CN103927906A - Big Dipper autonomous navigation method based on Big Dipper short message and 4G communication mode - Google Patents
Big Dipper autonomous navigation method based on Big Dipper short message and 4G communication mode Download PDFInfo
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Abstract
The invention discloses a Big Dipper autonomous navigation method based on a Big Dipper short message and a 4G communication mode. Namely, a Big Dipper type airborne device acquires information of the current position, speed, time and the like of an airplane in real time and issues the information in the form of an ADS-C message according to the requirement of a ground system. Meanwhile, a ground low altitude flight operation monitoring system receives airspace situation information from other systems, and after coding and processing the situation of the other airplanes around a target airplane, the ground low altitude flight operation monitoring system sends the situation to the Big Dipper type airborne device in the form of the short message through a Big Dipper directing type user machine or the 4G communication device. According to the Big Dipper autonomous navigation method, the positioning information sent by the Big Dipper type airborne device can be received, monitoring can be achieved at a low altitude, flying data of the position, height, speed and the like in the flying process of a navigation aircraft can be recorded in real time through an airborne data recording module, emergency directing communication can be conducted on the aircraft loaded with the Big Dipper type airborne device through a Big Dipper short message channel, and low altitude navigation seamless coverage can be achieved.
Description
Technical field
The present invention relates to the method for the Big Dipper independent navigation based on Big Dipper short message and 4G communication pattern, belong to the General Aviation applied technical field of air traffic control.
Background technology
At present, traditional prior art adopts secondary radar and ADS (Automatic Dependent Surveillance conventionally, automatic dependent surveillance) etc. technology monitors to solve the problem of low latitude aircraft " cannot see (over the horizon can not be identified) " to low altitude airspace, and adopting the shortcoming of the prior art of secondary radar is that radar coverage is low, maneuverability is poor; And adopt ADS technology to solve the supervision to low altitude airspace that existing air traffic control radar do not cover, need to set up land station, this will greatly increase cost and can not realize low latitude aircraft is monitored effectively again simultaneously.
Summary of the invention
The object of the present invention is to provide a kind of method that can overcome the Big Dipper independent navigation based on Big Dipper short message and 4G communication pattern of above-mentioned technical matters, the present invention is directed to low latitude aircraft target little, maneuverability is high, independence is strong, be difficult to accurately grasp the dynamic problem of flight, in conjunction with Chinese low-latitude flying feature, consider technology maturity, the factor of the aspects such as construction cost, compatible ADS-B (the Automatic Dependent Surveillance-Broadcast based on 1090ES communication, Automatic dependent surveillance broadcast), radar surveillance technology, in particular surroundings and some areas with Big Dipper short message, 4G, trunking communication is supplementary technical system, set up the Big Dipper/GPS multi-source location, ADS-C (the Automatic Dependent Surveillance-Contract of Big Dipper short message/4G multi-mode communication, Automated dependent surveillance contract) the low latitude independent navigation of pattern and operation inspection system.
The present invention is based on aeronautical telecommunication network and effectively solved the technical matterss such as the information such as aircraft supervision move in several data chain land station covering domain, switching, meanwhile, the present invention also solved well air to air, air to surface and ground-to-ground between the technical matters of exchanges data.
The hardware system of the method for the Big Dipper independent navigation based on Big Dipper short message and 4G communication pattern of the present invention is mainly comprised of airborne end equipment and ground surface end equipment; Described airborne end equipment comprises Big Dipper type airborne equipment and possesses the electronic flight services package of 4G communication service; Described ground surface end equipment comprises Big Dipper command type subscriber computer and installs the ground low-latitude flying operation monitoring system of 4G communication module additional.
The ultimate principle of the method for the Big Dipper independent navigation based on Big Dipper short message and 4G communication pattern of the present invention is: in low-latitude flying process, the requirement of the information such as the current position of Big Dipper type airborne equipment or electronic flight services package Real-time Obtaining aircraft, speed, time base area plane system issues with the form of ADS-C message; Simultaneously, ground low-latitude flying operation monitoring system receives the spatial domain situation information from other system, and after the situation coding of other aircraft of target aircraft periphery is processed, by Big Dipper command type subscriber computer or 4G communication facilities, in the mode of short message, send Big Dipper type airborne equipment or electronic flight services package to, to realize relevant Situation Awareness between accurate, real-time machine; For Big Dipper communication pattern, the information such as Big Dipper type airborne equipment or electronic flight services package synthesis display visual flight Electronic Aviation Map, self-position, periphery situation, have and support User Defined navigation way, driftage alarm is provided, collision alert, automatically generate the functions such as log.
The concrete steps of method of the present invention are as follows:
(1) airborne end equipment utilization Big Dipper Position Fixing Navigation System obtains the navigator fix information such as position, speed, time point of aircraft, these locating navigation informations are packaged into ADS-C standard information, by Big Dipper short message, communicate by letter or 4G mobile communication sends to ground low-latitude flying operation monitoring system;
(2) ground low-latitude flying operation monitoring system is collected the ADS-C of other aircrafts, draws simultaneously and connects outside radar information and ADS-B information, realizes comprehensive empty feelings and monitors; And the empty mood gesture of the periphery of corresponding airborne end equipment is packaged into ADS-C information sends to airborne end equipment;
(3) airborne end equipment is to periphery situation processes and displays, and carries out flight safety relevant treatment and warning prompting;
(4) airborne end equipment for flight collision, region conflict, aviation fuel lack, communication failure, the emergent report information such as be held as a hostage all by Big Dipper short message, is communicated by letter or 4G mobile communication sends to ground low-latitude flying operation monitoring system, for ground provides safe flight commander foundation;
(5) ground low-latitude flying operation monitoring system, for the flight information of collecting, meteorologic information information after examination, sends command information to airborne end equipment, for aircrew provides safe flight reference frame;
(6) in addition, airborne end equipment and ground low-latitude flying operation monitoring system need according to flight, commander can be by sending all kinds of real time interaction informations, for aerial mission is implemented and flight safety management and control provides reference frame.
Advantage of the present invention is as follows:
(1) can the information of low latitude aircraft be managed and be safeguarded, can store essential information and the multidate information of low latitude aircraft, can receive location register and the de-registration request of low latitude aircraft.
(2) can receive the locating information that Big Dipper type airborne equipment sends, by showing high available low latitude chart, realize flight assisting navigation function, be convenient to pilot and understand self-position.Multiple utility can be provided, and as navigation/monitoring mode switches, draw/speed of position is drawn calculating, rang ring etc., assisted user navigates.Swarming into forbidden zone, cross over spatial domain, leap hi-line area, with other aircraft spacings, in the situation such as nearer, initiatively to aircrew, send information warning.
(3) can be at low latitude real time monitoring: by ADS-C Ground-to-Air Data Link technology, to having loaded the low latitude aircraft of Big Dipper type airborne equipment and 4G communication facilities, carry out real time monitoring.
(4) can pass through on-board data logging modle, to the position in navigation aircraft flight course, highly, the flying quality such as speed carries out real time record.
(5) can with the aircraft that has loaded Big Dipper type airborne equipment, carry out emergency command communication by Big Dipper short message channel.
(6) can realize low level navigation seamless coverage: the Big Dipper/GPS multi-source is located obtaining of basic implementation space independent navigation information source; Ground surveillance is further improved roomage state information by air traffic control radar information and the ADSB of 1090E land station information.At the low dummy section that has 4G to cover, can reach Air-Ground data link by 4G communication; At the low altitude airspace covering without 4G, further by Big Dipper short message, the Air-Ground data link under seamless pattern is reached in communication.
Accompanying drawing explanation
Fig. 1 is the hardware system structure schematic diagram of the method for the Big Dipper independent navigation based on Big Dipper short message and 4G communication pattern of the present invention.
Embodiment
Below in conjunction with drawings and Examples, describe the present invention.As shown in Figure 1, the concrete steps of method of the present invention are as follows:
(1) airborne end equipment utilization Big Dipper Position Fixing Navigation System obtains the navigator fix information such as position, speed, time point of aircraft, these locating navigation informations are packaged into ADS-C standard information, by Big Dipper short message, communicate by letter or 4G mobile communication sends to ground low-latitude flying operation monitoring system;
(2) ground low-latitude flying operation monitoring system is collected the ADS-C of other aircrafts, draws simultaneously and connects outside radar information and ADS-B information, realizes comprehensive empty feelings and monitors; And the empty mood gesture of the periphery of corresponding airborne end equipment is packaged into ADS-C information sends to airborne end equipment;
(3) airborne end equipment is to periphery situation processes and displays, and carries out flight safety relevant treatment and warning prompting;
(4) airborne end equipment for flight collision, region conflict, aviation fuel lack, communication failure, the emergent report information such as be held as a hostage all by Big Dipper short message, is communicated by letter or 4G mobile communication sends to ground low-latitude flying operation monitoring system, for ground provides safe flight commander foundation;
(5) ground low-latitude flying operation monitoring system, for the flight information of collecting, meteorologic information information after examination, sends command information to airborne end equipment, for aircrew provides safe flight reference frame;
(6) in addition, airborne end equipment and ground low-latitude flying operation monitoring system need according to flight, commander can be by sending all kinds of real time interaction informations, for aerial mission is implemented and flight safety management and control provides reference frame.
The above; be only the specific embodiment of the present invention, but protection scope of the present invention is not limited to this, is anyly familiar with those skilled in the art in scope disclosed by the invention; the variation that can expect easily or replacement, all should be encompassed in the protection domain of the claims in the present invention.
Claims (1)
1. the method for the Big Dipper independent navigation based on Big Dipper short message and 4G communication pattern, is characterized in that, comprises following concrete steps:
(1) airborne end equipment utilization Big Dipper Position Fixing Navigation System obtains the navigator fix information such as position, speed, time point of aircraft, these locating navigation informations are packaged into ADS-C standard information, by Big Dipper short message, communicate by letter or 4G mobile communication sends to ground low-latitude flying operation monitoring system;
(2) ground low-latitude flying operation monitoring system is collected the ADS-C of other aircrafts, draws simultaneously and connects outside radar information and ADS-B information, realizes comprehensive empty feelings and monitors; And the empty mood gesture of the periphery of corresponding airborne end equipment is packaged into ADS-C information sends to airborne end equipment;
(3) airborne end equipment is to periphery situation processes and displays, and carries out flight safety relevant treatment and warning prompting;
(4) airborne end equipment for flight collision, region conflict, aviation fuel lack, communication failure, the emergent report information such as be held as a hostage all by Big Dipper short message, is communicated by letter or 4G mobile communication sends to ground low-latitude flying operation monitoring system, for ground provides safe flight commander foundation;
(5) ground low-latitude flying operation monitoring system, for the flight information of collecting, meteorologic information information after examination, sends command information to airborne end equipment, for aircrew provides safe flight reference frame;
(6) in addition, airborne end equipment and ground low-latitude flying operation monitoring system need according to flight, commander can be by sending all kinds of real time interaction informations, for aerial mission is implemented and flight safety management and control provides reference frame.
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| CN104501828A (en) * | 2014-12-29 | 2015-04-08 | 吉林大学 | General aviation onboard monitoring system |
| CN104504936A (en) * | 2014-12-09 | 2015-04-08 | 沈阳航空航天大学 | Low-cost general aviation aircraft navigation monitoring method and device |
| CN104750111A (en) * | 2015-03-09 | 2015-07-01 | 王琪杰 | Flying monitoring system of unmanned aerial vehicle |
| CN105070105A (en) * | 2015-07-29 | 2015-11-18 | 重庆赛乐威航空科技有限公司 | Low-altitude aircraft dynamic monitoring system |
| CN105610489A (en) * | 2016-01-05 | 2016-05-25 | 中国航空无线电电子研究所 | Low-altitude airspace monitoring system based on urban wireless communication network |
| CN105676249A (en) * | 2016-04-20 | 2016-06-15 | 中国民航大学 | Navigation airplane communication navigation monitoring system and method based on 4G/3G/BDS |
| CN105867272A (en) * | 2016-04-14 | 2016-08-17 | 中国电子科技集团公司第五十四研究所 | Safety monitoring method for universal aerial vehicle and unmanned aerial vehicle |
| CN105913692A (en) * | 2016-06-06 | 2016-08-31 | 北京威胜通达科技有限公司 | Flight monitoring service method and system thereof |
| CN106504588A (en) * | 2016-10-25 | 2017-03-15 | 中国民航大学 | Based on Beidou II and the multi-platform low latitude domain monitoring system and method for mobile network |
| CN107356940A (en) * | 2017-08-11 | 2017-11-17 | 四川联丰云网科技有限公司 | Low-altitude surveillance system based on Beidou satellite communication |
| CN107403563A (en) * | 2016-05-19 | 2017-11-28 | 中国民用航空总局第二研究所 | Open the navigation or air flight absolutely empty supervision equipment, method, system and all purpose aircraft |
| CN107591032A (en) * | 2016-07-07 | 2018-01-16 | 泰勒斯公司 | For calculating required navigational foreseeable apparatus and method |
| CN109191920A (en) * | 2018-08-24 | 2019-01-11 | 民航中南空管设备工程公司 | Beidou autonomous navigation method based on Big Dipper short message |
| CN109559566A (en) * | 2018-11-30 | 2019-04-02 | 南京航空航天大学 | A kind of planing method in busy airport termination environment visual flight air route |
| CN110379210A (en) * | 2019-07-30 | 2019-10-25 | 四川九洲空管科技有限责任公司 | A kind of civil aircraft exception flight monitoring method and device |
| CN110689763A (en) * | 2019-09-20 | 2020-01-14 | 中国飞行试验研究院 | Airborne auxiliary navigation method, device and system based on wireless reception |
| CN111181624A (en) * | 2019-12-25 | 2020-05-19 | 中电科航空电子有限公司 | Airborne Beidou system and application method thereof |
| CN112017479A (en) * | 2019-05-28 | 2020-12-01 | 华航信航空科技(浙江)有限公司 | Navigation flight monitoring and early warning system |
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| CN113328788B (en) * | 2021-06-08 | 2023-09-26 | 中国商用飞机有限责任公司 | Test system and test method for airborne Beidou short message receiving and transmitting system |
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