CN112193426A - Quick integration method for realizing plug and play of task load - Google Patents
Quick integration method for realizing plug and play of task load Download PDFInfo
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- CN112193426A CN112193426A CN202010952539.2A CN202010952539A CN112193426A CN 112193426 A CN112193426 A CN 112193426A CN 202010952539 A CN202010952539 A CN 202010952539A CN 112193426 A CN112193426 A CN 112193426A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
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Abstract
The invention belongs to the technical field of unmanned aerial vehicle design, and discloses a quick integration method for realizing plug and play of task loads, which comprises the steps of firstly analyzing the task loads, and determining the classification of each functional channel of the task loads, wherein the classification comprises an installation channel, a power supply channel, an instruction channel, an information transmission channel and a display control channel; then, designing standard plug-and-play interfaces according to the classification of each functional channel of the task load; and finally, integrating the task load on the airplane, wherein each functional channel of the task load is matched with the functional channel of the airplane. According to the invention, through a rapid integration method of load classification and functional channel design, plug and play of task loads are realized, the task load integration period is greatly shortened, the development cost is reduced, the requirements of users can be rapidly met, various task loads are integrated, and the application field of the unmanned aerial vehicle is expanded.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicle design, relates to an integration method of unmanned aerial vehicle task load, and particularly relates to a quick integration method for realizing plug and play of task load.
Background
With the continuous development of the application technology of the unmanned aerial vehicle, the unmanned aerial vehicle is more and more widely applied to military fields such as information reconnaissance, border patrol, ground attack, electronic countermeasure and the like and civil fields such as artificial precipitation, forest fire prevention, disaster prevention and control, emergency rescue, communication relay and the like. More and more domestic and foreign users put forward the demands, and various task loads specified by the users are rapidly integrated on the basis of the existing unmanned aerial vehicle task system so as to adapt to different task demands of the users. Traditional task load needs physical interface, communication interface, power supply interface etc. between special design task load and the unmanned aerial vehicle when integrated to unmanned aerial vehicle, and the development cycle is long, and the development cost is high to the development quantity is great, has the characteristics of variety. When the task load types reach dozens or hundreds, the load integration workload is huge, the development period is seriously lagged, and the cost is continuously increased.
Disclosure of Invention
In order to solve the problems, the invention provides a quick integration method for realizing the plug and play of the task load, which realizes the plug and play of the task load, greatly improves the speed of task load integration, and greatly reduces the upgrading period and the improvement cost of an unmanned aerial vehicle task system.
The technical scheme of the invention is as follows:
a fast integration method for realizing plug and play of task load, firstly analyzing the task load and determining the classification of each functional channel; then, designing standard plug-and-play interfaces according to the classification of each functional channel of the task load; and finally, integrating the task load on the airplane, wherein each functional channel of the task load is matched with the functional channel of the airplane.
Further, the functional channels of the task load comprise an installation channel, a power supply channel, a command channel, an information transmission channel and a display control channel.
Further, the installation channels of the task loads are classified into three types, namely large, medium and small according to the sizes of the task loads.
Further, the power supply channels of the task load are classified into three types, namely high, medium and low, according to the power consumption of the task load.
Further, the instruction channels of the task load are classified according to the communication bus interfaces of the task load, and are classified into 1553B types, RS442 types, ethernet types and other types of all communication buses used by the existing unmanned aerial vehicle.
Further, the information transmission channels of the task load are classified according to task information provided by the task load, and are divided into a digital video class, a high-definition image class and a digital report class; the digital video task load provides continuous and uninterrupted digital video intelligence for the unmanned aerial vehicle; the high-definition image task load provides high-definition image information of air, ground and sea for the unmanned aerial vehicle; the digital information task load provides digital information such as communication, radio and the like for the unmanned aerial vehicle.
Further, the display control channels of the task loads are classified according to the software concentration ratio of the ground control stations of the task loads and are divided into a centralized control type and a distributed control type; only the task load of the decentralized control class enables the design of a standard plug and play interface.
Furthermore, according to the classification of each functional channel of the task load, a plug-and-play interface matched with the installation channel, the power supply channel, the instruction channel, the information transmission channel and the display control channel is designed, then the integration work is distributed to each functional channel according to the classification condition of the task load, and the plug-and-play of the task load is realized through the distribution and combination of the functional channels.
The invention has the advantages that:
according to the invention, through a rapid integration method of load classification and functional channel design, plug and play of task loads are realized, the task load integration period is greatly shortened, the development cost is reduced, the requirements of users can be rapidly met, various task loads are integrated, and the application field of the unmanned aerial vehicle is expanded.
Drawings
FIG. 1 is a schematic diagram of a task load function channel classification method according to the present invention;
fig. 2 is a schematic diagram of a fast integration method of task load according to functional channel classification according to an embodiment of the present invention.
Detailed Description
This section is an example of the present invention and is provided to explain and illustrate the technical solutions of the present invention.
A fast integration method for realizing plug and play of task load, firstly analyzing the task load and determining the classification of each functional channel; then, designing standard plug-and-play interfaces according to the classification of each functional channel of the task load; and finally, integrating the task load on the airplane, wherein each functional channel of the task load is matched with the functional channel of the airplane.
The functional channels of the task load comprise an installation channel, a power supply channel, an instruction channel, an information transmission channel and a display control channel. The installation channels of the task loads are classified according to the sizes of the task loads and are divided into three types, namely large, medium and small. The power supply channels of the task loads are classified into three types, namely high, medium and low, according to the power consumption of the task loads. The command channels of the task load are classified according to the communication bus interfaces of the task load, and are divided into 1553B type, RS442 type, Ethernet type and other types of all communication buses used by the existing unmanned aerial vehicle. The information transmission channels of the task load are classified according to task information provided by the task load and are divided into a digital video class, a high-definition image class and a digital information class; the digital video task load provides continuous and uninterrupted digital video intelligence for the unmanned aerial vehicle; the high-definition image task load provides high-definition image information of air, ground and sea for the unmanned aerial vehicle; the digital information task load provides digital information such as communication, radio and the like for the unmanned aerial vehicle. The display control channels of the task load are classified according to the software concentration ratio of the ground control station of the task load and are divided into a centralized control type and a distributed control type; only the task load of the decentralized control class enables the design of a standard plug and play interface.
According to the classification of each functional channel of the task load, a plug-and-play interface matched with the installation channel, the power supply channel, the instruction channel, the information transmission channel and the display control channel is designed, then the integration work is distributed to each functional channel according to the classification condition of the functional channels of the task load, and the plug-and-play of the task load is realized through the distribution and combination of the functional channels.
Another embodiment of the present invention is described below with reference to the drawings.
The invention provides a rapid integration method based on load classification and functional channel design for better solving the problem of integration of various task loads of an unmanned aerial vehicle, so that plug and play of the task loads are realized, the task load integration speed is greatly improved, and the upgrading period and the improvement cost of an unmanned aerial vehicle task system are greatly reduced. The technology is successfully applied to the task load integration design process of the multi-type unmanned aerial vehicle.
Unmanned aerial vehicle task load is the main component of task system, and the kind and the function of task load have decided unmanned aerial vehicle application area's width and degree of depth. At present, the task load is various in kind and various in function, but according to unmanned aerial vehicle task load size, power consumption, the task information that provides etc. can be with the task load carry out following classification, as shown in fig. 1:
classifying according to task load volume: can be divided into three categories, large, medium and small.
Classifying according to task load power consumption: can be divided into three categories of high, medium and low.
Classifying according to task load communication bus interfaces: can be classified as 1553B, RS422, ethernet, etc.
The task information provided by the task load is classified into the following categories.
(1) Digital video class payload
The digital video load mainly provides continuous and uninterrupted digital video information for the unmanned aerial vehicle, and comprises a photoelectric monitoring/aiming nacelle, a visible light monitoring nacelle, an infrared monitoring nacelle and the like.
(2) High definition image class load
The high-definition image loads mainly provide high-definition image information of air, ground and sea for the unmanned aerial vehicle, and comprise a meteorological radar, a synthetic aperture radar, a high-altitude visible light CCD camera, a multispectral camera, a hyperspectral camera and the like.
(3) Digital information type load
The digital information load mainly provides digital information such as communication, radio and the like for the unmanned aerial vehicle, and comprises a communication relay load, an emergency communication load, a communication reconnaissance load, a radar reconnaissance load, an environmental measurement load and the like.
According to the software concentration degree of the ground control station, the centralized control and the distributed control are mainly adopted to realize the plug and play of the task load, a distributed control mode is required, and the load display control is realized by a load control software and a load display software interface.
In order to meet the requirement of rapid integration and plug and play of task loads, the unmanned aerial vehicle needs to provide a standard functional channel for the task loads so as to meet the requirements of interfaces such as load installation, power supply, instruction, information transmission and display. The plug and play task load is quickly integrated to design the following functional channels: the device comprises an installation channel, a power supply channel, an instruction channel, an information transmission channel and a display control channel. And then, according to task load classification, distributing the integration work to each functional channel, and realizing the plug-and-play of the task load through the distribution and combination of the functional channels.
Fig. 2 is a typical block diagram for fast integration of task loads, where the unmanned aerial vehicle designs various plug-and-play function channels, and selects a corresponding function channel according to different types of task loads to be integrated, so as to realize plug-and-play of task loads without changing the state of the unmanned aerial vehicle.
The unmanned aerial vehicle platform needs the predesigned installation passageway that adapts to the installation of various volume task loads, provides big, well, little equipment cabin and ventral string point, supplies task load optional equipment. The power supply system provides high (2500Kw), medium (1000Kw) and low (300Kw)28V direct current power supply channels, and meets power supply requirements of different task loads. The instruction channel is formed by transmission buses such as 1553B, RS422 and Ethernet, and is crosslinked through a ground control station, a link system and a task machine, so that instruction transmission is provided for task loads, and load control is realized. The design of the information transmission channels comprises that a HD-SDI bus transmits task load digital video, a CameraLink bus transmits task load high-definition images, and a 1394B bus transmits task load digital information, a task data recorder compresses and records reconnaissance data of each information transmission channel, and the compressed data is transmitted to an unmanned aerial vehicle ground control station through a link system. The display control channel is arranged in the ground control station of the unmanned aerial vehicle, and load control software, display software and the ground station are integrated through a standard protocol interface to complete display control of the task load.
Claims (8)
1. A fast integration method for realizing plug and play of task load is characterized in that firstly, the task load is analyzed to determine the classification of each functional channel; then, designing standard plug-and-play interfaces according to the classification of each functional channel of the task load; and finally, integrating the task load on the airplane, wherein each functional channel of the task load is matched with the functional channel of the airplane.
2. The method as claimed in claim 1, wherein the functional channels of the task load include installation channel, power supply channel, command channel, intelligence transmission channel and display control channel.
3. The method according to claim 2, wherein the installation channels of the task load are classified into three categories, i.e. large, medium and small, according to the size of the task load.
4. The method according to claim 2, wherein the power supply channels of the task load are classified into high, medium and low according to the power consumption of the task load.
5. The method according to claim 2, wherein the command channels of the task load are classified according to the communication bus interface of the task load, and are classified into any communication bus types currently used by the unmanned aerial vehicle, such as 1553B type, RS442 type, and ethernet type.
6. The method of claim 2, wherein the information transmission channels of the task load are classified into digital video, high definition image and digital newspaper according to the task information provided by the task load; the digital video task load provides continuous and uninterrupted digital video intelligence for the unmanned aerial vehicle; the high-definition image task load provides high-definition image information of air, ground and sea for the unmanned aerial vehicle; the digital information task load provides digital information such as communication, radio and the like for the unmanned aerial vehicle.
7. The method as claimed in claim 2, wherein the display control channels of the task load are classified according to the software concentration of the ground control station of the task load, and are classified into a centralized control type and a distributed control type; only the task load of the decentralized control class enables the design of a standard plug and play interface.
8. The method as claimed in claim 2, wherein the plug-and-play interface is adapted to the installation channel, the power supply channel, the command channel, the intelligence transmission channel and the display control channel according to the classification of each functional channel of the task load, and the integration work is distributed to each functional channel according to the classification of the task load, and the plug-and-play of the task load is realized by the distribution and combination of the functional channels.
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2881544A3 (en) * | 2004-01-27 | 2006-08-04 | Sinovia Sa | Ground or edge segment forming method for air or land or underwater robot, involves controlling spatial and time constraints and constraints related to modularity and evolutionary character of modular software |
| EP3057812A1 (en) * | 2013-10-15 | 2016-08-24 | Skypersonic LLC | Enclosed drone apparatus and method for use thereof |
| CN106919153A (en) * | 2017-01-12 | 2017-07-04 | 西南电子技术研究所（中国电子科技集团公司第十研究所） | Electronic equipment on satellite Integrated system management and control framework |
| US20170255198A1 (en) * | 2016-03-04 | 2017-09-07 | Animusoft Corporation | Drone and robot control systems and methods |
| CN107422742A (en) * | 2017-08-16 | 2017-12-01 | 广东容祺智能科技有限公司 | A kind of unmanned plane multifunctional service Towed bird system |
| CN108762295A (en) * | 2018-02-09 | 2018-11-06 | 华南理工大学 | Integrated unmanned aerial vehicle control system based on software bus |
-
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- 2020-09-11 CN CN202010952539.2A patent/CN112193426B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2881544A3 (en) * | 2004-01-27 | 2006-08-04 | Sinovia Sa | Ground or edge segment forming method for air or land or underwater robot, involves controlling spatial and time constraints and constraints related to modularity and evolutionary character of modular software |
| EP3057812A1 (en) * | 2013-10-15 | 2016-08-24 | Skypersonic LLC | Enclosed drone apparatus and method for use thereof |
| US20170255198A1 (en) * | 2016-03-04 | 2017-09-07 | Animusoft Corporation | Drone and robot control systems and methods |
| CN106919153A (en) * | 2017-01-12 | 2017-07-04 | 西南电子技术研究所（中国电子科技集团公司第十研究所） | Electronic equipment on satellite Integrated system management and control framework |
| CN107422742A (en) * | 2017-08-16 | 2017-12-01 | 广东容祺智能科技有限公司 | A kind of unmanned plane multifunctional service Towed bird system |
| CN108762295A (en) * | 2018-02-09 | 2018-11-06 | 华南理工大学 | Integrated unmanned aerial vehicle control system based on software bus |
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