CN107422742A - A kind of unmanned plane multifunctional service Towed bird system - Google Patents
A kind of unmanned plane multifunctional service Towed bird system Download PDFInfo
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- CN107422742A CN107422742A CN201710704409.5A CN201710704409A CN107422742A CN 107422742 A CN107422742 A CN 107422742A CN 201710704409 A CN201710704409 A CN 201710704409A CN 107422742 A CN107422742 A CN 107422742A
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 23
- 238000004891 communication Methods 0.000 claims abstract description 12
- 238000009434 installation Methods 0.000 claims abstract description 10
- 238000000034 method Methods 0.000 claims abstract description 8
- 230000005540 biological transmission Effects 0.000 claims description 9
- 238000012544 monitoring process Methods 0.000 claims description 3
- 238000012545 processing Methods 0.000 claims description 3
- 240000002853 Nelumbo nucifera Species 0.000 description 3
- 235000006508 Nelumbo nucifera Nutrition 0.000 description 3
- 235000006510 Nelumbo pentapetala Nutrition 0.000 description 3
- 238000001514 detection method Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 238000007726 management method Methods 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses a kind of unmanned plane multifunctional service Towed bird system, it is related to unmanned air vehicle technique field, including airflight plateform system and ground control centre system, the control flying platform system includes unmanned vehicle flight control system, intelligent load universal interface system and loading device, the intelligent load universal interface system includes remote sensing load installation module, remote sensing load power supply module and interface message configuration module, the ground control centre system is provided with floor synthetic command and control system, the floor synthetic command and control system includes flight control modules, link control module, load control module and flight tracking control module.A kind of unmanned plane multifunctional service Towed bird system provided by the invention, which possesses, quickly changes function, the power supply of built-in high-quality, communication interface, different loads only need easy configuration, it is simple to operate, intelligence degree is high, realize the control load operation of the remote independent by way of flight course planning.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of unmanned plane multifunctional service Towed bird system.
Background technology
Current unmanned plane aerial device is typically made up of unmanned plane during flying platform, mission payload, communication link three parts.
Mission payload subsystem refers to complete detection, collection and record, assists to complete the dress for having particular task function of air objective
Put, generally comprise photoelectric nacelle, damping head, camera, thermal infrared imager, and megaphone, gas detecting instrument, Throwing device, spy
The device of the types of applications scene such as illuminator.These devices, which only need to be installed on unmanned plane, can meet simply to work, reach
Certain mission effectiveness.
Chinese Patent Application No. discloses a kind of unmanned plane load self-identifying and parameter Self Matching for 201710147178.2
Method and ground Adaptable System, after load is carried on unmanned plane, sends and look into from the flight controller of unmanned plane to load
Instruction is ask, load sends response message according to query statement to flight controller, and flight controller is from the response message received
In parse load numbering, realize the automatic identification of unmanned plane load type；Parameter Self Matching method is based on load automatic identification,
If it is unidentified go out load numbering, using zero load under flight attitude control parameter as current control parameter, if identifying load
Numbering x, then xth group control parameter Px is transferred to control unmanned plane to carry out power matching and flight attitude adjustment；Based on load
The ground Adaptable System of automatic identification function can then activate automatically control interface, shielding and current load corresponding to load without
The interface of pass, more preferable solution is provided for the clustered control mode of multi-machine collaborative, this scheme integrates because loading functionality is single
Spend low, dismantle in actual use, change cumbersome, operability is weak.
Chinese Patent Application No. discloses a kind of unmanned plane load universal interface system, the nothing for 201410233637.5
Man-machine load universal interface system, there is provided a set of software and hardware specification, can make various types of user equipmenies and unmanned plane without
Link together seam, share the resource of unmanned plane, such as flying quality, communication data chain, energy resource supply.With prior art phase
Than this invention simplifies designing and developing for UAV flight's equipment, improving the resource utilization and work of unmanned plane during flying system
Make efficiency.The present invention also substantially increases the information content of loading device simultaneously, is set for the load of further Development of Novel function
It is standby to have established solid foundation.The present invention uses the data bus interface of industrial standard, reduces the development cost of loading device,
By this interface, unmanned plane during flying platform abstraction can not can known about nobody by developer into data object, loading device
On the basis of the details of machine flying platform, the New function of unmanned vehicle is realized.The interface system of this scheme does not supply accordingly
Electric module and load install module, and the low installation of integrated level is inconvenient.
The content of the invention
It is an object of the invention to provide a kind of unmanned plane multifunctional service Towed bird system, to solve to cause in the prior art
Above-mentioned multinomial defect.
A kind of unmanned plane multifunctional service Towed bird system, including airflight plateform system and ground control centre system,
Connected between the airflight plateform system and ground control centre system by radio communication, the control flying platform system
System includes unmanned vehicle flight control system, intelligent load universal interface system and loading device, and the intelligent load is general
Interface system one end is connected in unmanned vehicle flight control system, and one end is connected on loading device, and the intelligent load is led to
Include remote sensing load installation module, remote sensing load power supply module and interface message configuration module, the ground control with interface system
Centring system processed is provided with floor synthetic command and control system, the floor synthetic command and control system include flight control modules,
Link control module, load control module and flight tracking control module.
Preferably, the loading device also can perform control by remote control remote control by ground control centre system.
Preferably, the flight control modules are used for the monitoring of flying quality, instruction transmission and data processing etc..
Preferably, the link control module is used for link management, frame synchronization, flow control and Error Control, and by number
Separated according to control information, transparent transmission and addressing.
Preferably, the load control module is used to send load control instruction, obtains the sensing data of load.
Preferably, the flight tracking control module makes space shuttle be flown by prebriefed pattern, and realization is automatically flown automatic
Control.
Preferably, the remote sensing load installation module is used to install different remote sensing load, the installation of the remote sensing load
Mode is fast-assembling screw-fashion.
Preferably, the remote sensing load power supply end module is provided needed for a variety of loading devices such as 5 volts, 9 volts, 12 volts and 14 volts
The voltage wanted.
Preferably, the interface message configuration module is used to tell characteristic possessed by different loading devices, specifically
Including the voltage required for loading device, control method, information transmission and image procossing etc..
The advantage of the invention is that：Technical scheme sustained load quick-replaceable, unmanned plane can autonomous classification loads
Lotus type, produced and contacted by intelligent load universal interface system between flight control system and loading device, realization passes through course line
The control load operation of the mode remote independent of planning, reduces operating personnel's quantity required during unmanned machine operation, and compatibility is appointed
The business original function of load, intensive tasks flexibility, device use unified communication interface, and all load are designed to fast-assembling rotation
The mode of twisting, the inconvenience of outside cabling is reduced, securely and reliably, whether flight control system detection loading device function is normal before work, if
Self-test is abnormal, will send alarm, reminds assisting user inspection to fix a breakdown, before flight, flight control system will be according to load
Lotus type, amendment center of gravity, control parameter make that posture that aircraft is overall and operating process are more stable reliable, and unmanned plane gondola can
Carrying equipment enriches, and meets various application scenarios, a tractor serves several purposes, can greatly improve the stability of aircraft, for inspection, rescue
Help, early warning tries to gain time precious to one, lifted operating efficiency, unmanned aerial vehicle remote sensing load universal intelligent interface platform, which possesses, quickly to be changed
Function, the power supply of built-in high-quality, communication interface, different loads only need easy configuration, simple to operate, intelligence degree
It is high.
Brief description of the drawings
Fig. 1 is airflight plateform system schematic diagram of the present invention.
Fig. 2 is ground control centre systematic schematic diagram of the present invention.
Embodiment 1
To be easy to understand the technical means, the inventive features, the objects and the advantages of the present invention, with reference to
Embodiment, the present invention is expanded on further.
As shown in Figure 1 to Figure 2, a kind of unmanned plane multifunctional service Towed bird system, including airflight plateform system and ground
Face control centre system, connected between the airflight plateform system and ground control centre system by radio communication, institute
Stating control flying platform system includes unmanned vehicle flight control system, intelligent load universal interface system and loading device, institute
Intelligent load universal interface system one end to be stated to be connected in unmanned vehicle flight control system, one end is connected on loading device,
The intelligent load universal interface system includes remote sensing load installation module, remote sensing load power supply module and interface message configuration
Module, the ground control centre system are provided with floor synthetic command and control system, the floor synthetic command and control system bag
Flight control modules, link control module, load control module and flight tracking control module are included, loading device is connected to intelligent load
With flight control system handshake communication on lotus universal interface system, flight control system obtains initialization default setting, and bristles with anger to earth station
Order, ground control centre system automatic spring respective loads control menu, different load have default communication code, fly control system
As long as system can note load information, including weight, center of gravity, windage, interface plug number (longevity after reading corresponding communication code
Life limit is a definite value, has reached and has suggested that replacing), flight control system reads autonomous amendment flight parameter after information coding, chooses
Optimal flight configuration, and gradually optimize own adaptation parameter, power output value and distribution ability, lifting system electric stability,
Increase seismic stability.
In the present embodiment, the loading device can also be held by remote control remote control by ground control centre system
Row control.
In the present embodiment, the flight control modules are used for the monitoring of flying quality, instruction transmission and data processing etc..
In the present embodiment, the link control module is used for link management, frame synchronization, flow control and Error Control,
And data and control information is separated, transparent transmission and addressing.
In the present embodiment, the load control module is used to send load control instruction, obtains the sensor number of load
According to.
In the present embodiment, the flight tracking control module makes space shuttle be flown by prebriefed pattern, realizes full-automatic flight
Automatically control.
Embodiment 2
To be easy to understand the technical means, the inventive features, the objects and the advantages of the present invention, with reference to
Embodiment, the present invention is expanded on further.
A kind of unmanned plane multifunctional service Towed bird system, including airflight plateform system and ground control centre system,
Connected between the airflight plateform system and ground control centre system by radio communication, the control flying platform system
System includes unmanned vehicle flight control system, intelligent load universal interface system and loading device, and the intelligent load is general
Interface system one end is connected in unmanned vehicle flight control system, and one end is connected on loading device, and the intelligent load is led to
Include remote sensing load installation module, remote sensing load power supply module and interface message configuration module, the ground control with interface system
Centring system processed is provided with floor synthetic command and control system, the floor synthetic command and control system include flight control modules,
Link control module, load control module and flight tracking control module.
In the present embodiment, the remote sensing load installation module is used to install different remote sensing load, the remote sensing load
Mounting means be fast-assembling screw-fashion, integrated level height is easy to the dismounting and replacing of remote sensing load.
In the present embodiment, the remote sensing load power supply end module provides a variety of load such as 5 volts, 9 volts, 12 volts and 14 volts and set
Standby required voltage.
In addition, the interface message configuration module is used to tell characteristic possessed by different loading devices, specific bag
Include voltage, control method, information transmission and image procossing required for loading device etc..
As known by the technical knowledge, the present invention can pass through the embodiment party of other essence without departing from its spirit or essential feature
Case is realized.Therefore, embodiment disclosed above, for each side, all it is merely illustrative, is not only.Institute
Have within the scope of the present invention or be included in the invention in the change being equal in the scope of the present invention.
Claims (9)
1. a kind of unmanned plane multifunctional service Towed bird system, it is characterised in that controlled including airflight plateform system and ground
Centring system, connected between the airflight plateform system and ground control centre system by radio communication, the control
Flying platform system includes unmanned vehicle flight control system, intelligent load universal interface system and loading device, the intelligence
Change load universal interface system one end to be connected in unmanned vehicle flight control system, one end is connected on loading device, the intelligence
Load universal interface system, which can be changed, includes remote sensing load installation module, remote sensing load power supply module and interface message configuration module,
The ground control centre system is provided with floor synthetic command and control system, and the floor synthetic command and control system includes flight
Control module, link control module, load control module and flight tracking control module.
A kind of 2. unmanned plane multifunctional service Towed bird system according to claim 1, it is characterised in that：The loading device
Control also can be performed by ground control centre system by remote control remote control.
A kind of 3. unmanned plane multifunctional service Towed bird system according to claim 1, it is characterised in that：The flight control
Module is used for the monitoring of flying quality, instruction transmission and data processing etc..
A kind of 4. unmanned plane multifunctional service Towed bird system according to claim 1, it is characterised in that：The link control
Module is used for link management, frame synchronization, flow control and Error Control, and data and control information is separated, transparent transmission and
Addressing.
A kind of 5. unmanned plane multifunctional service Towed bird system according to claim 1, it is characterised in that：The load control
Module is used to send load control instruction, obtains the sensing data of load.
A kind of 6. unmanned plane multifunctional service Towed bird system according to claim 1, it is characterised in that：The flight tracking control
Module makes space shuttle be flown by prebriefed pattern, realizes that automatically flies automatically controls.
A kind of 7. unmanned plane multifunctional service Towed bird system according to claim 1, it is characterised in that：The remote sensing load
Installation module is used to install different remote sensing load, and the mounting means of the remote sensing load is fast-assembling screw-fashion.
A kind of 8. unmanned plane multifunctional service Towed bird system according to claim 1, it is characterised in that：The remote sensing load
End module of powering provides the voltage required for a variety of loading devices such as 5 volts, 9 volts, 12 volts and 14 volts.
A kind of 9. unmanned plane multifunctional service Towed bird system according to claim 1, it is characterised in that：The interface message
Configuration module be used to telling different loading devices possessed by characteristic, specifically include voltage required for loading device, control
Method, information transmission and image procossing processed etc..
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710704409.5A CN107422742A (en) | 2017-08-16 | 2017-08-16 | A kind of unmanned plane multifunctional service Towed bird system |
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| CN201710704409.5A CN107422742A (en) | 2017-08-16 | 2017-08-16 | A kind of unmanned plane multifunctional service Towed bird system |
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| CN201710704409.5A Pending CN107422742A (en) | 2017-08-16 | 2017-08-16 | A kind of unmanned plane multifunctional service Towed bird system |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112193426A (en) * | 2020-09-11 | 2021-01-08 | 中国航空工业集团公司成都飞机设计研究所 | Quick integration method for realizing plug and play of task load |
| CN113341775A (en) * | 2021-06-02 | 2021-09-03 | 天津云圣智能科技有限责任公司 | Pod dispatching method, device and system |
| CN114490500A (en) * | 2021-12-29 | 2022-05-13 | 西北工业大学 | Comprehensive intelligent flight control computing platform for smart application |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103274046A (en) * | 2013-04-28 | 2013-09-04 | 唐粮 | Modularized pilotless helicopter for task loads |
| CN104724295A (en) * | 2014-05-30 | 2015-06-24 | 广州安云电子科技有限公司 | Universal interface system for unmanned aerial vehicle loads |
| CN204790572U (en) * | 2015-01-13 | 2015-11-18 | 青岛海山海洋装备有限公司 | General lift -launch system of unmanned submerge ware AUV's load under water |
| CN105137755A (en) * | 2015-08-27 | 2015-12-09 | 成都飞机工业（集团）有限责任公司 | Unmanned air vehicle mission load self-adaptive distribution method |
| CN205738124U (en) * | 2016-05-12 | 2016-11-30 | 普宙飞行器科技（深圳）有限公司 | One is conveniently replaceable load device and unmanned plane |
| CN107024937A (en) * | 2017-03-13 | 2017-08-08 | 武汉飞流智能技术有限公司 | The self-identifying of unmanned plane load and parameter Self Matching method and ground Adaptable System |
-
2017
- 2017-08-16 CN CN201710704409.5A patent/CN107422742A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103274046A (en) * | 2013-04-28 | 2013-09-04 | 唐粮 | Modularized pilotless helicopter for task loads |
| CN104724295A (en) * | 2014-05-30 | 2015-06-24 | 广州安云电子科技有限公司 | Universal interface system for unmanned aerial vehicle loads |
| CN204790572U (en) * | 2015-01-13 | 2015-11-18 | 青岛海山海洋装备有限公司 | General lift -launch system of unmanned submerge ware AUV's load under water |
| CN105137755A (en) * | 2015-08-27 | 2015-12-09 | 成都飞机工业（集团）有限责任公司 | Unmanned air vehicle mission load self-adaptive distribution method |
| CN205738124U (en) * | 2016-05-12 | 2016-11-30 | 普宙飞行器科技（深圳）有限公司 | One is conveniently replaceable load device and unmanned plane |
| CN107024937A (en) * | 2017-03-13 | 2017-08-08 | 武汉飞流智能技术有限公司 | The self-identifying of unmanned plane load and parameter Self Matching method and ground Adaptable System |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112193426A (en) * | 2020-09-11 | 2021-01-08 | 中国航空工业集团公司成都飞机设计研究所 | Quick integration method for realizing plug and play of task load |
| CN112193426B (en) * | 2020-09-11 | 2023-05-26 | 中国航空工业集团公司成都飞机设计研究所 | Quick integration method for realizing plug-and-play of task load |
| CN113341775A (en) * | 2021-06-02 | 2021-09-03 | 天津云圣智能科技有限责任公司 | Pod dispatching method, device and system |
| CN114490500A (en) * | 2021-12-29 | 2022-05-13 | 西北工业大学 | Comprehensive intelligent flight control computing platform for smart application |
| CN114490500B (en) * | 2021-12-29 | 2024-03-08 | 西北工业大学 | Comprehensive intelligent flight control computing platform for general intelligent application |
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Application publication date: 20171201 |
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