CN105791398A - Multi-task component communications method for unmanned airplane vehicle - Google Patents
Multi-task component communications method for unmanned airplane vehicle Download PDFInfo
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- CN105791398A CN105791398A CN201610110146.0A CN201610110146A CN105791398A CN 105791398 A CN105791398 A CN 105791398A CN 201610110146 A CN201610110146 A CN 201610110146A CN 105791398 A CN105791398 A CN 105791398A
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/12—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/12—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
- H04L67/125—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks involving control of end-device applications over a network
Abstract
The present invention discloses a multi-task component communications method for an unmanned airplane vehicle. Specifically, the method includes a first step of for a certain unmanned airplane vehicle, determining, according to a system need, the quantity of replaceable task components communicating with a communications hub device; a second step of sequentially marking a component type code of each task component; a third step of setting a general communications frame format of the communications hub device and each task component; and a fourth step of identifying, by the communications hub device, the task component according to the component type code Ti, and acquiring or filling information content of the task component Ti, so as to finish communications. According to the method, in a case in which the change cost is minimum, the adaptability of the communications hub device to the multi-task component is realized, so that the cost for system transformation or research and development is reduced, the research and development progress is accelerated, the method is flexible and convenient, maintenance in later period is simple, benefits are maximized, and a reliable and convenient method is offered for loading or replacement of the multi-task component of the multi-purpose unmanned airplane vehicle.
Description
Technical field
The invention belongs to unmanned aerial vehicle (UAV) control field, specifically, refer to a kind of multitask assembly means of communication being applied to unmanned plane.
Background technology
Along with quickly application and the development of unmanned air vehicle technique, particularly in military outstanding representation so that unmanned plane is increasingly subject to the favor of people.Unmanned plane has the advantage that climate condition limits seldom, can use round the clock, can charge into dangerous area overhead implemented for long periods and monitors and scout to obtain information, and energy real-time Transmission target image etc.；And, unmanned plane is because of without pilot, the physiological limit of pilot need not be considered, can be designed to simple in construction, lightweight, size is little, easy to use, easily operated and maintenance, therefore its development takes, production cost and maintenance expense more much lower than manned aircraft, also can save training pilot a large amount of expenses.
Dividing according to purposes, unmanned plane generally can be divided into following a few class:
1) target drone: the state of flight of simulated aircraft, guided missile and other various aircraft；Performance and training fighter-pilot, air defense means operator mainly for the identification of the empty weapons of various boats (preventing).
2) reconnaissance plane: carry out strategy, campaign and tactical reconnaissance, monitors battlefield, and the operation for army provides intelligence.Reconnaissance and surveillance unmanned plane is that current class is more complete, and the unmanned plane widely applied in actual combat, if the U.S. is at " global hawk " scounting aeroplane ground, " faint star " stealthy scounting aeroplane, " Predator " scounting aeroplane, " knight " scounting aeroplane.
3) bait unmanned plane: lure the electronic reconnaissance equipment starts such as enemy's radar into, obtain for information about；Analog information decoy, lures enemy's air defense means shooting, attracts enemy's firepower, and shielding one's own side's group of planes is prominent anti-.
4) UAV for electronic countermeasure: be divided into EP-3 electronic reconnaissance plane EP-3 and electronic interferences unmanned plane, the former is used for collecting communications intelligence and the electronic intelligence of enemy, for instance 147 series unmanned planes of Ruian company；The latter is used for the communication and command system of enemy is carried out electronic interferences, such as the air-Exjam unmanned plane of the U.S..
5) unmanned plane is attacked: attack, intercept ground and aerial target；Attack unmanned plane and carry the precision guided weapon of small-sized and big power, laser weapon or antiradiation missile, implement to attack and intercept the tactical missile being in motors in boost phase penetration to important goals such as enemy radar, the communication and command equipment, tanks.
6) communication relay unmanned plane: utilize unmanned plane to other warplanes or the signal such as land, naval's transmitted image, generally carry out trunking traffic with the unmanned plane being mounted with hyperfrequency and very high frequency(VHF) radio communication equipment.
7) unmanned plane of other purposes: unmanned plane can be also used for the measurement of target discriminating, laser irradiation, the aerial relay station of remote data transfer, antisubmarine, artillery fire correction and distant place upper atmosphere and the scouting etc. to chemistry, germ contamination and radioprotective.
In the system of unmanned plane forms, a crucial maincenter equipment is flight control computer.It similarly is the brain of unmanned plane, is control and the administrative center of full machine, is again the communications backbone equipment of full machine.Most of airborne equipment is required for and its communication, thus realization is mutual with what the remote pilot on ground and remote measurement showed.It needs to carry out communication with the task component on machine, engine system, air data system, navigation system, comprehensive detection system, airborne link device, blank pipe answering system etc..On the one hand, it passes through these communications, obtains the various positions of unmanned plane, status information in real time, selects suitable control strategy to realize the flight that unmanned plane is omnidistance is controlled and management；On the other hand, its real-time reception is from earth station's telecommand of airborne link device and is distributed to corresponding airborne equipment, also to collect the telemetry of other airborne equipments of packing simultaneously, earth station is passed back, in order to earth station operator can understand the state of unmanned plane in real time and control it by airborne link device.That is, it is ensured that smoothly completing of a subtask, it is necessary that the effective communication of task component and flight control computer.
The unmanned plane of different purposes, equipped with different task components.As target drone, its task component is some target equipment, and the task component of reconnaissance plane is then some reconnaissance equipments, such as photoelectric platform, digital camera etc.；Bait unmanned plane, UAV for electronic countermeasure, communication relaying unmanned plane etc., its task component then correspondence is bait equipment, countermeasures set, communication trunking etc..Namely different task components, determines the different purposes of unmanned plane.When there being different mission requirements, then the upper different unmanned plane of group completes corresponding task.Such as, when having scouting and communication relay task, use reconnaissance UAV；When having communication relay task, use communication relaying unmanned plane；When having electronic countermeasures mission, use UAV for electronic countermeasure.Usual then need this at least three framves unmanned plane is carried out maintaining.
At present, in order to save expenses of military expenditure, various countries are intended to exploitation and adapt to the multi-purpose unmanned aerial vehicle of different environment under battle conditions, or are adapted as multi-purpose unmanned aerial vehicle on the basis of original unmanned plane.Because as such, it is possible to met multiple-task demand by single rack unmanned plane, development, use cost is made to be substantially reduced.
Being expanded to multiduty demand in order to meet single rack unmanned plane by special purpose, simplest mode is the mode adopting the task component that changes the outfit.Because this mode is for whole UAS, it is only necessary to change task component and just can realize multiduty purpose.Both need not change another unmanned plane, it is not required that change other equipment being associated with task component, such as flight control computer, such Least-cost, both reduced cost, reduction of expenditure, and use and flexible, and later maintenance is simple.
So, to reach only to change task component and realize multiduty purpose, it is desirable to flight control computer must flow through same communication interface and multiple task component communications, and flight control computer is capable of identify that task component.How solving this problem, will be the special purpose unmanned plane key point that is extended to that multipurpose faces, this be also the problem that the present invention will solve.
Summary of the invention
The present invention is directed to current unmanned plane and extend multiduty demand, by communication will be carried out with communications backbone equipment after the generalization of many Frames, it is only necessary to change task component and achieve that the multipurpose function of unmanned plane；Propose a kind of multitask assembly means of communication being applied to unmanned plane, specifically comprise the following steps that
Step one: for certain unmanned plane, configures according to system, it is determined that with the replacing task component quantity that communications backbone equipment carries out communication；
Determine that the replacing task component with communications backbone device talk is m, m >=2；
Step 2: the component type code of each task component of labelling successively；
Component type code respectively T1, T2 ..., Ti ..., Tm；
Step 3: set the universal communication frame format of communications backbone equipment and each task component is as follows:
| Frame head | Component type code Ti | The information content of Ti |
Step 4: communications backbone equipment is according to component type code Ti identification mission assembly, and obtains or fill in the information content of task component Ti, completes communication；
First, communications backbone equipment judges the component type code of current task assembly, then, obtains or fills in the information content that current component type codes is corresponding, complete and the communication of current task assembly from universal communication frame format.
It is an advantage of the current invention that: by adopting the unitized method of many Frames, when Least-cost, realize the communications backbone equipment adaptability to multitask assembly, can for unmanned plane transformation or development reduction of expenditure, accelerate Development Schedule, and flexible and convenient to use, later maintenance is simple, maximizing the benefits, the multitask assembly for realizing multi-purpose unmanned aerial vehicle changes the outfit and provides a reliable shortcut easily.
Accompanying drawing explanation
Fig. 1 is a kind of multitask assembly means of communication theory diagram being applied to unmanned plane of the present invention；
Fig. 2 is a kind of multitask assembly means of communication flow chart being applied to unmanned plane of the present invention；
Detailed description of the invention
Below in conjunction with accompanying drawing and example, the present invention is described in further detail.
As shown in Figure 1, communications backbone equipment requires over a communication interface and multiple task component communications, being a general communication frames form with the communication frames format setting of multiple task component communications, in this universal communication frame format, each task component is set man-to-man component type code, communications backbone equipment utilization component type code identifies corresponding task component, then according to component type code, obtain or fill in the information content of this task component, complete and the communication of corresponding task assembly, thus realizing the communications backbone equipment purpose by a communication interface with multiple task component communications；
A kind of multitask assembly means of communication being applied to unmanned plane of the present invention, as in figure 2 it is shown, specifically comprise the following steps that
Step one: for certain unmanned plane, configures according to system, it is determined that with the replacing task component quantity that communications backbone equipment carries out communication；
Needs according to UAS, have m task component to change the outfit demand, it is thus determined that needing the replacing task component with communications backbone device talk is m；Wherein m >=2；The optional flight control computer of communications backbone equipment；
Step 2: determine the component type code of the also each task component of labelling successively；
The component type code determining first task component is T1；
The component type code determining second task component is T2；
The like, it is determined that the component type code of m-th task component is Tm；
Step 3: set the universal communication frame format of communications backbone equipment and each task component；
Universal communication frame format is as follows:
| Frame head | Component type code Ti | The information content of Ti |
Component type code Ti therein has respectively: T1, T2 ... Tm, it may be assumed that
When component type code is T1, communication frames form is:
| Frame head | T1 | The information content of T1 |
When component type code is T2, communication frames form is:
| Frame head | T2 | The information content of T2 |
The like, when component type code is Tm, communication frames form is:
| Frame head | Tm | The information content of Tm |
Step 4: communications backbone equipment is according to component type code Ti identification mission assembly, and obtains or fill in the corresponding information content of task component Ti, completes communication；
During communication, first communications backbone equipment obtain the component type code of current task assembly:
If component type code is T1, then it represents that the task component now loaded is first task component, communications backbone equipment obtains from universal communication frame format or fills in the information content of first task component, completes and the communication of first task component；
If component type code is T2, then it represents that the task component now loaded is second task component, communications backbone equipment obtains from universal communication frame format or fills in the information content of second task component, completes and the communication of second task component；
By that analogy, if component type code is Tm, then it represents that the task component now loaded is m-th task component, communications backbone equipment obtains from universal communication frame format or fills in the information content of m-th task component, completes and the communication of m-th task component.
Embodiment 1:
The present invention is applied to certain unmanned plane, and this unmanned plane can only load a task component, it is necessary to the task component changed the outfit has 2: EO-1 hyperion platform, SAR radar；
Realize concretely comprising the following steps of the present invention:
Step one: the needs according to UAS, it is determined that the replacing task component quantity carrying out communication with communications backbone equipment is 2；
It is EO-1 hyperion platform, SAR radar respectively with the replacing task component of communications backbone device talk；
Step 2: the component type code of 2 task components of labelling successively:
The component type code of labelling EO-1 hyperion platform is 0xAA；
The component type code of labelling SAR radar is 0xCC；
Step 3: set the universal communication frame format of communications backbone equipment and each task component is as follows:
When component type code is 0xAA, communication frames form is:
| Frame head | 0xAA | The information content of EO-1 hyperion platform |
When component type code is 0xCC, communication frames form is:
| Frame head | 0xCC | The information content of SAR radar |
Step 4: communications backbone equipment is according to component type code identification mission assembly, and obtains or fill in the information content of task component, completes communication；
During communication, communications backbone equipment first determines whether the component type code of current task assembly:
If component type code is 0xAA, then it represents that the task component now loaded is EO-1 hyperion platform, communications backbone equipment obtains from universal communication frame format or fills in the information content of EO-1 hyperion platform, completes and the communication of EO-1 hyperion platform；
If component type code is 0xCC, then it represents that the task component now loaded is SAR radar, communications backbone equipment obtains from universal communication frame format or fills in the information content of SAR radar, completes and the communication of SAR radar；
Embodiment 2:
The present invention is applied to certain unmanned plane, and this unmanned plane can load 2 task components simultaneously, and one of them task component is communication relay set, is the equipment that every time must fill；Another task component selects from 3 reconnaissance equipments, including: comprehensive photoelectric platform, multi-function monitoring radar, digital camera, can need to change the outfit according to every subtask.Therefore this UAS needs 3 task components changed the outfit to include: comprehensive photoelectric platform, multi-function monitoring radar, digital camera；
Realize concretely comprising the following steps of the present invention:
Step one: the needs according to UAS, it is determined that the replacing task component carrying out communication with communications backbone equipment is 3；
With the replacing task component of communications backbone device talk respectively: comprehensive photoelectric platform, multi-function monitoring radar, digital camera；
Step 2: the component type code of 3 task components of labelling successively；
The component type code of the comprehensive photoelectric platform of labelling is 0x33；
The component type code of labelling multi-function monitoring radar is 0x66；
The component type code of labelling digital camera is 0x99；
Step 3: set the universal communication frame format of communications backbone equipment and each task component is as follows:
When component type code is 0x33, communication frames form is:
| Frame head | 0x33 | The information content of comprehensive photoelectric platform |
When component type code is 0x66, communication frames form is:
| Frame head | 0x66 | The information content of multi-function monitoring radar |
When component type code is 0x99, communication frames form is:
| Frame head | 0x99 | The information content of digital camera |
Step 4: communications backbone equipment is according to component type code identification mission assembly, and obtains or fill in the information content of task component, completes communication；
During communication, communications backbone equipment first determines whether component type code:
If component type code is 0x33, then it represents that the task component now loaded is comprehensive photoelectric platform, communications backbone equipment obtains from universal communication frame format or fills in the information content of comprehensive photoelectric platform, completes and the communication of comprehensive photoelectric platform；
If component type code is 0x66, then it represents that the task component now loaded is multi-function monitoring radar, communications backbone equipment obtains from universal communication frame format or fills in the information content of multi-function monitoring radar, completes and the communication of multi-function monitoring radar；
If component type code is 0x99, then it represents that the task component now loaded is digital camera, communications backbone equipment obtains from universal communication frame format or fills in the information content of digital camera, completes the communication with digital camera.
Claims (1)
1. the multitask assembly means of communication being applied to unmanned plane, it is characterised in that specifically comprise the following steps that
Step one: for certain unmanned plane, configures according to system, it is determined that with the replacing task component quantity that communications backbone equipment carries out communication；
Determine that the replacing task component with communications backbone device talk is m, m >=2；
Step 2: the component type code of each task component of labelling successively；
Component type code respectively T1, T2 ..., Ti ..., Tm；
Step 3: set the universal communication frame format of communications backbone equipment and each task component is as follows:
Step 4: communications backbone equipment is according to component type code Ti identification mission assembly, and obtains or fill in the information content of task component Ti, completes communication；
First, communications backbone equipment judges the component type code of current task assembly, then, obtains or fills in the information content that current component type codes is corresponding, complete and the communication of current task assembly from universal communication frame format.
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109460060A (en) * | 2018-12-05 | 2019-03-12 | 四川航天系统工程研究所 | It is unmanned to equip intelligent coordinated control assembly and control method |
| CN111641489A (en) * | 2020-04-29 | 2020-09-08 | 北航长鹰航空科技(台州)有限公司 | Multitask component communication method applied to unmanned aerial vehicle |
| CN113034872A (en) * | 2019-12-25 | 2021-06-25 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle link data transmission method and device |
| WO2022022023A1 (en) * | 2020-07-28 | 2022-02-03 | 北京理工大学 | Method for controlling networking of laser terminal guidance aircrafts |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101710243A (en) * | 2009-12-23 | 2010-05-19 | 北京航空航天大学 | Method for selecting remote control mode of unmanned plane |
| CN102591346A (en) * | 2011-12-05 | 2012-07-18 | 大连理工大学 | Small-size handheld ground monitoring system for unmanned aerial vehicle |
| CN103970044A (en) * | 2014-05-09 | 2014-08-06 | 北京航空航天大学 | General hierarchical design method for unmanned aerial vehicle remote control command/telemetry parameter frame |
| EP2938044A1 (en) * | 2012-12-24 | 2015-10-28 | Tencent Technology (Shenzhen) Company Limited | System, method, apparatus, and server for displaying network medium information |
| CN105116908A (en) * | 2015-07-20 | 2015-12-02 | 清华大学 | Communication method for unmanned aerial vehicle visual formation coordination |
-
2016
- 2016-02-29 CN CN201610110146.0A patent/CN105791398A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101710243A (en) * | 2009-12-23 | 2010-05-19 | 北京航空航天大学 | Method for selecting remote control mode of unmanned plane |
| CN102591346A (en) * | 2011-12-05 | 2012-07-18 | 大连理工大学 | Small-size handheld ground monitoring system for unmanned aerial vehicle |
| EP2938044A1 (en) * | 2012-12-24 | 2015-10-28 | Tencent Technology (Shenzhen) Company Limited | System, method, apparatus, and server for displaying network medium information |
| CN103970044A (en) * | 2014-05-09 | 2014-08-06 | 北京航空航天大学 | General hierarchical design method for unmanned aerial vehicle remote control command/telemetry parameter frame |
| CN105116908A (en) * | 2015-07-20 | 2015-12-02 | 清华大学 | Communication method for unmanned aerial vehicle visual formation coordination |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109460060A (en) * | 2018-12-05 | 2019-03-12 | 四川航天系统工程研究所 | It is unmanned to equip intelligent coordinated control assembly and control method |
| CN113034872A (en) * | 2019-12-25 | 2021-06-25 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle link data transmission method and device |
| CN111641489A (en) * | 2020-04-29 | 2020-09-08 | 北航长鹰航空科技(台州)有限公司 | Multitask component communication method applied to unmanned aerial vehicle |
| CN111641489B (en) * | 2020-04-29 | 2023-03-21 | 北航长鹰航空科技(台州)有限公司 | Multitask component communication method applied to unmanned aerial vehicle |
| WO2022022023A1 (en) * | 2020-07-28 | 2022-02-03 | 北京理工大学 | Method for controlling networking of laser terminal guidance aircrafts |
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