CN107826261A - A kind of multifunctional single rotor wing unmanned aerial vehicle control platform - Google Patents
A kind of multifunctional single rotor wing unmanned aerial vehicle control platform Download PDFInfo
- Publication number
- CN107826261A CN107826261A CN201710951015.XA CN201710951015A CN107826261A CN 107826261 A CN107826261 A CN 107826261A CN 201710951015 A CN201710951015 A CN 201710951015A CN 107826261 A CN107826261 A CN 107826261A
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- control platform
- main body
- key
- aerial vehicle
- unmanned aerial
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- 238000003780 insertion Methods 0.000 claims abstract description 13
- 230000037431 insertion Effects 0.000 claims abstract description 13
- 238000012545 processing Methods 0.000 claims abstract description 13
- 239000004973 liquid crystal related substance Substances 0.000 claims description 28
- 238000004026 adhesive bonding Methods 0.000 claims 1
- 238000003466 welding Methods 0.000 claims 1
- 230000005540 biological transmission Effects 0.000 abstract description 4
- 238000012423 maintenance Methods 0.000 abstract description 2
- 238000000034 method Methods 0.000 abstract description 2
- 230000008569 process Effects 0.000 abstract description 2
- 210000002683 foot Anatomy 0.000 description 7
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- 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)
- Mechanical Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of multifunctional single rotor wing unmanned aerial vehicle control platform,Including control platform main body,The right-hand member of the upside of the control platform main body is provided with order and performs key,And the order performs key insertion and is arranged in control platform main body,The rear side that the order performs the left end of key is provided with speed lifting key and power switch,And the speed lifting key and power switch are electrically connected with control platform main body,And lifted provided with speed lifting key to carry out the speed of unmanned plane,Be advantageous to the stabilized flight of unmanned plane,And key is performed to perform unmanned plane during flying task using order,Add unmanned aerial vehicle (UAV) control platform feature,And carry out the takeoff and landing of unmanned plane with landing expansion plate,Be advantageous to the permanent operation of unmanned plane,With this come keep flight and controllability,Processing and transmission come signal is carried out by wireless receiving instrument,And in the process maintenance data processing unit come prevent the external world interference,And encryption performance is strong.
Description
Technical field
The present invention relates to unmanned aerial vehicle (UAV) control platform technology field, specially a kind of multifunctional single rotor wing unmanned aerial vehicle control is flat
Platform.
Background technology
Nowadays more by the way of speed control, the residual non-uniformity for estimating unmanned plane by averaged power spectrum algorithm is averaged
Value, and then the velocity amplitude that unmanned plane should currently adjust is calculated, change itself speed by unmanned plane, realize and reached simultaneously
Go in 20 years, Unmanned Aerial Vehicle in the air, monitoring, play key in communication rescue and numerous application fields such as take photo by plane
Role, in China, due to lacking advanced unmanned plane (UAV) spray application and control device, gap is larger compared with external,
It is always a blank so as to cause China to carry out farm-forestry crop spraying using unmanned plane (UAV), is carried out in rescue and relief work dangerous
The feedback of situation is to organize to rescue;For media, real-time news report and remote interview can be carried out, should for individual
With, can be used for being taken photo in the sky and remote control distributor, it is very extensive in the application of military aspect, have it is simple in construction, use
Convenient, the features such as operation cost is low, flight precision is high and is easy to intellectuality.
Current single rotor wing unmanned aerial vehicle control platform, is almost only used for the flight of unmanned plane, function is single, and does not have
There is unmanned plane landing platform, easily cause the damage of unmanned plane, while control platform volume is larger is unfavorable for carrying, and reduces control
The utilization rate of platform processed, the processing of signal and transmission are easily interfered, and encryption performance is poor, will not nobody is straight as current
The machine of liter and four rotor wing unmanned aerial vehicles equally flexibly and easily operate.
So how to design a kind of multifunctional single rotor wing unmanned aerial vehicle control platform, turning into us will currently solve the problems, such as.
The content of the invention
It is an object of the invention to provide a kind of multifunctional single rotor wing unmanned aerial vehicle control platform, to solve above-mentioned background technology
The middle flight for proposing almost to be only used for unmanned plane, function is single, and does not have unmanned plane landing platform, easily causes nobody
The damage of machine, while control platform volume is larger is unfavorable for carrying, the problem of reducing the utilization rate of control platform.
To achieve the above object, the present invention provides following technical scheme：A kind of multifunctional single rotor wing unmanned aerial vehicle control platform,
Including control platform main body, the right-hand member of the upside of the control platform main body is provided with order and performs key, and the order performs
Key insertion is arranged in control platform main body, and the rear side that the order performs the left end of key is opened provided with speed lifting key and power supply
Close, and speed lifting key and power switch are electrically connected with control platform main body, the front end of the control platform main body
Wireless receiving instrument is provided with, and the control platform main body is fixedly connected with wireless receiving instrument, the left end of the wireless receiving instrument
Provided with locking groove, and the locking groove insertion is arranged in control platform main body, and the upper left side of the locking groove is set
There is direction control lever, and the direction control lever is connected with control platform subject activity, the rear side of the control platform main body
Upper end is connected with liquid crystal display, and data processing equipment, and the liquid crystal are provided with the right side of the liquid crystal display
Show that device is electrically connected with data processing equipment, the upside of the liquid crystal display is provided with indicator lamp and locker, and the instruction
Lamp insertion is arranged in liquid crystal display, and the back of the liquid crystal display is provided with meteorological detector, and the liquid crystal display
Device is fixedly connected with meteorological detector, and the positive front end of the meteorological detector is bonded with information connector, described information connector
The center of front end be provided with sensor, and described information connector is connected with sensor signal, the control platform main body
One end be provided with landing expansion plate, the left end of the landing expansion plate is fixed with coprocessor, and the rear side of institute's coprocessor is set
There is adjuster, and the adjuster is flexibly connected with landing expansion plate.
Further, the center of the upper surface of the speed lifting key is provided with solar panel, and sun electricity
Pond plate insertion is arranged in control platform main body.
Further, the lower right side of the liquid crystal display is provided with carrier, and the liquid crystal display and carrier
It is flexibly connected.
Further, the back of the landing expansion plate is provided with inclined plate, and the landing expansion plate and inclined plate weld.
Further, the upper end of described information connector is provided with memory card, and described information connector and memory card electricity
Property connection.
Further, the bottom that the order performs key is provided with waterproof foot pad, and the waterproof foot pad and control platform master
Body passes through strength glue bond.
Further, USB interface is provided with the right side of the control platform main body, and the USB interface is opened on control
In main platform body.
Compared with prior art, the beneficial effects of the invention are as follows：This kind of multifunctional single rotor wing unmanned aerial vehicle control platform, passes through
Improvement to control platform main body, and lifted provided with speed lifting key to carry out the speed of unmanned plane, be advantageous to the steady of unmanned plane
Fixed flight, and key is performed to perform unmanned plane during flying task using order, unmanned aerial vehicle (UAV) control platform feature is added, and transport
The takeoff and landing of unmanned plane is carried out with landing expansion plate, be advantageous to the permanent operation of unmanned plane, keep flying with this
And controllability, the processing and transmission come signal are carried out by wireless receiving instrument, and maintenance data processing unit is come in the process
The interference in the external world is prevented, and encryption performance is strong, and utilization orientation control-rod carries out the flexible operating of unmanned plane, and using taking
Band device carries to be controlled main platform body, improves the utilization rate of control platform main body, is easy to promote the use of.
Brief description of the drawings
Fig. 1 is the overall structure diagram of the present invention；
Fig. 2 is the partial structural diagram of present invention landing expansion plate；
Fig. 3 is the partial structural diagram of the meteorological detector of the present invention；
In figure：1- control platform main bodys；2- waterproof foots pad；3-USB interfaces；4- orders perform key；5- speed lifts key；6- power supplys
Switch；7- solar panels；8- liquid crystal displays；9- indicator lamps；10- data processing equipments；11- carriers；12- direction controllings
Bar；13- wireless receiving instrument；14- locks groove；15- lockers；16- landing expansion plates；17- coprocessors；18- adjusters；
19- inclined plates；20- meteorology detectors；21- information connectors；22- sensors；23- memory cards.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made
Embodiment, belong to the scope of protection of the invention.
Fig. 1-3 are referred to, the present invention provides technical scheme：A kind of multifunctional single rotor wing unmanned aerial vehicle control platform, including control
Main platform body 1 processed, the right-hand member of the upside of the control platform main body 1 is provided with order and performs key 4, and the order performs key 4
Insertion is arranged in control platform main body 1, and the rear side that the order performs the left end of key 4 is opened provided with speed lifting key 5 and power supply
6 are closed, and speed lifting key 5 and power switch 6 are electrically connected with control platform main body 1, the control platform main body 1
Front end is provided with wireless receiving instrument 13, and the control platform main body 1 is fixedly connected with wireless receiving instrument 13, the wireless receiving
The left end of instrument 13 is provided with locking groove 14, and locking groove 14 insertion is arranged in control platform main body 1, and the locking is recessed
The upper left side of groove 14 is provided with direction control lever 12, and the direction control lever 12 is flexibly connected with control platform main body 1, described
The upper end of the rear side of control platform main body 1 is connected with liquid crystal display 8, and the right side of the liquid crystal display 8 is provided with number
According to processing unit 10, and the liquid crystal display 8 is electrically connected with data processing equipment 10, the upside of the liquid crystal display 8
Provided with indicator lamp 9 and locker 15, and the insertion of the indicator lamp 9 is arranged in liquid crystal display 8, the liquid crystal display 8
Back is provided with meteorological detector 20, and the liquid crystal display 8 is fixedly connected with meteorological detector 20, the meteorological detector
20 positive front end is bonded with information connector 21, and the center of the front end of described information connector 21 is provided with sensor 22, and
Described information connector 21 is connected with the signal of sensor 22, and one end of the control platform main body 1 is provided with landing expansion plate 16, institute
The left end for stating landing expansion plate 16 is fixed with coprocessor 17, and the rear side of institute's coprocessor 17 is provided with adjuster 18, and described
Adjuster 18 is flexibly connected with landing expansion plate 16.
Further, the center of the upper surface of the speed lifting key 5 is provided with solar panel 7, and the sun
The insertion of cell panel 7 is arranged in control platform main body 1, carries out absorption solar energy by solar panel 7, and be supplied to control
Main platform body 1 uses.
Further, the lower right side of the liquid crystal display 8 is provided with carrier 11, and the liquid crystal display 8 is with taking
Band device 11 is flexibly connected, and the carrying of main platform body 1 is controlled by carrier 11, is advantageous to making for control platform main body 1
With rate.
Further, the back of the landing expansion plate 16 is provided with inclined plate 19, and the landing expansion plate 16 and inclined
Plate 19 is welded, and the safe falling of unmanned plane is carried out by using inclined plate 19, and with easy to use, simple to operate, peace
The advantages that overall height is imitated.
Further, the upper end of described information connector 21 is provided with memory card 23, and described information connector 21 and storage
The electric connection of card 23 is deposited, the information of control platform main body 1 is stored using memory card 23, avoids the loss of information.
Further, the bottom that the order performs key 4 is provided with waterproof foot pad 2, and the waterproof foot pad 2 and control platform
Main body 1 carries out waterproof using waterproof foot pad 2, improves the practicality of control platform main body 1 by strength glue bond.
Further, the right side of the control platform main body 1 is provided with USB interface 3, and the USB interface 3 is opened on control
In main platform body 1 processed, information transmission is carried out by USB interface 3, battalion's cost is low, flight precision is high and it is intelligent to be easy to.
Operation principle：This kind of multifunctional single rotor wing unmanned aerial vehicle control platform, first, control platform main body 1 is placed in suitable
The place of conjunction, by waterproof foot pad 2 come prevent water enter unmanned aerial vehicle (UAV) control platform in, while will landing expansion plate 16 be placed on it is flat
Steady place, and by power switch 6, then to carry out taking off for unmanned plane, unmanned plane is now carried out by direction control lever 12
Heading freely controls, and then absorbs solar energy using solar panel 7, and be supplied to unmanned aerial vehicle (UAV) control platform to make
With, secondly by with speed lifting key 5 come carry out the speed of unmanned plane lifting, by wireless receiving instrument 13 come enter row information pass
Send, meteorological detection is carried out using meteorological detector 20, ensure that unmanned plane is flown in meteorological good premise, then using order
Key 4 is performed to perform unmanned plane during flying task, main platform body 1 and sensor are controlled followed by information connector 21
22 connections, are advantageous to the processing of information, the storage of flight information are carried out by memory card 23, finally, pass through the expansion plate that lands
16 and inclined plate 19 to carry out unmanned plane safe falling, while carry out the coordination of unmanned plane landing using coprocessor 17, and
The length adjustment of expansion plate 16 of landing is carried out using adjuster 18, carries out reminding staff's control platform by indicator lamp 9
The operation conditions of main body 1, locker 15 is embedded in locking groove 14, is advantageous to the protection of control platform main body 1.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of changes, modification can be carried out to these embodiments, replace without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (7)
1. a kind of multifunctional single rotor wing unmanned aerial vehicle control platform, including control platform main body（1）, it is characterised in that：The control
Main platform body（1）Upside right-hand member be provided with order perform key（4）, and the order performs key（4）Insertion is arranged at control
Main platform body（1）In, the order performs key（4）Left end rear side be provided with speed lifting key（5）And power switch（6）, and
The speed lifts key（5）And power switch（6）With control platform main body（1）It is electrically connected with, the control platform main body（1）
Front end be provided with wireless receiving instrument（13）, and the control platform main body（1）With wireless receiving instrument（13）It is fixedly connected, it is described
Wireless receiving instrument（13）Left end be provided with locking groove（14）, and the locking groove（14）Insertion is arranged at control platform main body
（1）In, the locking groove（14）Upper left side be provided with direction control lever（12）, and the direction control lever（12）With control
Main platform body（1）It is flexibly connected, the control platform main body（1）The upper end of rear side be connected with liquid crystal display（8）, institute
State liquid crystal display（8）Right side data processing equipment is installed（10）, and the liquid crystal display（8）With data processing equipment
（10）It is electrically connected with, the liquid crystal display（8）Upside be provided with indicator lamp（9）And locker（15）, and the indicator lamp（9）
Insertion is arranged at liquid crystal display（8）In, the liquid crystal display（8）Back be provided with meteorological detector（20）, and it is described
Liquid crystal display（8）With meteorological detector（20）It is fixedly connected, the meteorological detector（20）Positive front end be bonded with information company
Connect device（21）, described information connector（21）The center of front end be provided with sensor（22）, and described information connector
（21）With sensor（22）Signal connects, the control platform main body（1）One end be provided with landing expansion plate（16）, the landing
Expansion plate（16）Left end be fixed with coprocessor（17）, institute's coprocessor（17）Rear side be provided with adjuster（18）, and institute
State adjuster（18）With the expansion plate that lands（16）It is flexibly connected.
A kind of 2. multifunctional single rotor wing unmanned aerial vehicle control platform according to claim 1, it is characterised in that：The speed carries
Rise key（5）The center of upper surface be provided with solar panel（7）, and the solar panel（7）Insertion is arranged at control
Main platform body（1）In.
A kind of 3. multifunctional single rotor wing unmanned aerial vehicle control platform according to claim 1, it is characterised in that：The liquid crystal
Show device（8）Lower right side be provided with carrier（11）, and the liquid crystal display（8）With carrier（11）It is flexibly connected.
A kind of 4. multifunctional single rotor wing unmanned aerial vehicle control platform according to claim 1, it is characterised in that：The landing is stretched
Contracting plate（16）Back be provided with inclined plate（19）, and the landing expansion plate（16）With inclined plate（19）Welding.
A kind of 5. multifunctional single rotor wing unmanned aerial vehicle control platform according to claim 1, it is characterised in that：Described information connects
Connect device（21）Upper end be provided with memory card（23）, and described information connector（21）With memory card（23）It is electrically connected with.
A kind of 6. multifunctional single rotor wing unmanned aerial vehicle control platform according to claim 1, it is characterised in that：The order is held
Line unit（4）Bottom be provided with waterproof foot pad（2）, and the waterproof foot pad（2）With control platform main body（1）It is gluing by strength
Close.
A kind of 7. multifunctional single rotor wing unmanned aerial vehicle control platform according to claim 1, it is characterised in that：The control is flat
Platform main body（1）Right side be provided with USB interface（3）, and the USB interface（3）It is opened on control platform main body（1）In.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710951015.XA CN107826261A (en) | 2017-10-13 | 2017-10-13 | A kind of multifunctional single rotor wing unmanned aerial vehicle control platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710951015.XA CN107826261A (en) | 2017-10-13 | 2017-10-13 | A kind of multifunctional single rotor wing unmanned aerial vehicle control platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107826261A true CN107826261A (en) | 2018-03-23 |
Family
ID=61647954
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710951015.XA Pending CN107826261A (en) | 2017-10-13 | 2017-10-13 | A kind of multifunctional single rotor wing unmanned aerial vehicle control platform |
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|---|---|---|---|---|
| CN203845022U (en) * | 2014-04-28 | 2014-09-24 | 赵子滨 | Automation platform for providing service for routing inspection unmanned plane |
| CN204173164U (en) * | 2014-09-19 | 2015-02-25 | 南京海格专用车技术有限公司 | Unmanned aerial vehicle remote sensing surveillance and monitoring mobile platform dedicated operations seat |
| CN104386258A (en) * | 2014-08-20 | 2015-03-04 | 华南农业大学 | Feeding platform and feeding method suitable for field operation feeding for agricultural unmanned aerial vehicle |
| CN105416515A (en) * | 2015-12-07 | 2016-03-23 | 武汉理工大学 | Carrying device for quad-rotor unmanned aerial vehicle |
| CN205624081U (en) * | 2016-05-12 | 2016-10-12 | 江西兴航智控航空工业有限公司 | Automatic unmanned aerial vehicle remote controller of spraying insecticide |
| CN205787907U (en) * | 2016-05-23 | 2016-12-07 | 西安天成益邦电子科技有限公司 | A kind of unmanned aerial vehicle controls work station |
-
2017
- 2017-10-13 CN CN201710951015.XA patent/CN107826261A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203845022U (en) * | 2014-04-28 | 2014-09-24 | 赵子滨 | Automation platform for providing service for routing inspection unmanned plane |
| CN104386258A (en) * | 2014-08-20 | 2015-03-04 | 华南农业大学 | Feeding platform and feeding method suitable for field operation feeding for agricultural unmanned aerial vehicle |
| CN204173164U (en) * | 2014-09-19 | 2015-02-25 | 南京海格专用车技术有限公司 | Unmanned aerial vehicle remote sensing surveillance and monitoring mobile platform dedicated operations seat |
| CN105416515A (en) * | 2015-12-07 | 2016-03-23 | 武汉理工大学 | Carrying device for quad-rotor unmanned aerial vehicle |
| CN205624081U (en) * | 2016-05-12 | 2016-10-12 | 江西兴航智控航空工业有限公司 | Automatic unmanned aerial vehicle remote controller of spraying insecticide |
| CN205787907U (en) * | 2016-05-23 | 2016-12-07 | 西安天成益邦电子科技有限公司 | A kind of unmanned aerial vehicle controls work station |
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Application publication date: 20180323 |