 2012-11-07 | 民航数据通信有限责任公司 | Fitting analyzing method based on radar track |
CN102881188B (en) * | 2012-10-18 | 2014-12-17 | 四川九洲空管科技有限责任公司 | Method for establishing track of broadcast automatic related monitoring target |
CN103413463B (en) * | 2013-08-07 | 2015-08-26 | 四川九洲空管科技有限责任公司 | The data of a kind of ADS-B target and radar target hold fusion implementation method |
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CN104933900A (en) * | 2015-06-26 | 2015-09-23 | 中国人民解放军63898部队 | Display control method and system for secondary radar command post system |
CN106205219B (en) * | 2016-08-31 | 2019-03-05 | 北京招通致晟科技有限公司 | Aircraft monitoring method and device based on fusion of multiple radar information |
CN114783211B (en) * | 2022-03-22 | 2023-09-15 | 南京莱斯信息技术股份有限公司 | Scene target monitoring enhancement system and method based on video data fusion |
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