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 PDFInfo
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- 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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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
Technical field
The Wing Newsletter location navigation safe operation management backup system that is used for the navigation field belongs to the navigator that is applied in the General Aviation field.
Background technology
Often drive aviation operation aircraft, can make driver's working strength very big, and complicated data manipulation has increased driver's working load, in order to alleviate driver's work load, improve aircraft operation efficient, strengthen the safe flight guarantee, need command centre can understand at any time jurisdiction operation aircraft more specific location information, coursespeed, the information such as height need that solution exists at present always because the difficult problem that the limited navigation operation aircraft position that causes of wireless communication can't be grasped.
Summary of the invention
In order to address the above problem, the invention discloses the Wing Newsletter location navigation safe operation management backup system for the navigation field, this system is applicable to General Aviation operation aircraft, can alleviate driver workload, improve aircraft operation efficient, strengthen the safe flight guarantee, make command centre can understand at any time jurisdiction operation aircraft more specific location information, coursespeed, the information such as height, solved exist at present always because the difficult problem that the wireless communication limited navigation operation aircraft position that causes can't be grasped.
The object of the present invention is achieved like this:
Be used for the Wing Newsletter location navigation safe operation management backup system in navigation field, comprise central controller, connect locating module, attitude measurement module, the airplane data input interface of central processing unit data input pin; The demonstration touch-control module, communication interface and the video voice module that connect central processing unit bidirectional data transfers end.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described demonstration touch-control module comprises display screen and touch-screen, and touch-screen is configured in the display screen upper surface; Wherein, display screen is LCDs.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described demonstration touch-control module is 4.3 cun, 5 cun, 5.3 cun, 7 cun or 8 cun touch-screens, resolution is 800 * 480 or 960 * 540.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described locating module is the Big Dipper/GPS bimodulus locating module.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described attitude measurement module comprises three axis accelerometer, three-axis gyroscope and three axle magnetoresistive transducers.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described airplane data input interface matches with existing device on the aircraft, and described airplane data input interface is USB interface, PS/2 interface, SATA interface, 1394 interfaces, RS-232 interface or RS-485 interface.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described communication interface comprises wireless signal transmitter and wireless signal receiver.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described video voice module comprise and show display screen that touch-control module shares and personal loudspeaker.
Because the present invention is used for the Wing Newsletter location navigation safe operation management backup system in navigation field, comprise central controller, and the demonstration touch-control module that is connected with central controller, locating module, attitude measurement module, airplane data input interface, communication interface and video voice module; This design is so that this assisting navigation equipment is applicable to General Aviation operation aircraft, can alleviate driver workload, improve aircraft operation efficient, strengthen the safe flight guarantee, make command centre can understand at any time jurisdiction operation aircraft more specific location information, coursespeed, the information such as height, solved exist at present always because the difficult problem that the wireless communication limited navigation operation aircraft position that causes can't be grasped.
Description of drawings
Fig. 1 is safe operation management circuit of auxiliary system connection diagram of the present invention.
Among the figure: 1 central controller, 2 shows touch-control module, 3 locating modules, 4 attitude measurement modules, 41 three axis accelerometers, 42 three-axis gyroscopes, 43 3 axle magnetoresistive transducers, 5 airplane data input interfaces, 6 communication interfaces, 7 video voice modules.
Embodiment
Below in conjunction with accompanying drawing the specific embodiment of the invention is described in further detail.
The Wing Newsletter location navigation safe operation management backup system that is used for the navigation field of present embodiment, the circuit connection diagram of this safe operation management backup system as shown in Figure 1, this safe operation management backup system comprises central controller 1, connects locating module 3, attitude measurement module 4, the airplane data input interface 5 of central processing unit 1 data input pin; The demonstration touch-control module 2, communication interface 6 and the video voice module 7 that connect central processing unit 1 bidirectional data transfers end.
Described demonstration touch-control module 2 comprises display screen and touch-screen, and touch-screen is configured in the display screen upper surface; Wherein, show that it is 800 * 480 demonstration touch screen that touch-control module 2 is preferably 8 cun resolution, can also select other size, such as 4.3 cun, 5 cun, 5.3 cun, 7 cun or 8 cun, and other resolution, such as 960 * 540.
Described locating module 3 is preferably the Big Dipper/GPS bimodulus locating module, can also select locating module of the Big Dipper.
Described attitude measurement module 4 comprises three axis accelerometer 41, three-axis gyroscope 42 and three axle magnetoresistive transducers 43.And the quantity of three axis accelerometer 41 is no less than two, and the quantity of three-axis gyroscope 42 is no less than two, and the quantity of three axle magnetoresistive transducers 43 is no less than two, has only drawn one of them in accompanying drawing 1.
Described airplane data input interface 5 matches with existing device on the aircraft, and described airplane data input interface 5 is preferably USB interface; This interface can also be chosen as PS/2 interface, SATA interface, 1394 interfaces, RS-232 interface or RS-485 interface.
Described communication interface 6 comprises wireless signal transmitter and wireless signal receiver.
Described video voice module 7 comprises and shows display screen that touch-control module 2 shares and personal loudspeaker.
Safe operation management backup system of the present invention is applied to the General Aviation field, can alleviate driver workload, improve aircraft operation efficient, strengthen the safe flight guarantee, make command centre can understand at any time jurisdiction operation aircraft more specific location information, coursespeed, the information such as height, solved exist at present always because the difficult problem that the wireless communication limited navigation operation aircraft position that causes can't be grasped.
Claims (8)
1. the Wing Newsletter location navigation safe operation management backup system that is used for the navigation field, it is characterized in that comprising central controller (1), connect locating module (3), attitude measurement module (4), the airplane data input interface (5) of central processing unit (1) data input pin; The demonstration touch-control module (2), communication interface (6) and the video voice module (7) that connect central processing unit (1) bidirectional data transfers end.
2. the Wing Newsletter location navigation safe operation management backup system for the navigation field according to claim 1 it is characterized in that described demonstration touch-control module (2) comprises display screen and touch-screen, and touch-screen is configured in the display screen upper surface; Wherein, display screen is LCDs.
3. backup system is managed in the Wing Newsletter location navigation safe operation for the navigation field according to claim 2, it is characterized in that described demonstration touch-control module is 4.3 cun, 5 cun, 5.3 cun, 7 cun or 8 cun touch-screens, resolution is 800 * 480 or 960 * 540.
4. the Wing Newsletter location navigation safe operation management backup system for the navigation field according to claim 1 is characterized in that described locating module (3) is the Big Dipper/GPS bimodulus locating module.
5. the Wing Newsletter location navigation safe operation management backup system for the navigation field according to claim 1 is characterized in that described attitude measurement module (4) comprises three axis accelerometer (41), three-axis gyroscope (42) and three axle magnetoresistive transducers (43).
6. backup system is managed in the Wing Newsletter location navigation safe operation for the navigation field according to claim 1, it is characterized in that described airplane data input interface (5) matches with existing device on the aircraft, described airplane data input interface (5) is USB interface, PS/2 interface, SATA interface, 1394 interfaces, RS-232 interface or RS-485 interface.
7. the Wing Newsletter location navigation safe operation management backup system for the navigation field according to claim 1 is characterized in that described communication interface (6) comprises wireless signal transmitter and wireless signal receiver.
8. the Wing Newsletter location navigation safe operation management backup system for the navigation field according to claim 1 is characterized in that described video voice module (7) comprises and shows display screen that touch-control module (2) shares and personal loudspeaker.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012104379592A CN102914305A (en) | 2012-11-06 | 2012-11-06 | Aircraft communication, positioning and navigation safety operation management auxiliary system for general aviation field |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012104379592A CN102914305A (en) | 2012-11-06 | 2012-11-06 | Aircraft communication, positioning and navigation safety operation management auxiliary system for general aviation field |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102914305A true CN102914305A (en) | 2013-02-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012104379592A Pending CN102914305A (en) | 2012-11-06 | 2012-11-06 | Aircraft communication, positioning and navigation safety operation management auxiliary system for general aviation field |
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Cited By (1)
| 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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| US20110241901A1 (en) * | 2005-07-05 | 2011-10-06 | Gulfstream Aerospace Corporation | Standby Display Aircraft Management System |
| CN102343980A (en) * | 2010-07-28 | 2012-02-08 | 霍尼韦尔国际公司 | Method and system for attitude differentiation in enhanced vision images |
| CN202435404U (en) * | 2011-12-16 | 2012-09-12 | 西安上尚机电有限公司 | Air communication relay and reconnaissance system |
| CN102707725A (en) * | 2012-06-12 | 2012-10-03 | 桂林飞宇电子科技有限公司 | Fixed-wing automatic navigation flight control system and using method thereof |
| CN202869495U (en) * | 2012-11-06 | 2013-04-10 | 哈尔滨盈盛翔科技开发有限公司 | Safe operation management auxiliary system for aircraft communication location and navigation used for general aviation field |
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2012
- 2012-11-06 CN CN2012104379592A patent/CN102914305A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110241901A1 (en) * | 2005-07-05 | 2011-10-06 | Gulfstream Aerospace Corporation | Standby Display Aircraft Management System |
| CN102343980A (en) * | 2010-07-28 | 2012-02-08 | 霍尼韦尔国际公司 | Method and system for attitude differentiation in enhanced vision images |
| CN202435404U (en) * | 2011-12-16 | 2012-09-12 | 西安上尚机电有限公司 | Air communication relay and reconnaissance system |
| CN102707725A (en) * | 2012-06-12 | 2012-10-03 | 桂林飞宇电子科技有限公司 | Fixed-wing automatic navigation flight control system and using method thereof |
| CN202869495U (en) * | 2012-11-06 | 2013-04-10 | 哈尔滨盈盛翔科技开发有限公司 | Safe operation management auxiliary system for aircraft communication location and navigation used for general aviation field |
Cited By (1)
| 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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Application publication date: 20130206 |