CN106741901A - Aircraft, system and implementation method with visual output function - Google Patents
Aircraft, system and implementation method with visual output function Download PDFInfo
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- CN106741901A CN106741901A CN201710003256.1A CN201710003256A CN106741901A CN 106741901 A CN106741901 A CN 106741901A CN 201710003256 A CN201710003256 A CN 201710003256A CN 106741901 A CN106741901 A CN 106741901A
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- 230000000007 visual effect Effects 0.000 title claims abstract description 84
- 238000000034 method Methods 0.000 title claims abstract description 18
- 230000000694 effects Effects 0.000 claims abstract description 18
- 238000003384 imaging method Methods 0.000 claims description 3
- 238000004804 winding Methods 0.000 claims description 3
- 230000006870 function Effects 0.000 description 19
- 238000005516 engineering process Methods 0.000 description 8
- 230000008520 organization Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 239000010409 thin film Substances 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 235000011089 carbon dioxide Nutrition 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/06—Helicopters with single rotor
-
- 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/18—Stabilised platforms, e.g. by gyroscope
-
- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/08—Systems for measuring distance only
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Computer Networks & Wireless Communication (AREA)
- Automation & Control Theory (AREA)
- Controls And Circuits For Display Device (AREA)
Abstract
The invention provides a kind of aircraft with visual output function, and corresponding system and implementation method, belong to aircraft field.Visual display structure is provided with aircraft in the present invention, in the case of landing after state of flight or flight, visual observing effect is provided to the user in ground.This invention enables to aircraft to provide a kind of visual display effect to the user on ground in the state of flight or landing, especially can give people offer by visual display structure when crowd is dredged and dredge route.
Description
Technical field
The invention belongs to aircraft field.
Background technology
In the prior art, as preferred and non-limiting, aircraft is frequently used for entertaining and taking pictures field of photography.Aircraft
May include aircraft body, undercarriage, propeller, wing, empennage, and peripheral hardware camera and audio player etc..It is based on
Function and be easy to the characteristics of flexibly controlling that aircraft can fly, can also be applied to other field, such as in crowd density
Place generation fire higher or religionist collective occur to dredge crowd during emergency situations when paying respects to, or for specific mesh
Mark is monitored.But aircraft of the prior art can't be used for these purposes.
The content of the invention
It is an object of the invention to provide a kind of aircraft with visual output function, and corresponding system and realization
Method, visual display structure is provided with by aircraft, in the case of landing after state of flight or flight, is carried to user
For visual observing effect.
Further, the aircraft with visual output function is rotary aircraft, or fixed-wing formula aircraft, or
Jet aircraft, or umbrella wing formula aircraft, or flapping-wing type aircraft or dirigible one of which.
Further, the aircraft is provided with image unit, and the content that the image unit shoots can be regarded by described
Feel that display structure shows.
Further, described to be provided with lighting unit with aircraft, the lighting unit can be according to instruction to object
It is illuminated.
Further, the aircraft is provided with navigation elements and automatic cruising unit, and the navigation elements are according to destination
Optimal navigation way can be automatically planned, the automatic cruising unit can be cruised according to optimal navigation way.
Further, the aircraft is provided with the unit that amplifies, and the unit that amplifies can amplify voice signal and play out
Come.
Further, the visual display structure is display screen, and the display screen hangs on aircraft lower section or according to viewing
Angle is arranged at aircraft side.
Further, shown visual display structure is the display screen that can be folded, and is realized by opening the display screen for folding
The presentation of information in bigger region.
Further, shown visual display structure includes more than two display units, can come to open respectively as needed
The display unit of varying number.
Further, also including projection structure, the projection structure can set phase according to the Visual Observations Observations angle of user
The perspective plane answered, is projected with the content shown in visual display structure to projection structure.
Further, also including projection structure, the projection structure includes curling display unit and spool, and the curling shows
Unit winding is arranged on spool, it is possible to is closed up relative to spool or is opened.
Further, projection structure and more than one flight structure are provided with the aircraft, the flight structure can
Hang the perspective plane and depart from aircraft, the projection structure is used to project the content shown in visual display structure.
Further, also including projection structure, the projection structure is using in medium of the space eruption with imaging characteristic
Form is projected.
Further, also including rotational structure, the rotational structure connects visual display structure and aircraft, the aircraft
The angle of inclination of visual display structure can be adjusted by rotational structure.
Present invention additionally comprises a kind of implementation method of the aircraft with visual output function, the method includes following step
Suddenly：
In the case of landing after state of flight or flight, the user earthward gone up by visual display structure provides vision
On observing effect.
Present invention additionally comprises a kind of system of the aircraft with visual output function, the system includes：
Flying unit, the flight for controlling aircraft；
Visual display structure, in the case of landing after state of flight or flight, provides to the user in ground
Visual observing effect.
Brief description of the drawings
Fig. 1 is a kind of structural representation of embodiment of the aircraft with visual output function of the present invention.
Fig. 2 is the Flight Vehicle Structure schematic diagram with visual output function and camera function of the present invention.
Fig. 3 is the structural representation of rotational structure of the present invention.
Fig. 4 is the structural representation of aircraft group of the present invention.
Fig. 5 is the flow chart of the implementation method of the aircraft with visual output function of the present invention.
Fig. 6 is the system schematic of the aircraft with visual output function in the present invention.
Specific embodiment
Shared vehicle and its stop position indicating means, client are provided the present invention below in conjunction with the drawings and specific embodiments
End and system are described in further detail.It should be noted that technical characteristic or technical characteristic described in following embodiments
Combination be not construed as isolated, they can be mutually combined so as to reach superior technique effect.In following realities
Apply in the accompanying drawing of example, the identical label that each accompanying drawing occurs represents identical feature or part, can be applied to different embodiments
In.Therefore, once being defined in a certain Xiang Yi accompanying drawing, then it need not further be begged in subsequent accompanying drawing
By.
It should be noted that, depicted structure, ratio, size etc. in this specification institute accompanying drawing are only used to coordinate explanation
Content disclosed in book, so that those skilled in the art understands and reads, is not limited to invent enforceable restriction bar
Part, the modification of any structure, the change of proportionate relationship or the adjustment of size are not influenceing to invent effect and the institute's energy that can be generated
Under the purpose reached, all should fall in the range of the technology contents disclosed in invention to be covered.The side of being preferable to carry out of the invention
The scope of formula includes other realization, wherein the order of described or discussion can not be pressed, including function involved by basis is pressed
Basic mode simultaneously or in the opposite order, carrys out perform function, and this should be by the skill of embodiments of the invention art
Art personnel understood.
May be not discussed in detail for technology, method and apparatus known to person of ordinary skill in the relevant, but suitable
In the case of, the technology, method and apparatus should be considered as authorizing a part for specification.Institute that is shown here and discussing
Have in example, any occurrence should be construed as merely exemplary, not as limitation.Therefore, exemplary embodiment
Other examples can have different values.
The present invention is a kind of aircraft with visual output function, as preferred and non-limiting, is used in the present embodiment
Quadrotor, as shown in figure 1, it includes aircraft body 100, the rotor 110 above aircraft, and positioned at winged
Undercarriage 120 below row device, the display screen 140 in Fig. 1 illustrates a floor map for public place, in the schematic diagram
The information such as fire escape, major trunk roads and orientation are identified with, for Evacuation.
Used as preferred and non-limiting, rotor 110 is symmetrically distributed at four direction around body, and four rotors
In sustained height plane, as an example, the structure and radius of four rotors are all identical, and wherein each rotor is respectively configured an electricity
Machine, four motors are symmetrically mounted at the bracket end of aircraft.
It is in the present embodiment, real by controlling four rotating speeds of motor to change variable rotor speed as preferred and non-limiting
Existing lift variation, so as to control attitude and the position of aircraft.
Fig. 2 is the structural representation of the aircraft with camera function in the present invention.Including fuselage 200, rotor 210, spiral shell
Rotation oar 220, lighting unit 230, undercarriage 240, image unit 250, connecting rod 130 and display screen 140.The image unit
250 contents for shooting can be shown by the visual display structure.Lead between image unit 250 and visual display structure
Cross and electrically connect or be of coupled connections so that the content captured by image unit 250 can be transferred to visual display structure and pass through
Visual display structure shows.
As an example, visual display structure uses display screen 140, and display screen material is that TFT (thin film transistor (TFT)), TFD are (thin
Film diode), one of UFB (colorful display screen technology) and OLED (Organic Electricity laser display).As an example, display screen leads to
Cross connecting rod 140 and be connected to aircraft lower section.
As an example, also including rotational structure 300, the rotational structure 300 passes through junction 310 and aircraft bottom phase
Connection, as shown in figure 3, aircraft can adjust the angle of inclination of visual display structure by rotational structure 300.So can
Advantageously watched in the user positioned at ground.
As an example, image unit 250 includes two cameras, and can automatically adjust Jiao according to the distance of object
Away from.Can so enable that aircraft is monitored to specific objective thing, and monitored results are passed to visual display structure,
The content that user can show according to visual display structure carries out monitor in real time to object, also, in the present embodiment, flight
Storage organization is additionally provided with device, the content captured by image unit 250 is stored in storage organization simultaneously, when can preset storage
Between threshold value, for example, it can be set to being to preserve the shooting video within two hours, then reach two hours when video is shot
When, the video that storage organization shoots before will being automatically deleted two hours.
As an example, the lighting unit 230 in the present embodiment includes light source and focusing structure, can be to ground by focusing
It is focused irradiation, scattering or tracking radiation.In the present embodiment, lighting unit 230 is used to be irradiated photographic subjects thing,
Reach the purpose that shooting effect becomes apparent from.
As an example, navigation elements and automatic cruising unit, shown navigation elements and automatic cruising are additionally provided with aircraft
Electrically connected between unit or be of coupled connections, user can preset destination, then navigation elements are according to when prelocalization and default mesh
The distance between ground make optimal navigation way, the optimal navigation way that then automatic cruising unit makes according to navigation elements
Automatic cruising is carried out, so as to fly automatically to the top of predeterminated position.
As an example, audio playing unit is additionally provided with aircraft, user can preset voice or is input into by remote control
Voice, and played back by audio playing unit.In the present embodiment, aircraft can hover on specific destination
Side, and audio broadcasting is carried out, under particular circumstances, reminding people to note specific item, reaching to be reminded than word more has
The purpose of effect.
Used as preferred and non-limiting, visual display structure of the invention is the display screen that can be folded, and is folded by opening
Display screen realize the presentation of information in bigger region.
As an example, shown visual display structure may also include more than two display units, can come to divide as needed
Not Da Kai varying number display unit.
Used as preferred and non-limiting, also including projection structure, the projection structure can be according to the Visual Observations Observations angle of user
Spend to set corresponding curtain 170, projecting apparatus 150 is located at aircraft lower section.In the present embodiment, projection structure is with face at a slant
Direction earthward is set, and the curtain 170 of projection can more facilitate user to watch towards ground.
As an example, projection structure includes curling display unit and spool, and the curling display unit winding is arranged at volume
On axle, it is possible to close up relative to spool or open.Under non-working condition, curling unit is close on spool, is made
With under state, curling unit is to launch relative to spool.So cause that the folding of projection structure is more flexible, in the shape for folding
Area occupied can be saved under state.
Projection structure in the present embodiment is arranged in aircraft, and including more than one Miniature Vehicle structure 160, is made
It is citing, two Miniature Vehicle structures 160 is set in the present embodiment, the Miniature Vehicle structure 160 is relative to aircraft 100
It is independent, aircraft 100 can be departed from, it is also possible to be called small aircraft, when needing to be projected, Miniature Vehicle structure
160 can carry curtain 170 flies away from aircraft 100, and the curtain 170 of carrying is perspective plane, by the throwing on aircraft 100
Shadow instrument 150 is projected.So enable to projected position more flexible, beneficial to user's viewing.
As preferred and non-limiting, the side on perspective plane can be served as using the medium with imaging characteristic is erupted in space
Formula come realize projection function.As an example, this medium selects vapor or dry ice.This method causes that projection is cleverer
Live, and save perspective plane and take up room.And with effect attractive in appearance, more people can be attracted to watch.
As an example, it would however also be possible to employ the mode of line holographic projections is shown that this display causes that display effect is more forced
Very, more aesthetic and more people can be attracted to watch.
As preferred and non-limiting, distance measurement unit, the distance measurement unit are provided with aircraft in the present invention
After detecting the distance between aircraft and user, display effect is adjusted according to the distance；Or preset optimal viewing distance, root
The distance between aircraft and user are adjusted according to optimal viewing distance.
As an example, the distance measurement technology in the present embodiment uses radar range finding, the optimal viewing distance of user preset
It it is 5 meters, then when the distance that radar is measured is 10 meters, aircraft can automatically reduce height, drop to and stop close to when 5 meters
Landing, suspends in the air, is easy to user to watch.
Used as preferred and non-limiting, another method is, when the distance that radar range finding is detected is more than 5 meters, to put automatically
Font in big visual display structure such that it is able to allow user it can be clearly seen that content on visual display unit.
Used as preferred and non-limiting, also including collecting unit, the collecting unit can gather user action or voice, enter
One step ground, user action can be one of gesture, walk and lip reading, and the visual display structure is adjusted according to user action and voice
Whole shown content.In the present embodiment, the content that can be shown using gesture control visual display structure, collecting unit is to gesture
Collection can use ToF (flight time of light) technology, structured light technique or millimeter Radar Technology, when collecting unit collection
To after the gesture of user, the gesture motion according to user forms corresponding control command, so that display visual display structure energy
Enough show corresponding content.
As shown in figure 5, the present embodiment is a kind of implementation method of the aircraft with visual output function, including following step
Suddenly：
As preferred and non-limiting, in the case of landing after state of flight or flight, by visual display structure to ground
User on face provides visual observing effect.
Specific method is comprised the following steps：
S1：Start aircraft, aircraft is in state of flight；
S2：The user earthward gone up by carry-on visual display structure provides visual observing effect.
As an example, the switch of aircraft, pre-set flight paths and flying height are first turned on, or using remote control dress
The state of flight of control aircraft is put, behind aircraft flight to default destination and preset height, carry-on regarding is opened
Feel display structure, the visual display structure in the present embodiment is display screen, and display screen is set to 45 degree of angles direction directed downwardly, side
Just user's viewing, aircraft can play the recording being preset in storage organization when necessary, so that being inconvenient to watch aobvious
The user of display screen can also know the content on display screen.
As an example, display screen can be fixed at aircraft lower section, it would however also be possible to employ the mode of projection, using projection
Mode needs one piece of curtain, and curtain can hang on aircraft lower section, and projecting apparatus is located at the upright position to curtain under aircraft,
It is convenient that curtain is projected.
As shown in fig. 6, shown in Fig. 6 be aerocraft system structured flowchart 400, including：Lighting unit 410, image unit
440th, memory cell 420 and visual display structure 430.Lighting unit 410 is used to image ground when image unit 440
When, the target to be imaged of image unit 440 is illuminated, for improving photographic effect；Memory cell 420 is used for shooting
Content captured by unit 440 is stored, and to save memory space, user can be preset in one shooting of time period of storage
Hold, for example the content of shooting to nearest two hours is stored；Content captured by image unit 440 can directly by regarding
Feel that display structure 430 is played out, or storage is in memory cell 420, or while visual display structure 430 is played out
It is stored in memory cell 420；The content stored in memory cell 420 directly can be broadcast by visual display structure 430
Put, such as user can preset broadcasting content in memory cell 420, then be played out by visual display structure 430.
In several embodiments provided by the present invention, it should be understood that ground refers to the place relative with sky, bag
Earth surface and sea level are included, and positioned at the object on earth surface or sea level.
Aircraft may also include the winged control plate for controlling flight, and flying control plate includes circuit board and be arranged on circuit board
Functional module for realizing predetermined function, functional module can include controller module, processor module, sensor assembly
Deng.Further, sensor assembly can include inertia measuring module, temperature sensor module, Height sensor module, distance
Sensor assembly etc..Inertia measuring module includes acceleration transducer and gyroscope, and inertia measuring module can measure nobody
The flight attitude information of aircraft.
Disclosed relevant apparatus and method in embodiment, can realize by another way.For example, described above
Device embodiment be schematical, for example, the division of the module or unit, only a kind of division of logic function is actual
There can be other dividing mode when realizing, such as multiple units or component can be combined or be desirably integrated into another and be
System, or some features can be ignored, or not perform.It is another, shown or discussed coupling or direct-coupling each other
Or communication connection can be the INDIRECT COUPLING or communication connection of device or unit by some interfaces, can be it is electrical, machinery or
Other forms.
The unit that is illustrated as separating component can be or may not be it is physically separate, it is aobvious as unit
The part for showing can be or may not be physical location, you can with positioned at a place, or can also be distributed to multiple
On NE.Some or all of unit therein can be according to the actual needs selected to realize the purpose of the present embodiment.
In addition, during each functional unit in each embodiment of the invention can be integrated in a processing unit, it is also possible to
It is that unit is individually physically present, it is also possible to which two or more units are integrated in a unit.Above-mentioned integrated list
Unit can both be realized in the form of hardware, it would however also be possible to employ the form of SFU software functional unit is realized.
Embodiments of the invention are the foregoing is only, the scope of the claims of the invention is not thereby limited, it is every to utilize this hair
Equivalent structure or equivalent flow conversion that bright specification and accompanying drawing content are made, or directly or indirectly it is used in other related skills
Art field, is included within the scope of the present invention.
Claims (15)
1. a kind of aircraft with visual output function, it is characterised in that：Aircraft is provided with visual display structure, for
In the case of landing after state of flight or flight, visual observing effect is provided to the user in ground.
2. a kind of aircraft with visual output function according to claim 1, it is characterised in that：The aircraft is
Rotary aircraft, or fixed-wing formula aircraft, or jet aircraft, or umbrella wing formula aircraft, or flapping-wing type aircraft or
Dirigible.
3. a kind of aircraft with visual output function according to claim 1, it is characterised in that：On the aircraft
Image unit is provided with, the content that the image unit shoots can be shown by the visual display structure.
4. a kind of aircraft with visual output function according to claim 1, it is characterised in that：On the aircraft
Navigation elements and automatic cruising unit are provided with, the navigation elements can automatically plan optimal navigation way, the automatic cruising
Unit can be cruised according to optimal navigation way.
5. a kind of aircraft with visual output function according to claim 1, it is characterised in that：On the aircraft
Audio playing unit is provided with, the audio playing unit can amplify voice signal and play back.
6. a kind of aircraft with visual output function according to claim 1, it is characterised in that：The visual display
Structure is display screen, and the display screen hangs on aircraft lower section or is arranged at aircraft side according to viewing angle.
7. a kind of aircraft with visual output function according to claim 1, it is characterised in that：Shown visual display
Structure is the display screen that can be folded, and the presentation of information in bigger region is realized by opening the display screen for folding.
8. a kind of aircraft with visual output function according to claim 1, it is characterised in that：Shown visual display
Structure includes more than two display units, can as needed carry out to open respectively the display unit of varying number.
9. a kind of aircraft with visual output function according to claim 1, it is characterised in that：Also include that projection is tied
Structure, the projection structure can set corresponding perspective plane according to the Visual Observations Observations angle of user, with visual display structure
The content of display is projected to projection structure.
10. a kind of aircraft with visual output function according to claim 1, it is characterised in that：Also include projection
Structure, the projection structure includes curling display unit and spool, and the curling display unit winding is arranged on spool, and can
Close up or open with relative to spool.
A kind of 11. aircraft with visual output function according to claim 1, it is characterised in that：The aircraft
Projection structure and at least one flight structure are inside provided with, the flight structure can hang the perspective plane and depart from aircraft,
The projection structure is used to project the content shown in visual display structure.
A kind of 12. aircraft with visual output function according to claim 1, it is characterised in that：Also include projection
Structure, the projection structure is projected using in the form of medium of the space eruption with imaging characteristic.
A kind of 13. aircraft with visual output function according to claim 1, it is characterised in that：Also include rotating
Structure, the rotational structure connects the visual display structure and the aircraft, and the aircraft can be by the rotation
Structure adjusts the angle of inclination of the visual display structure.
A kind of 14. implementation methods of the aircraft with visual output function, it is characterised in that：The method includes:
In the case of landing after state of flight or flight, the user earthward gone up by visual display structure provides visual
Observing effect.
A kind of 15. systems of the aircraft with visual output function, it is characterised in that：The system includes,
Flying unit, the flight for controlling aircraft；
Visual display structure, in the case of landing after state of flight or flight, vision is provided to the user in ground
On observing effect.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710003256.1A CN106741901A (en) | 2017-01-04 | 2017-01-04 | Aircraft, system and implementation method with visual output function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710003256.1A CN106741901A (en) | 2017-01-04 | 2017-01-04 | Aircraft, system and implementation method with visual output function |
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| Publication Number | Publication Date |
|---|---|
| CN106741901A true CN106741901A (en) | 2017-05-31 |
Family
ID=58949402
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710003256.1A Withdrawn CN106741901A (en) | 2017-01-04 | 2017-01-04 | Aircraft, system and implementation method with visual output function |
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| CN105517664A (en) * | 2014-05-30 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Systems and methods for uav docking |
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2017
- 2017-01-04 CN CN201710003256.1A patent/CN106741901A/en not_active Withdrawn
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|---|---|---|---|---|
| US20120104155A1 (en) * | 2010-11-02 | 2012-05-03 | Groen Brothers Aviation, Inc. | Tail jet apparatus and method for low speed yaw control of a rotorcraft |
| CN102566955A (en) * | 2010-12-30 | 2012-07-11 | 上海量明科技发展有限公司 | Display range adjustable display method and system |
| CN105517664A (en) * | 2014-05-30 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Systems and methods for uav docking |
| CN104820422A (en) * | 2015-04-20 | 2015-08-05 | 杨珊珊 | Unmanned aerial vehicle |
| CN104908960A (en) * | 2015-06-03 | 2015-09-16 | 东华大学 | Air command unmanned aerial vehicle capable of performing man-machine conversation function |
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Application publication date: 20170531 |
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