CN204433057U - A kind of with bat type aircraft - Google Patents
A kind of with bat type aircraft Download PDFInfo
- Publication number
- CN204433057U CN204433057U CN201420872189.9U CN201420872189U CN204433057U CN 204433057 U CN204433057 U CN 204433057U CN 201420872189 U CN201420872189 U CN 201420872189U CN 204433057 U CN204433057 U CN 204433057U
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- China
- Prior art keywords
- button
- ground
- aircraft
- steady arm
- control circuit
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Abstract
The utility model discloses one with bat type aircraft, comprise aircraft body, and the ground controller be connected with the wireless telecommunications of aircraft body; Aircraft body comprises flight control circuit, and with flight control circuit be connected flight locating module, fly wireless communication module and pick up camera; Ground controller is steady arm, comprises control housing, and is provided with the ground control circuit, terrestrial wireless communicating circuit and the ground locating module that control in housing; Terrestrial wireless communicating circuit, ground locating module and ground control circuit are electrically connected; Steady arm also comprise be located at control on housing with clapping button; Be electrically connected with bat button and ground control circuit; Terrestrial wireless communicating circuit is connected with the wireless telecommunications of flight wireless communication line.The utility model is after operator presses with bat button, and aircraft body according to the locating information of the steady arm received, can be taken pictures with the height preset, angle and distance to the object or person with steady arm or make a video recording, and reaches the object with clapping.
Description
Technical field
The utility model relates to a kind of small aircraft, particularly relates to a kind of with bat type aircraft.
Background technology
In prior art, have the small aircraft (unmanned vehicle) that much can carry out taking photo by plane, but these small aircrafts are in shooting process, for the shooting to other people or article as many, and are not suitable for carrying out trailing type shooting to the object of movement.Can directly with the function button clapped because the ground controller of small aircraft of the prior art (being also called remote controller) does not have, also not there is positioning function, cause utilizing small aircraft to carry out becoming very complicated with bat, and inconvenient operation.
Therefore, be necessary to develop the small aircraft that can carry out easily with clapping.
Utility model content
In order to overcome above-mentioned the deficiencies in the prior art part, the purpose of this utility model is to provide a kind of with bat type aircraft.
One, with bat type aircraft, comprises aircraft body, and the ground controller be connected with the wireless telecommunications of aircraft body; Described aircraft body comprises flight control circuit, and with flight control circuit be connected flight locating module, fly wireless communication module and pick up camera; Described ground controller is steady arm, comprises control housing, and is provided with the ground control circuit, terrestrial wireless communicating circuit and the ground locating module that control in housing; Described terrestrial wireless communicating circuit, ground locating module and ground control circuit are electrically connected; Described steady arm also comprise be located at control on housing with clapping button; Described is electrically connected with bat button and ground control circuit; Described terrestrial wireless communicating circuit is connected with the wireless telecommunications of flight wireless communication line.
Its further technical scheme is: described steady arm also comprises distance setting button, highly setting button and the angle initialization button being located at and controlling on housing.
Its further technical scheme is: described is mechanical button or electronic touching type I button with bat button, apart from setting button, highly setting button and angle initialization button.
Its further technical scheme is: described aircraft body is also provided with the imageing sensor for flight navigation upwards extended.
Its further technical scheme is: described flight locating module and ground locating module are GPS locating module or the Big Dipper locating module.
Its further technical scheme is: described aircraft body is provided with the steady The Cloud Terrace of increasing to downward-extension, and the below of the steady The Cloud Terrace of described increasing is provided with described pick up camera.
Its further technical scheme is: described steady arm is provided with the shooting read-out for showing with clapping image.
Its further technical scheme is: described steady arm is wear-type structure, be provided with control that housing is connected wear connection part.
Its further technical scheme is: the control housing of described steady arm is provided with the illuminating circuit carrying out when taking for aircraft body identifying; Described illuminating circuit and ground control circuit are electrically connected.
The utility model beneficial effect is compared with prior art: the ground controller that the utility model adopts with bat aircraft is steady arm, be provided with special following and clap button, after operator presses with bat button, the intrinsic flight control circuit of aircraft, can according to the locating information of the steady arm received, object or person with steady arm can being taken pictures or be made a video recording with the height preset, angle and distance, reaching the object with clapping.Owing to being provided with clapping button, operating in a key, very simply.The setting of correlation parameter can also be carried out by distance setting button, highly setting button and angle initialization button, thus allow, with bat, there is more alerting ability.
Below in conjunction with the drawings and specific embodiments, the utility model is further described.
Accompanying drawing explanation
Fig. 1 is a kind of using state schematic diagram with bat type aircraft specific embodiment of the utility model;
Fig. 2 is a kind of circuit structure block scheme with bat type aircraft specific embodiment of the utility model;
Fig. 3 is the plan sketch of a kind of steady arm with bat type aircraft specific embodiment of the utility model;
Fig. 4 is the side schematic view of Fig. 3;
Fig. 5 is a kind of plan sketch with bat type aircraft specific embodiment of the utility model.
Reference numeral
10 aircraft bodies 11 fly control circuit
12 flight locating module 13 pick up cameras
14 flight wireless communication line 20 steady arms
201 wear connection part 21 controls housing
22 ground control circuit 23 terrestrial wireless communicating circuits
24 ground locating module 25 self-timer buttons
26 distance setting buttons 27 highly set button
28 angle initialization buttons 29 are made a video recording read-out
202 directionkeys
Detailed description of the invention
In order to more fully understand technology contents of the present utility model, below in conjunction with specific embodiment the technical solution of the utility model being introduced further and illustrating, but being not limited to this.
As shown in Figures 1 to 4, the utility model one, with bat type aircraft, comprises aircraft body 10, and the ground controller be connected with aircraft body 10 wireless telecommunications; Aircraft body 10 comprise flight control circuit 11, and with flight control circuit 11 be connected flight locating module 12, fly wireless communication module 12 and pick up camera 13; Ground controller is steady arm 20, comprises and controls housing 21, and is provided with the ground control circuit 22, terrestrial wireless communicating circuit 23 and the ground locating module 24 that control in housing 21; Terrestrial wireless communicating circuit 23, ground locating module 24 are electrically connected with ground control circuit 22; Steady arm 20 also comprise be located at control on housing 21 with clapping button 25; Be electrically connected with ground control circuit 22 with clapping button 25; Terrestrial wireless communicating circuit 23 is connected with the wireless telecommunications of flight wireless communication line 14.When aircraft body is in airflight state, aircraft control people handles steady arm, press with clapping button, effector (i.e. steady arm) sends location information to aircraft (i.e. aircraft body), flying vehicles control circuit controls aircraft body according to its location information and follows steady arm, and taken pictures continuously by camera alignment steady arm or make a video recording, thus realize the object of track shot.Store in flight control circuit acquiescence with clapping parameter (i.e. distance, height and angle), each flight is with after clapping, and what set follows bat parameter to be kept to fly in control circuit.Aircraft body 10 is provided with the steady The Cloud Terrace 15 of increasing to downward-extension, and the below increasing steady The Cloud Terrace 15 is provided with described pick up camera.
Steady arm 20 also comprises is located at distance setting button 26 (can be set as straight-line distance therebetween, also can be set as the distance of horizontal direction therebetween) controlled on housing 21, highly setting button 27 (namely between aircraft body and steady arm in the distance of vertical direction) and angle initialization button 28.Also be provided with the directionkeys 202 for controlling heading, lifting key 203, decline key 204 and start key 205.
Conveniently aircraft body carries out track shot in flight course, can increase identification mechanism.In the present embodiment, the control housing 2` of steady arm 20 is provided with the illuminating circuit 221 carrying out when taking for aircraft body identifying; Illuminating circuit 221 and ground control circuit 22 are electrically connected.Wherein, illuminating circuit can adopt infrared light, send the infrared light of the suitable wavelength that easy camera collection being shot judges, the camera acquisition of aircraft body is to image and judge infrared light place image relative position and control the steady cloud platform rotation of described increasing to make its camera alignment with the steady arm of illuminating circuit.Aircraft body is followed be taken people or object (such as automobile) and pick up camera and is aimed at always and be taken people or object and the whole moving process that realizes taking people or object is all recorded in pick up camera.
Wherein, follow bat button, distance setting button, highly setting button and angle initialization button can be mechanical button or electronic touching type I button.Flight locating module and ground locating module also can be GPS locating module or the Big Dipper locating module.
As shown in Figure 3 and Figure 4, steady arm 20 is also provided with the shooting read-out 29 for showing with clapping image, steady arm is wear-type structure, be provided with control that housing 21 is connected wear connection part 201, mobile person can be facilitated steady arm to be worn over head (such as ride fan).
In other embodiment, steady arm can have additional magnetic fixing structure, can steady arm on cycle frame or the vehicle frame of automobile, carry out track shot with this.
In other embodiment, aircraft body is also provided with the imageing sensor for flight navigation upwards extended, and navigator display is provided with on steady arm, the image in aircraft front is shown during for flying, because the heading of aircraft can change, therefore, imageing sensor is the top being fixed on aircraft body by rotating mechanism.This rotating mechanism is electrically connected with flight control circuit, is controlled by flight control circuit.In other embodiment, steady arm also can be allowed only to be provided with a read-out, by arranging a display switching push button, the displaying contents of read-out be switched, switches between navigation picture and photographed images.
In other embodiment, steady arm also can adopt other structure, does not such as arrange read-out; Again such as, distance setting button, highly setting button and angle initialization button are replaced realizing by numerical key.
In sum, the ground controller that the utility model adopts with bat aircraft is steady arm, be provided with special following and clap button, after operator presses with bat button, the intrinsic flight control circuit of aircraft, according to the locating information of the steady arm received, the object or person with steady arm can being taken pictures or be made a video recording with the height preset, angle and distance, reaching the object with clapping.Owing to being provided with clapping button, operating in a key, very simply.The setting of correlation parameter can also be carried out by distance setting button, highly setting button and angle initialization button, thus allow, with bat, there is more alerting ability.Be applicable to very much the track shot of a lot of sports fan (driving in such as by bike, skiing, roller-skating or open air).
Above-mentionedly only further illustrate technology contents of the present utility model with embodiment; so that reader is easier to understand; but do not represent embodiment of the present utility model and be only limitted to this, any technology done according to the utility model extends or recreation, all by protection of the present utility model.Protection domain of the present utility model is as the criterion with claims.
Claims (9)
1., with a bat type aircraft, comprise aircraft body, and the ground controller be connected with the wireless telecommunications of aircraft body; It is characterized in that described aircraft body comprises flight control circuit, and with flight control circuit be connected flight locating module, fly wireless communication module and pick up camera; Described ground controller is steady arm, comprises control housing, and is located at the ground control circuit, terrestrial wireless communicating circuit and the ground locating module that control in housing; Described terrestrial wireless communicating circuit, ground locating module and ground control circuit are electrically connected; Described steady arm also comprise be located at control on housing with clapping button; Described is electrically connected with bat button and ground control circuit; Described terrestrial wireless communicating circuit is connected with the wireless telecommunications of flight wireless communication line.
2. one according to claim 1 is with bat type aircraft, it is characterized in that described steady arm also comprises distance setting button, highly setting button and the angle initialization button being located at and controlling on housing.
3. one according to claim 2 is with bat type aircraft, it is characterized in that button is clapped in described following, distance sets button, highly set button and angle initialization button is mechanical button or electronic touching type I button.
4. one according to claim 1 is with bat type aircraft, it is characterized in that described aircraft body is also provided with the imageing sensor for flight navigation upwards extended.
5. one according to claim 1 is with bat type aircraft, it is characterized in that described flight locating module and ground locating module are GPS locating module or the Big Dipper locating module.
6. one according to claim 1 is with bat type aircraft, and it is characterized in that described aircraft body is provided with the steady The Cloud Terrace of increasing to downward-extension, the below of the steady The Cloud Terrace of described increasing is provided with described pick up camera.
7. one according to claim 1 is with bat type aircraft, it is characterized in that described steady arm is provided with the shooting read-out for showing with clapping image.
8. one according to claim 1 is with bat type aircraft, it is characterized in that described steady arm is wear-type structure, be provided with control that housing is connected wear connection part.
9. one according to claim 1 is with bat type aircraft, it is characterized in that the control housing of described steady arm is provided with the illuminating circuit carrying out when taking for aircraft body identifying; Described illuminating circuit and ground control circuit are electrically connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420872189.9U CN204433057U (en) | 2014-12-31 | 2014-12-31 | A kind of with bat type aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420872189.9U CN204433057U (en) | 2014-12-31 | 2014-12-31 | A kind of with bat type aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204433057U true CN204433057U (en) | 2015-07-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420872189.9U Expired - Fee Related CN204433057U (en) | 2014-12-31 | 2014-12-31 | A kind of with bat type aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204433057U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104527978A (en) * | 2014-12-31 | 2015-04-22 | 深圳雷柏科技股份有限公司 | Followed shooting type aircraft and followed shooting method thereof |
| CN105430261A (en) * | 2015-11-16 | 2016-03-23 | 杨珊珊 | Photographing method of unmanned aerial vehicle and photographing device of unmanned aerial vehicle |
-
2014
- 2014-12-31 CN CN201420872189.9U patent/CN204433057U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104527978A (en) * | 2014-12-31 | 2015-04-22 | 深圳雷柏科技股份有限公司 | Followed shooting type aircraft and followed shooting method thereof |
| CN105430261A (en) * | 2015-11-16 | 2016-03-23 | 杨珊珊 | Photographing method of unmanned aerial vehicle and photographing device of unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150701 Termination date: 20181231 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |