CN108438211A - A kind of multiple no-manned plane system combining unmanned plane and combinations thereof formula - Google Patents
A kind of multiple no-manned plane system combining unmanned plane and combinations thereof formula Download PDFInfo
- Publication number
- CN108438211A CN108438211A CN201810204329.8A CN201810204329A CN108438211A CN 108438211 A CN108438211 A CN 108438211A CN 201810204329 A CN201810204329 A CN 201810204329A CN 108438211 A CN108438211 A CN 108438211A
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- China
- Prior art keywords
- module
- unmanned plane
- plane
- flight
- control
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- 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
- B64D47/00—Equipment not otherwise provided for
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- 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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- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
Abstract
The invention discloses a kind of multiple no-manned plane systems combining unmanned plane and combinations thereof formula, it is related to air vehicle technique field, including unmanned plane, the unmanned plane folds tripod, magnetic generating means and pantograph linkage mechanism equipped with electronic, the pantograph linkage mechanism is made of electric telescopic rod and lock, described to latch the output end for being fixedly mounted on electric telescopic rod；It can be needed to be freely combined and detach in the air according to scene using the unmanned plane of the structure, constitute knockdown multiple no-manned plane structure, form unmanned generator terminal, and constitute system with the control command centre end on ground, the process of combination and separation is remotely automatically controlled in real time by controlling command centre's end realization, manipulation is convenient, controllability is high, it can ensure the stabilized flight of knockdown multiple no-manned plane structure, it can give the unmanned plane installation of different sizes and shapes is identical can composite structure, applicability is high, can also meet the outdoor study demand of requirements at the higher level.
Description
Technical field
The present invention relates to air vehicle technique field, more particularly to a kind of multiple no-manned plane combining unmanned plane and combinations thereof formula
System.
Background technology
In recent years, unmanned air vehicle technique is quickly grown, and can be made by carrying mission payload such as fire extinguisher bomb, emergency article etc.
Multiple industries such as industry and being widely used in takes photo by plane, inspection, fire-fighting, investigation.However, the structure of a frame unmanned plane is fixed, take
The load weight of load is also fixed, if encountering heavy weight load, it is necessary to using the unmanned plane that can carry more heavy－duty, be needed
To select unmanned plane type, applicability small according to load weight.Application number 201710415296.7 discloses a kind of unmanned plane list
First and a kind of Combined unmanned machine, unmanned plane unit include motor, and motor includes rotor and stator, and main paddle is equipped on rotor
Leaf, around being circumferentially provided with several side wings in stator, multiple unmanned plane units by connecting bracket fixed Combination, every frame nobody
The size shape of machine is the same, and needs to complete combination before ground is taken off, and cannot achieve aerial intelligences combination, it is necessary to be determined in advance
Good number of combinations, application scenarios have limitation.
Invention content
The present invention provides a kind of multiple no-manned plane system combining unmanned plane and combinations thereof formula, is deposited for solving the prior art
Various defects.
To achieve the above object, the present invention provides technical solution below：One kind can combine unmanned plane, including unmanned plane,
The unmanned plane folds tripod, magnetic generating means and pantograph linkage mechanism equipped with electronic, and the pantograph linkage mechanism is by electronic
Telescopic rod and lock form, described to latch the output end for being fixedly mounted on electric telescopic rod.
A kind of knockdown multiple no-manned plane system, including unmanned generator terminal and command and control center end, the unmanned generator terminal are set
There are flight control modules, GPS positioning module, flight data recording module, control wireless transport module on switch and machine, it is described to fly
Row control module, GPS positioning module and flight data recording module are connect with wireless transport module on machine, the control switch
It is connect with flight control modules, the control command centre is equipped with control module, data analysis module and ground-based wireless transmissions mould
Block, the ground-based wireless transmissions module are connect with wireless transport module on machine, the data analysis module and ground-based wireless transmissions
Module connects, and is connect with control module, and the control module is connect with ground-based wireless transmissions module.
Preferably, Flight Condition Data of the flight data recording module for recording unmanned plane in real time.
Preferably, the GPS positioning module is used to be accurately positioned the real time position residing for unmanned plane in real time.
Preferably, the control switch is electrically connected with magnetic generating means.
It is using the advantageous effect of above technical scheme：The present invention provides a kind of unmanned plane and combinations thereof formulas of combining
Multiple no-manned plane system can need to be freely combined and detach in the air according to scene using the unmanned plane of the structure, constitute combination
The multiple no-manned plane structure of formula forms unmanned generator terminal, and constitutes system, the mistake of combination and separation with the control command centre end on ground
Journey is remotely automatically controlled in real time by controlling command centre's end realization, and manipulation is convenient, and controllability is high, can ensure knockdown more
The stabilized flight of unmanned plane structure, can give different sizes and shapes unmanned plane installation it is identical can composite structure, applicability
Height can also meet the outdoor study demand of requirements at the higher level.
Description of the drawings
Fig. 1 is the structural schematic diagram that can combine unmanned plane；
Fig. 2 is the system construction drawing of the system.
Specific implementation mode
Below against attached drawing, by the description of the embodiment, making to the specific implementation mode of the present invention further details of
Explanation, it is therefore an objective to those skilled in the art be helped to have more complete, accurate and deep reason to the design of the present invention, technical solution
Solution, and contribute to its implementation.
Fig. 1 and Fig. 2 shows the specific implementation mode of the present invention：One kind can combine unmanned plane, including unmanned plane, it is described nobody
Machine be equipped with it is electronic fold tripod, magnetic generating means and pantograph linkage mechanism, the pantograph linkage mechanism by electric telescopic rod and
Lock composition, it is described to latch the output end for being fixedly mounted on electric telescopic rod.
A kind of knockdown multiple no-manned plane system, including unmanned generator terminal and command and control center end, the unmanned generator terminal are set
There are flight control modules, GPS positioning module, flight data recording module, control wireless transport module on switch and machine, it is described to fly
Row control module, GPS positioning module and flight data recording module are connect with wireless transport module on machine, the control switch
It is connect with flight control modules, the control command centre is equipped with control module, data analysis module and ground-based wireless transmissions mould
Block, the ground-based wireless transmissions module are connect with wireless transport module on machine, the data analysis module and ground-based wireless transmissions
Module connects, and is connect with control module, and the control module is connect with ground-based wireless transmissions module.
Flight Condition Data of the flight data recording module for recording unmanned plane in real time；The GPS positioning module
Real time position for being accurately positioned in real time residing for unmanned plane；The control switch is electrically connected with magnetic generating means.
The principle of the present invention and its course of work：
Based on above-mentioned, the present invention is a kind of multiple no-manned plane system combining unmanned plane and combinations thereof formula, is pacified on unmanned plane
Electronic tripod, magnetic generating means and the pantograph linkage mechanism folded of dress is electrically connected with the flight control modules of unmanned plane
, in anabolic process, flight control modules control command is issued by controlling command centre end, electronic tripod is folded to realize
Automatically-retractable folding avoids generating obstacle in multiple unmanned plane anabolic processes, and the flight data recording module of multiple unmanned planes is real
The respective Flight Condition Datas of Shi Jilu, while the respective residing real-time position of the GPS positioning module Real-time Feedback of multiple unmanned planes
It sets, and Flight Condition Data information and location information are just transferred to ground-based wireless transmissions module by wireless transport module on machine, and
Data analysis module is further transmitted information to, data analysis module is analyzed the related data of unmanned plane, obtained in real time
Go out real-time analysis result, and structural transmission will be analyzed to control module, control module will be sent by ground-based wireless transmissions module
Command information, wireless transport module receives command information on machine, and passes to flight control modules, and corresponding unmanned plane reception refers to
Information is enabled, and the respective flight attitude of adjust automatically is docked in the air, control switch starts magnetic generating means, utilizes magnetism
Unmanned plane is promoted to concentrate docking, the electric telescopic rod of unmanned plane stretches out, carries out blocking fixation by respective lock, to multiple
Unmanned plane constitutes a knockdown entirety, be used as medium, realization signal by controlling command centre end between multiple unmanned planes
Between intercommunication, ensure the consistency of state of flight, the unmanned plane after combination will meet more job requirements, detach
Journey after retracting electric telescopic rod, realizes the releasing of lock, to sum up institute by controlling the flight attitude of each unmanned plane
State, can be needed to be freely combined and detach in the air according to scene using the unmanned plane of the structure, constitute it is knockdown mostly nobody
Machine structure forms unmanned generator terminal, and constitutes system with the control command centre end on ground, and combination and the process detached pass through control
Command centre end realizes and remotely automatically controls in real time that manipulation is convenient, and controllability is high, can ensure knockdown multiple no-manned plane structure
Stabilized flight, can give the unmanned plane installation of different sizes and shapes it is identical can composite structure, applicability is high, can also meet
The outdoor study demand of requirements at the higher level.
The present invention is exemplarily described above in association with attached drawing, it is clear that the present invention implements not by above-mentioned side
The limitation of formula, as long as using the improvement of the various unsubstantialities of inventive concept and technical scheme of the present invention progress；Or not
It is improved, the above-mentioned design of the present invention and technical solution are directly applied into other occasions, in protection scope of the present invention
Within.
Claims (5)
1. one kind can combine unmanned plane, it is characterised in that：Including unmanned plane, the unmanned plane folds tripod, magnetism equipped with electronic
Generating means and pantograph linkage mechanism, the pantograph linkage mechanism are made of electric telescopic rod and lock, the fixed peace of the lock
Mounted in the output end of electric telescopic rod.
2. a kind of knockdown multiple no-manned plane system a kind of as defined in claim 1, it is characterised in that：Including unmanned plane
End and command and control center end, the unmanned generator terminal be equipped with flight control modules, GPS positioning module, flight data recording module,
Control switch and machine on wireless transport module, the flight control modules, GPS positioning module and flight data recording module with
Wireless transport module connects on machine, and the control switch is connect with flight control modules, and the control command centre is equipped with control
Module, data analysis module and ground-based wireless transmissions module, the ground-based wireless transmissions module connect with wireless transport module on machine
It connects, the data analysis module is connect with ground-based wireless transmissions module, and is connect with control module, the control module and ground
Wireless transport module connects.
3. a kind of knockdown multiple no-manned plane system according to claim 2, it is characterised in that：The flight data recording
Flight Condition Data of the module for recording unmanned plane in real time.
4. a kind of knockdown multiple no-manned plane system according to claim 2, it is characterised in that：The GPS positioning module
Real time position for being accurately positioned in real time residing for unmanned plane.
5. a kind of knockdown multiple no-manned plane system according to claim 2, it is characterised in that：The control switch and magnetic
Property generating means be electrically connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810204329.8A CN108438211A (en) | 2018-03-13 | 2018-03-13 | A kind of multiple no-manned plane system combining unmanned plane and combinations thereof formula |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810204329.8A CN108438211A (en) | 2018-03-13 | 2018-03-13 | A kind of multiple no-manned plane system combining unmanned plane and combinations thereof formula |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108438211A true CN108438211A (en) | 2018-08-24 |
Family
ID=63194854
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810204329.8A Pending CN108438211A (en) | 2018-03-13 | 2018-03-13 | A kind of multiple no-manned plane system combining unmanned plane and combinations thereof formula |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111766894A (en) * | 2020-03-25 | 2020-10-13 | 湖南大学 | Modularized variable unmanned aerial vehicle system and delivery method thereof |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205524962U (en) * | 2016-03-30 | 2016-08-31 | 深圳市高巨创新科技开发有限公司 | Modular unmanned aerial vehicle |
| CN106114837A (en) * | 2016-07-21 | 2016-11-16 | 上海宝冶集团有限公司 | Parallel unmanned plane is used in a kind of building pipe fitting transport |
| CN106394865A (en) * | 2016-08-30 | 2017-02-15 | 上海交通大学 | Separable type double multi-rotor unmanned aircrafts |
| CN107472521A (en) * | 2017-06-22 | 2017-12-15 | 深圳大学 | The control method of more rotor flying platforms and more rotor flying platforms |
-
2018
- 2018-03-13 CN CN201810204329.8A patent/CN108438211A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205524962U (en) * | 2016-03-30 | 2016-08-31 | 深圳市高巨创新科技开发有限公司 | Modular unmanned aerial vehicle |
| CN106114837A (en) * | 2016-07-21 | 2016-11-16 | 上海宝冶集团有限公司 | Parallel unmanned plane is used in a kind of building pipe fitting transport |
| CN106394865A (en) * | 2016-08-30 | 2017-02-15 | 上海交通大学 | Separable type double multi-rotor unmanned aircrafts |
| CN107472521A (en) * | 2017-06-22 | 2017-12-15 | 深圳大学 | The control method of more rotor flying platforms and more rotor flying platforms |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111766894A (en) * | 2020-03-25 | 2020-10-13 | 湖南大学 | Modularized variable unmanned aerial vehicle system and delivery method thereof |
| CN111766894B (en) * | 2020-03-25 | 2023-01-31 | 湖南大学 | Modularized variable unmanned aerial vehicle system and delivery method thereof |
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| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180824 |