CN102914305A - Aircraft communication, positioning and navigation safety operation management auxiliary system for general aviation field - Google Patents

Aircraft communication, positioning and navigation safety operation management auxiliary system for general aviation field Download PDF

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Publication number
CN102914305A
CN102914305A CN2012104379592A CN201210437959A CN102914305A CN 102914305 A CN102914305 A CN 102914305A CN 2012104379592 A CN2012104379592 A CN 2012104379592A CN 201210437959 A CN201210437959 A CN 201210437959A CN 102914305 A CN102914305 A CN 102914305A
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China
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navigation
aircraft
module
interface
operation management
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CN2012104379592A
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Chinese (zh)
Inventor
李伟
王学智
赵新宇
王建伟
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哈尔滨盈盛翔科技开发有限公司
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Priority to CN2012104379592A priority Critical patent/CN102914305A/en
Publication of CN102914305A publication Critical patent/CN102914305A/en

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Abstract

The invention relates to an aircraft communication, positioning and navigation safety operation management auxiliary system for the general aviation field, belonging to the navigation equipment applied to the general aviation field. The auxiliary system comprises a central control unit (1) as well as a positioning module (3), an attitude measurement module (4) and an aircraft data input interface (5) which are connected with the data input end of the central control unit (1), and further comprises a display touch module (2) a communication interface (6) and a video-voice module (7) which are connected with the bidirectional data transmission end of the central control unit (1). The safety operation management auxiliary system disclosed by the invention is applicable to general aviation working aircrafts; and according to the safety operation management auxiliary system, the workload of pilots is reduced, the working performance of the aircrafts is enhanced, the safe flight guarantee is enhanced, a command center is enabled to know the information such as specific locations, courses, navigational speeds, heights of administered working aircrafts, and the difficulty, existing at present, that the location of general aviation working aircrafts cannot be known because of the wireless communication limitation is solved.

Description

用于通航领域的飞机通讯定位导航安全运行管理辅助系统 Aircraft communications positioning and navigation system for the safe operation and management assistance in the field of navigation

技术领域 FIELD

[0001] 用于通航领域的飞机通讯定位导航安全运行管理辅助系统属于应用在通用航空领域的导航设备。 [0001] aircraft navigation safety communications operation management support system for navigation is an application in the field of general aviation navigation equipment.

背景技术 Background technique

[0002] 经常驾驶航空作业飞机,会使驾驶员工作强度极大,而复杂的数据操作又增加了驾驶员的工作负荷,为了减轻驾驶员的工作负担,提高飞机作业效率,增强安全飞行保障,需要指挥中心能随时了解所辖作业飞机具体位置信息,航向航速,高度等信息,需要解决目前一直存在的由于无线电通信受限所导致的通航作业飞机位置无法掌握的难题。 [0002] aircraft aviation operations often driving, the driver will work great strength, and complex data manipulation and increase the workload of the driver in order to reduce pilot workload and improve the operational efficiency of aircraft, flight support enhanced security, command Center can readily understand the need to work under the jurisdiction of a specific aircraft position information, course speed, height and other information, there has been a need to address the current position of the aircraft due to the operation of the navigation radio communication is limited as a result of not grasp the problem.

发明内容[0003] 为了解决上述问题,本发明公开了用于通航领域的飞机通讯定位导航安全运行管理辅助系统,该系统适用于通用航空作业飞机,能减轻驾驶员工作负荷,提高飞机作业效率,增强安全飞行保障,使指挥中心能随时了解所辖作业飞机具体位置信息,航向航速,高度等信息,解决了目前一直存在的由于无线电通信受限所导致的通航作业飞机位置无法掌握的难题。 [0003] In order to solve the above problems, the present invention discloses a communications aircraft navigation system for safe operation and management assistance in the field of navigation, the system is suitable for general aviation aircraft operations, can reduce the driver's workload, improve operational efficiency of the aircraft, enhance flight safety guarantee, the command center can readily understand the operation of aircraft under the jurisdiction of a specific location, course speed, height and other information, there has been a solution to the current position of the navigation operations because the aircraft radio communication is limited as a result of not grasp the problem.

[0004] 本发明的目的是这样实现的: [0004] The object of the present invention is implemented as follows:

用于通航领域的飞机通讯定位导航安全运行管理辅助系统,包括中央控制器,连接中央处理器数据输入端的定位模块、姿态测量模块、飞机数据输入接口;连接中央处理器双向数据传输端的显示触控模块、通信接口以及视频语音模块。 Aircraft navigation communications operation management support system for safe navigation areas, including a central controller, the central processor connected to the data input terminal positioning module, the posture measuring module, aircraft data input interface; bidirectional data transmission terminal is connected to the central processor to display the touch module, video and voice communication interface module.

[0005] 上述用于通航领域的飞机通讯定位导航安全运行管理辅助系统,所述的显示触控模块包括显示屏和触摸屏,并且触摸屏配置在显示屏上表面;其中,显示屏为液晶显示屏。 [0005] The aircraft communication navigation operation management support system for the safe navigation of the art, the touch display module includes a display screen and a touch screen and a touch screen disposed on the display surface; wherein the display is a liquid crystal display.

[0006] 上述用于通航领域的飞机通讯定位导航安全运行管理辅助系统,所述的显示触控模块为4. 3寸、5寸、5. 3寸、7寸或8寸触摸屏,分辨率为800X480或960X540。 [0006] The aircraft communication navigation operation management support system for the safe navigation of the art, the touch display module is 4.3 inches, 5 inches, 5.3 inches, 7 inches or 8 inch touch screen, a resolution of 800X480 or 960X540.

[0007] 上述用于通航领域的飞机通讯定位导航安全运行管理辅助系统,所述的定位模块为北斗/GPS双模定位模块。 [0007] The aircraft communication navigation operation management support system for the safe navigation of the art, the positioning module Beidou / GPS dual-mode positioning module.

[0008] 上述用于通航领域的飞机通讯定位导航安全运行管理辅助系统,所述的姿态测量模块包括三轴加速度计、三轴陀螺仪以及三轴磁阻传感器。 [0008] The aircraft communication navigation operation management support system for the safe navigation of the art, the attitude measurement module comprises a three-axis accelerometer, a three-axis gyroscope and three axis magnetoresistive sensor.

[0009] 上述用于通航领域的飞机通讯定位导航安全运行管理辅助系统,所述的飞机数据输入接口与飞机上已有设备相配合,所述的飞机数据输入接口为USB接口、PS/2接口、SATA接口、1394 接口、RS-232 接口或RS-485 接口。 [0009] The aircraft communication navigation operation management support system for the safe navigation of the art, existing devices fitted on the aircraft data input interface with an aircraft, the aircraft data input interface is a USB interface, PS / 2 interfaces , SATA interface, a 1394 interface, RS-232 interface, or RS-485 interface.

[0010] 上述用于通航领域的飞机通讯定位导航安全运行管理辅助系统,所述的通信接口包括无线信号发射器和无线信号接收器。 [0010] The aircraft communication navigation operation management support system for the safe navigation of the art, the communication interface comprises a wireless signal transmitter and a wireless signal receiver.

[0011] 上述用于通航领域的飞机通讯定位导航安全运行管理辅助系统,所述的视频语音模块包括与显示触控模块共用的显示屏以及自用的扬声器。 [0011] The aircraft communication navigation operation management support system for the safe navigation of the art, the speech module comprises a video display and a speaker module common touch screen and personal use.

[0012] 由于本发明用于通航领域的飞机通讯定位导航安全运行管理辅助系统,包括中央控制器,以及与中央控制器连接的显示触控模块、定位模块、姿态测量模块、飞机数据输入接口、通信接口以及视频语音模块;这种设计使得该辅助导航设备适用于通用航空作业飞机,能减轻驾驶员工作负荷,提高飞机作业效率,增强安全飞行保障,使指挥中心能随时了解所辖作业飞机具体位置信息,航向航速,高度等信息,解决了目前一直存在的由于无线电通信受限所导致的通航作业飞机位置无法掌握的难题。 [0012] Since the present invention is safe for an aircraft communication navigation operation management support system in the field of navigation, including a central controller, and the touch display module is connected to the central controller, the positioning module, the posture measuring module, aircraft data input interface, video and voice communication interface module; this design allows the auxiliary navigation device for use in general aviation aircraft operations, can reduce pilot workload and improve operating efficiency of the aircraft, flight support enhanced security, the command center can readily understand the specific aircraft under the jurisdiction of the job location information, course speed, height and other information, there has been a solution to the current position of the navigation operations because the aircraft radio communication is limited as a result of not grasp the problem.

附图说明 BRIEF DESCRIPTION

[0013] 图I是本发明安全运行管理辅助系统电路连接示意图。 [0013] Figure I is a safety operation management support system according to the present invention is a circuit connection diagram.

[0014] 图中:1中央控制器、2显示触控模块、3定位模块、4姿态测量模块、41三轴加速度计、42三轴陀螺仪、43三轴磁阻传感器、5飞机数据输入接口、6通信接口、7视频语音模块。 [0014] FIG: a central controller, the touch display module 2, module 3 is positioned, attitude measurement module 4, three-axis accelerometer 41, 42 three-axis gyroscope, a three-axis magnetoresistive sensor 43, aircraft data input interface 5 , a communication interface 6, 7 video voice module.

具体实施方式[0015] 下面结合附图对本发明具体实施方式作进一步详细描述。 DETAILED DESCRIPTION [0015] The following drawings of specific embodiments of the present invention will be described in further detail in conjunction.

[0016] 本实施例的用于通航领域的飞机通讯定位导航安全运行管理辅助系统,该安全运行管理辅助系统的电路连接示意图如图I所示,该安全运行管理辅助系统包括中央控制器1,连接中央处理器I数据输入端的定位模块3、姿态测量模块4、飞机数据输入接口5 ;连接中央处理器I双向数据传输端的显示触控模块2、通信接口6以及视频语音模块7。 [0016] The airplane communication navigation operation management support system for the safe navigation of the art embodiments, the safety circuit operation management support system connection diagram shown in FIG. I, the safety operation management support system includes a central controller 1, a central processor connected to the data input terminal I 3 of the positioning module, attitude measurement module 4, the data input interface plane 5; I connect the central processor bidirectional data transmission terminal module touch display panel 2, video and voice communication interface module 6 7.

[0017] 所述的显示触控模块2包括显示屏和触摸屏,并且触摸屏配置在显示屏上表面;其中,显示触控模块2优选为8寸分辨率为800X480的显示触控屏,还可以选择其它尺寸,如4. 3寸、5寸、5. 3寸、7寸或8寸,以及其它分辨率,如960X540。 [0017] The display module 2 includes a touch screen and a touch screen and a touch screen disposed on the display surface; wherein the touch display module 2 is preferably 8-inch display with a resolution of 800X480 touch screen, may choose other sizes, such as 4.3 inches, 5 inches, 5.3 inches, 7 inches or 8 inches, and other resolutions, such as 960X540.

[0018] 所述的定位模块3优选为北斗/GPS双模定位模块,还可以选择北斗一号定位模块。 [0018] The positioning module 3 is preferably Compass / GPS dual-mode positioning module, you can also choose Beidou positioning module.

[0019] 所述的姿态测量模块4包括三轴加速度计41、三轴陀螺仪42以及三轴磁阻传感器43。 [0019] The posture measurement module 4 comprises a three-axis accelerometer 41, a three-axis gyroscope 42 and a three-axis magnetoresistive sensor 43. 且三轴加速度计41的数量不少于两个,三轴陀螺仪42的数量不少于两个,三轴磁阻传感器43的数量不少于两个,在附图I中仅画出了其中一个。 And the number of three-axis accelerometer 41 is not less than two, the number of three-axis gyroscope 42 is not less than two, the number of three-axis magnetoresistive sensor 43 is not less than two, in the drawings shown only I One of the.

[0020] 所述的飞机数据输入接口5与飞机上已有设备相配合,所述的飞机数据输入接口5优选为USB接口;该接口还可以选择为PS/2接口、SATA接口、1394接口、RS-232接口或RS-485 接口。 Aircraft data input interface 5 cooperate with the aircraft existing equipment [0020] according to the aircraft data input interface 5 preferably is a USB interface; The interface can also be selected as a PS / 2 interface, SATA interface, a 1394 interface, RS-232 interface, or RS-485 interface.

[0021] 所述的通信接口6包括无线信号发射器和无线信号接收器。 [0021] The communication interface 6 comprises a wireless signal transmitter and a wireless signal receiver.

[0022] 所述的视频语音模块7包括与显示触控模块2共用的显示屏以及自用的扬声器。 [0022] The video sound module 7 comprising a speaker module 2 and the display of the touch screen and personal use in common.

[0023] 将本发明安全运行管理辅助系统应用于通用航空领域,能减轻驾驶员工作负荷,提高飞机作业效率,增强安全飞行保障,使指挥中心能随时了解所辖作业飞机具体位置信息,航向航速,高度等信息,解决了目前一直存在的由于无线电通信受限所导致的通航作业飞机位置无法掌握的难题。 [0023] The security operation management support system according to the present invention is applied to general aviation, the driver can reduce workload and improve operating efficiency of the aircraft, flight support enhanced security, the command center can readily understand the operation of aircraft under the jurisdiction of the specific location information, speed course , height and other information, there has been a solution to the current position of the navigation operations because the aircraft radio communication is limited as a result of not grasp the problem.

Claims (8)

1.用于通航领域的飞机通讯定位导航安全运行管理辅助系统,其特征在于包括中央控制器(1),连接中央处理器(I)数据输入端的定位模块(3)、姿态测量模块(4)、飞机数据输入接口( 5 );连接中央处理器(I)双向数据传输端的显示触控模块(2 )、通信接口( 6 )以及视频语音模块(7)。 1. Aircraft navigation communications operation management support system for safe navigation field, characterized by comprising a central controller (1) connected (I) of the data input terminal positioning module central processor (3), attitude measurement module (4) , aircraft data input interface (5); bidirectional data transmission terminal is connected to a central processing unit (I) of the touch display module (2), a communication interface (6) and a video sound module (7).
2.根据权利要求I所述的用于通航领域的飞机通讯定位导航安全运行管理辅助系统,其特征在于所述的显示触控模块(2)包括显示屏和触摸屏,并且触摸屏配置在显示屏上表面;其中,显示屏为液晶显示屏。 The aircraft communication navigation operation management support system for the safe navigation of the art according to claim I, wherein the touch display module (2) comprises a display and a touch screen and a touch screen disposed on a display screen surface; wherein the display is a liquid crystal display.
3.根据权利要求2所述的用于通航领域的飞机通讯定位导航安全运行管理辅助系统,其特征在于所述的显示触控模块为4. 3寸、5寸、5. 3寸、7寸或8寸触摸屏,分辨率为800X480 或960X540。 The safe operation of the aircraft communication navigation system for navigation assistance management field according to claim 2, wherein the touch display module is 4.3 inches, 5 inches, 5.3 inches, 7 inches or 8-inch touch screen with a resolution of 800X480 or 960X540.
4.根据权利要求I所述的用于通航领域的飞机通讯定位导航安全运行管理辅助系统,其特征在于所述的定位模块(3)为北斗/GPS双模定位模块。 The safe operation of the aircraft communication navigation system for navigation assistance management field according to claim I, wherein the positioning module (3) of Compass / GPS dual-mode positioning module.
5.根据权利要求I所述的用于通航领域的飞机通讯定位导航安全运行管理辅助系统,其特征在于所述的姿态测量模块(4 )包括三轴加速度计(41)、三轴陀螺仪(42 )以及三轴磁阻传感器(43)。 The safe operation of the aircraft communication navigation system for navigation assistance management field according to claim I, wherein said posture measuring module (4) comprises a three-axis accelerometer (41), a three-axis gyroscope ( 42) and a three-axis magnetoresistive sensor (43).
6.根据权利要求I所述的用于通航领域的飞机通讯定位导航安全运行管理辅助系统,其特征在于所述的飞机数据输入接口(5)与飞机上已有设备相配合,所述的飞机数据输入接口(5)为USB 接口、PS/2 接口、SATA 接口、1394 接口、RS-232 接口或RS-485 接口。 The aircraft communication navigation operation management support system for the safe navigation of the art according to claim I, wherein said data input interface airplane aircraft existing apparatus cooperating upper (5) of the aircraft, according to a data input interface (5) is a USB port, PS / 2 interfaces, SATA interface, a 1394 interface, RS-232 interface, or RS-485 interface.
7.根据权利要求I所述的用于通航领域的飞机通讯定位导航安全运行管理辅助系统,其特征在于所述的通信接口(6)包括无线信号发射器和无线信号接收器。 The safe operation of the aircraft communication navigation system for navigation assistance management field according to claim I, wherein said communication interface (6) comprises a wireless signal transmitter and a wireless signal receiver.
8.根据权利要求I所述的用于通航领域的飞机通讯定位导航安全运行管理辅助系统,其特征在于所述的视频语音模块(7 )包括与显示触控模块(2 )共用的显示屏以及自用的扬声器。 The aircraft communication navigation operation management support system for the safe navigation of the art according to claim I, wherein said video voice module (7) comprises a common touch with the display module (2) and a display screen own speakers.
CN2012104379592A 2012-11-06 2012-11-06 Aircraft communication, positioning and navigation safety operation management auxiliary system for general aviation field CN102914305A (en)

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Publication number Priority date Publication date Assignee Title
CN106530103A (en) * 2016-10-11 2017-03-22 北京农业智能装备技术研究中心 Aviation plant protection operation real-time supervision system

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