CN108791883A - A kind of party array unmanned plane and its control system - Google Patents
A kind of party array unmanned plane and its control system Download PDFInfo
- Publication number
- CN108791883A CN108791883A CN201810830739.3A CN201810830739A CN108791883A CN 108791883 A CN108791883 A CN 108791883A CN 201810830739 A CN201810830739 A CN 201810830739A CN 108791883 A CN108791883 A CN 108791883A
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- China
- Prior art keywords
- shell
- unmanned plane
- fixed
- communication module
- party
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000004891 communication Methods 0.000 claims abstract description 28
- 230000000694 effects Effects 0.000 claims abstract description 7
- 238000012935 Averaging Methods 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 230000001678 irradiating effect Effects 0.000 claims description 3
- 230000000505 pernicious effect Effects 0.000 claims description 3
- 230000001360 synchronised effect Effects 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000003993 interaction Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- 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
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The present invention relates to air vehicle technique fields, especially a kind of party array unmanned plane, including shell, shell is surrounded by four holders, three supporting rods are equipped on the inside of holder, supporting rod one end is equipped with lifting motor, the output end of lifting motor is equipped with rotor, shell side is equipped with communication module, side of the shell far from communication module is equipped with connecting rod, connecting rod is equipped with spill spin block, electric rotating machine is equipped in spill spin block, the one end of spill spin block far from electric rotating machine is fixed with color-changing lamp, the inside of shell is equipped with accumulator in the side of communication module, shell is fixed with distance-sensor in the side of accumulator, shell is fixed with control unit in side of the accumulator far from distance-sensor.The present invention also provides a kind of party control systems of array unmanned plane.Stage effect of the present invention is strong, and serious forgiveness is high, has market prospects, is suitble to promote.
Description
Technical field
The present invention relates to air vehicle technique field more particularly to a kind of party array unmanned plane and its control systems.
Background technology
UAV is referred to as " unmanned plane "（"UAV"）, controlled using radio robot and the program provided for oneself
The not manned vehicle that device manipulates.Unmanned plane is actually the general designation of unmanned vehicle, can be with from technical standpoint definition
It is divided into：Unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, nothing
People's parasol etc..Currently, unmanned plane is to work independently, ability to work is restricted, if group system can be formed, greatly
The ability to work of unmanned plane is improved, existing cluster unmanned plane performs poor performance when being shown for night, and easy damage out of control is badly in need of
A kind of party solves problem above with array unmanned plane.
Invention content
The purpose of the present invention is to solve existing in the prior art when unmanned plane is shown for night to perform poor performance, easily
The shortcomings that damage out of control, and a kind of party array unmanned plane and its control system proposed.
To achieve the goals above, present invention employs following technical solutions：
A kind of party array unmanned plane and its control system are designed, including shell, the shell surrounding are set by being welded and fixed
There is holder, four holders are symmetrical and uniformly on the housing, the holder is annular shape, the circle of the holder for setting
Three symmetrically arranged supporting rods are equipped with by being welded and fixed on the inside of ring, the one end of the supporting rod far from the holder passes through weldering
It connects and is fixed with lifting motor, the output end of the lifting motor is fixed with rotor, and the shell side is by being welded and fixed
Equipped with communication module, side of the shell far from the communication module is equipped with U-shaped gap, the opposite both sides of the U-shaped gap
It is equipped with connecting rod by being welded and fixed, spill spin block is rotatably connected to by shaft in the connecting rod, is passed through in the spill spin block
Screw is fixed with electric rotating machine, and the output end of the electric rotating machine is fixed with driving gear, fixes and set in the connecting rod
There is the fixed gear being meshed with the driving gear, the one end of the spill spin block far from the electric rotating machine is fixed with radium-shine
Lamp, the interior shell is cavity structure, and the inside of the shell is fixed with accumulator in the side of the communication module, described
Shell is fixed with distance-sensor in the side of the accumulator, and the shell is answered in the accumulator far from the distance perspective
The side of device is fixed with control unit, and described control unit is electrically connected by conducting wire with the accumulator.
Preferably, described control unit is CPU processor.
Preferably, the case top and bottom are screwed equipped with fender bracket, and the fender bracket is arc-shaped,
The fender bracket quantity of the shell unilateral side is two, and four fender brackets are symmetricly set on the shell both sides.
Preferably, the fender bracket and the holder are fixed with LED light by being glued, and the LED light is colorful LED
Lamp, the LED light are electrically connected by conducting wire with described control unit.
Preferably, the communication module includes GPS module and communication module.
Preferably, the distance-sensor, lifting motor, electric rotating machine, communication module, color-changing lamp pass through conducting wire and institute
State control unit electrical connection.
The present invention also provides a kind of party array unmanned planes and its control system, include the following steps：
S1, by several unmanned plane array arrangements on ground, make unmanned plane to hovering by communication module synchronous averaging lifting motor
State；
S2, by GPS module feed back space coordinate adjust unmanned plane array to party show scene top, at this time by with
The computer of communication module connection makes flare maneuver to unmanned plane and light instructs, and makes color-changing lamp or LED light according to live atmosphere
It shows different lighting effects, so that the irradiating angle of color-changing lamp is swung with stage music by the driving of electric rotating machine, set off by contrast existing
Field atmosphere；
S3, ensure adjacent unmanned plane pitch requirements by the feedback data of distance-sensor in flight course, prevent nobody
Machine, which collides, leads to pernicious chain reaction.
A kind of party array unmanned plane and its control system proposed by the present invention, advantageous effect are：By carrying LED
Mutual cooperation between the holder and fender bracket of lamp and the color-changing lamp with electric rotating machine makes party array unmanned plane at night
Stage expression effect and interaction capabilities reach best, improve ornamental performance, at the same by communication module and distance-sensor and
Mutual cooperation between control unit makes the collision rate of party array unmanned plane reduce, reduces operation cost.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of party array unmanned plane proposed by the present invention；
Fig. 2 is a kind of vertical profile structural schematic diagram of party array unmanned plane proposed by the present invention；
Fig. 3 is a kind of cross-sectional structural schematic diagram of party array unmanned plane proposed by the present invention.
In figure：Shell 1, holder 2, lifting motor 3, rotor 4, fender bracket 5, communication module 6, connecting rod 7, spill spin block 8, branch
Strut 9, color-changing lamp 10, LED light 11, electric rotating machine 12, driving gear 13, fixed gear 14, accumulator 15, distance-sensor 16,
Control unit 17.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.
Referring to Fig.1-3, a kind of party array unmanned plane and its control system, including shell 1,1 top of shell and bottom
It is screwed equipped with fender bracket 5, fender bracket 5 is arc-shaped, and unilateral 5 quantity of fender bracket of shell 1 is two, four guarantors
Retaining frame 5 is symmetricly set on 1 both sides of shell, and the setting of fender bracket 5 has effectively buffered impulse force when unmanned plane declines, improved nothing
Man-machine service life.
1 surrounding of shell is equipped with holder 2 by being welded and fixed, and four holders 2 are symmetrical and are uniformly arranged on shell 1, branch
Frame 2 is annular shape, and the annulus inside of holder 2 is equipped with three symmetrically arranged supporting rods 9 by being welded and fixed, and supporting rod 9 is separate
One end of holder 2 is equipped with lifting motor 3 by being welded and fixed, and the output end of lifting motor 3 is fixed with rotor 4, fender bracket 5 and
Holder 2 is fixed with LED light 11 by being glued, and LED light 11 is colorful LED lamp, and the setting of colorful LED lamp 11 makes party use
The night of array unmanned plane shows color desktop, more performs tension.
1 side of shell is equipped with communication module 6 by being welded and fixed, communication module 6 includes GPS module and communication module, shell
Side of the body 1 far from communication module 6 is equipped with U-shaped gap, and the opposite both sides of U-shaped gap are equipped with connecting rod 7 by being welded and fixed, even
Spill spin block 8 is rotatably connected to by shaft on extension bar 7, is screwed in spill spin block 8 equipped with electric rotating machine 12, electric rotating machine
12 output end is fixed with driving gear 13, and the fixed gear 14 being meshed with driving gear 13, rotation are fixed in connecting rod 7
The one end of switch block 8 far from electric rotating machine 12 is fixed with color-changing lamp 10, is cavity structure in shell 1, the inside of shell 1 is communicating
The side of module 6 is fixed with accumulator 15, and shell 1 is fixed with distance-sensor 16 in the side of accumulator 15, and shell 1 exists
Side of the accumulator 15 far from distance-sensor 16 is fixed with control unit 17, and control unit 17 is CPU processor, and control is single
Member 17 is electrically connected by conducting wire with accumulator 15, LED light 11, distance-sensor 16, lifting motor 3, electric rotating machine 12, communication mould
Block 6, color-changing lamp 10 are electrically connected by conducting wire with control unit 17.
In use, by between the holder 2 with LED light 11 and fender bracket 5 and the color-changing lamp 10 with electric rotating machine 12
It cooperates, so that party array unmanned plane is reached best in the stage expression effect and interaction capabilities at night, improve ornamental
Performance, while by the mutual cooperation between communication module 6 and distance-sensor 16 and control unit 17, make party array nobody
The collision rate of machine reduces, and reduces operation cost.
Embodiment
The present invention also provides a kind of party array unmanned planes and its control system, include the following steps：
S1, by several unmanned plane array arrangements on ground, make unmanned plane to hovering by communication module synchronous averaging lifting motor 3
State；
S2, by GPS module feed back space coordinate adjust unmanned plane array to party show scene top, at this time by with
The computer of communication module connection makes flare maneuver to unmanned plane and light instructs, and makes color-changing lamp 10 or LED light 11 according to scene
Atmosphere shows different lighting effects, so that the irradiating angle of color-changing lamp 10 is put with stage music by the driving of electric rotating machine 12
It is dynamic, set off live atmosphere by contrast；
S3, ensure adjacent unmanned plane pitch requirements by the feedback data of distance-sensor 16 in flight course, prevent nothing
Man-machine collide leads to pernicious chain reaction.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Any one skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (7)
1. a kind of party array unmanned plane, including shell（1）, which is characterized in that the shell（1）Surrounding is by being welded and fixed
Equipped with holder（2）, four holders（2）Symmetrical and uniform setting is in the shell（1）On, the holder（2）For annulus
Shape, the holder（2）Annulus on the inside of by be welded and fixed be equipped with three symmetrically arranged supporting rods（9）, the supporting rod（9）
Far from the holder（2）One end by be welded and fixed be equipped with lifting motor（3）, the lifting motor（3）Output end fix
Equipped with rotor（4）, the shell（1）Side is equipped with communication module by being welded and fixed（6）, the shell（1）Far from described logical
Interrogate module（6）Side be equipped with U-shaped gap, the opposite both sides of the U-shaped gap by be welded and fixed be equipped with connecting rod（7）, institute
State connecting rod（7）It is upper that spill spin block is rotatably connected to by shaft（8）, the spill spin block（8）It is inside screwed equipped with rotation
Motor（12）, the electric rotating machine（12）Output end be fixed with driving gear（13）, the connecting rod（7）On be fixed with
With the driving gear（13）The fixed gear being meshed（14）, the spill spin block（8）Far from the electric rotating machine（12）One end
It is fixed with color-changing lamp（10）, the shell（1）Interior is cavity structure, the shell（1）Inside in the communication module（6）
Side be fixed with accumulator（15）, the shell（1）In the accumulator（15）Side be fixed with distance-sensor
（16）, the shell（1）In the accumulator（15）Far from the distance-sensor（16）Side be fixed with control unit
（17）, described control unit（17）Pass through conducting wire and the accumulator（15）Electrical connection.
2. a kind of party array unmanned plane according to claim 1, which is characterized in that described control unit（17）For
CPU processor.
3. a kind of party array unmanned plane according to claim 1, which is characterized in that the shell（1）Top and bottom
Portion is screwed equipped with fender bracket（5）, the fender bracket（5）For arc-shaped, the shell（1）Unilateral fender bracket
（5）Quantity is two, four fender brackets（5）It is symmetricly set on the shell（1）Both sides.
4. a kind of party array unmanned plane according to claim 2, which is characterized in that the fender bracket（5）And it is described
Holder（2）LED light is fixed with by being glued（11）, the LED light（11）For colorful LED lamp, the LED light（11）It is logical
Cross conducting wire and described control unit（17）Electrical connection.
5. a kind of party array unmanned plane according to claim 1, which is characterized in that the communication module（6）Including
GPS module and communication module.
6. a kind of party array unmanned plane according to claim 1, which is characterized in that the distance-sensor（16）,
Lifting motor（3）, electric rotating machine（12）, communication module（6）, color-changing lamp（10）Pass through conducting wire and described control unit（17）Electricity
Connection.
7. a kind of party array unmanned plane and its control system according to claim 1-6, it is characterised in that：Including such as
Lower step：
S1, by several unmanned plane array arrangements on ground, pass through communication module synchronous averaging lifting motor（3）Make unmanned plane to outstanding
Stop state；
S2, by GPS module feed back space coordinate adjust unmanned plane array to party show scene top, at this time by with
The computer of communication module connection makes flare maneuver to unmanned plane and light instructs, and makes color-changing lamp（10）Or LED light（11）According to
Live atmosphere shows different lighting effects, passes through electric rotating machine（12）Driving make color-changing lamp（10）Irradiating angle with stage
Music is swung, and sets off live atmosphere by contrast；
S3, pass through distance-sensor in flight course（16）Feedback data ensure adjacent unmanned plane pitch requirements, prevent
Unmanned plane, which collides, leads to pernicious chain reaction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810830739.3A CN108791883A (en) | 2018-07-26 | 2018-07-26 | A kind of party array unmanned plane and its control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810830739.3A CN108791883A (en) | 2018-07-26 | 2018-07-26 | A kind of party array unmanned plane and its control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108791883A true CN108791883A (en) | 2018-11-13 |
Family
ID=64078234
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810830739.3A Pending CN108791883A (en) | 2018-07-26 | 2018-07-26 | A kind of party array unmanned plane and its control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108791883A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
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| CN104986331A (en) * | 2015-07-27 | 2015-10-21 | 致导科技（北京）有限公司 | Unmanned aerial vehicle rotor wing protection frame and unmanned aerial vehicle |
| CN205854525U (en) * | 2016-03-31 | 2017-01-04 | 翔升（上海）电子技术有限公司 | Rotating lens and unmanned plane |
| KR20170083379A (en) * | 2016-01-08 | 2017-07-18 | 한화테크윈 주식회사 | A flight vehicle comprising LADAR system |
| CN206398423U (en) * | 2016-12-23 | 2017-08-11 | 广州依威电子科技有限公司 | A kind of flight formula adjustment beam lamp |
| WO2018009950A1 (en) * | 2016-07-11 | 2018-01-18 | Ars Electronica Linz Gmbh & Co Kg | Unmanned aircraft and system for generating an image in the airspace |
| CN107943086A (en) * | 2017-12-21 | 2018-04-20 | 合肥灵猫传媒有限公司 | A kind of unmanned plane cluster makes a return voyage control system |
| CN108153327A (en) * | 2017-12-07 | 2018-06-12 | 浙江大学 | Formation light show system and control method outside a kind of quadrotor room |
-
2018
- 2018-07-26 CN CN201810830739.3A patent/CN108791883A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103419942A (en) * | 2013-09-10 | 2013-12-04 | 北京臻迪科技有限公司 | Unmanned aerial vehicle |
| CN104986331A (en) * | 2015-07-27 | 2015-10-21 | 致导科技（北京）有限公司 | Unmanned aerial vehicle rotor wing protection frame and unmanned aerial vehicle |
| KR20170083379A (en) * | 2016-01-08 | 2017-07-18 | 한화테크윈 주식회사 | A flight vehicle comprising LADAR system |
| CN205854525U (en) * | 2016-03-31 | 2017-01-04 | 翔升（上海）电子技术有限公司 | Rotating lens and unmanned plane |
| WO2018009950A1 (en) * | 2016-07-11 | 2018-01-18 | Ars Electronica Linz Gmbh & Co Kg | Unmanned aircraft and system for generating an image in the airspace |
| CN206398423U (en) * | 2016-12-23 | 2017-08-11 | 广州依威电子科技有限公司 | A kind of flight formula adjustment beam lamp |
| CN108153327A (en) * | 2017-12-07 | 2018-06-12 | 浙江大学 | Formation light show system and control method outside a kind of quadrotor room |
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| PB01 | Publication | ||
| PB01 | Publication | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20181113 |