CN106023560A - Folding type unmanned aerial vehicle remote controller - Google Patents
Folding type unmanned aerial vehicle remote controller Download PDFInfo
- Publication number
- CN106023560A CN106023560A CN201610546927.4A CN201610546927A CN106023560A CN 106023560 A CN106023560 A CN 106023560A CN 201610546927 A CN201610546927 A CN 201610546927A CN 106023560 A CN106023560 A CN 106023560A
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- CN
- China
- Prior art keywords
- lower house
- controller
- aerial vehicle
- antenna module
- unmanned aerial
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- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
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- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Support Of Aerials (AREA)
Abstract
The invention discloses a folding type unmanned aerial vehicle remote controller. The folding type unmanned aerial vehicle remote controller comprises a lower shell and an upper shell hinged to the lower shell. The upper shell rotates upwards to open the lower shell or rotates downwards to close the lower shell. The lower shell and the upper shell are internally provided with controllers for controlling an unmanned aerial vehicle. The lower shell is internally provided with an antenna module used for receiving and transmitting signals. The controllers communicate with the antenna module. In this way, the folding type unmanned aerial vehicle remote controller can operate the unmanned aerial vehicle through remote control buttons and a control panel at the same time, the structure is simple, using is convenient, and the folding type unmanned aerial vehicle remote controller is safe and reliable.
Description
Technical field
The present invention relates to unmanned plane field, particularly relate to a kind of collapsible unmanned controller.
Background technology
Unmanned controller is the main means being currently used for controlling unmanned plane.Existing unmanned aerial vehicle (UAV) control mode mostly is remote pilot, and it needs all multiparameters beamed back according to unmanned plane to be judged whether voluntarily to be suitable for sending control instruction by remote control manipulator.Existing remote controller is typically all and operates to control unmanned plane by RPB, and remote controller volume is relatively big, carries inconvenience.
Summary of the invention
The technical problem that present invention mainly solves is to provide a kind of collapsible unmanned controller, it is possible to manipulate unmanned plane by RPB and control panel simultaneously, and simple in construction is easy to use, safe and reliable.
For solving above-mentioned technical problem, the technical scheme that the present invention uses is: provide a kind of collapsible unmanned controller, including lower house and the upper shell being hinged on lower house, described upper shell is rotated up opening lower house or rotating down to close lower house, the controller for controlling unmanned plane it is mounted in described lower house and upper shell, being also equipped with the antenna module for accepting and launch signal inside described lower house, described controller is connected with antenna module.
In a preferred embodiment of the present invention, in the mounting groove body that described antenna module is hinged on lower house, described antenna module rotates to be installed cell body to depart from or is recovered to install cell body.
In a preferred embodiment of the present invention, described lower house being additionally provided with the RPB assembly for controlling unmanned plane, described RPB assembly is connected with antenna module.
In a preferred embodiment of the present invention, described controller is panel computer or mobile phone.
In a preferred embodiment of the present invention, the left and right sides of described lower house is additionally provided with handle, is additionally provided with multiple louvre bottom described lower house.
The invention has the beneficial effects as follows: the collapsible unmanned controller of the present invention, it is possible to manipulate unmanned plane by RPB and control panel, simple in construction simultaneously, easy to use, safe and reliable.
Accompanying drawing explanation
For the technical scheme being illustrated more clearly that in the embodiment of the present invention, in describing embodiment below, the required accompanying drawing used is briefly described, apparently, accompanying drawing in describing below is only some embodiments of the present invention, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings, wherein:
Fig. 1 is the perspective view of the present invention collapsible unmanned controller one preferred embodiment;
Fig. 2 is the front view of collapsible unmanned controller shown in Fig. 1;
Fig. 3 is the upward view of collapsible unmanned controller shown in Fig. 2;
In accompanying drawing, the labelling of each parts is as follows: 1, lower house, and 2, upper shell, 3, controller, 4, antenna module, 5, cell body is installed, 6, RPB assembly, 7, handle, 8, louvre.
Detailed description of the invention
Technical scheme in the embodiment of the present invention will be clearly and completely described below, it is clear that described embodiment is only a part of embodiment of the present invention rather than whole embodiments.Based on the embodiment in the present invention, all other embodiments that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of protection of the invention.
Refer to Fig. 1, a kind of collapsible unmanned controller, including lower house 1 and the upper shell 2 being hinged on lower house 1, upper shell 2 is rotated up opening lower house 1 or rotating down to close lower house 1, the controller 3 for controlling unmanned plane it is mounted in lower house 1 and upper shell 2, lower house 1 is internal is also equipped with the antenna module 4 for accepting and launch signal, and controller 3 is connected with antenna module 4.
It addition, antenna module 4 is hinged in the installation cell body 5 on lower house 1, antenna module 4 rotates to be installed cell body 5 to depart from or is recovered to install cell body 5.
It addition, be additionally provided with the RPB assembly 6 for controlling unmanned plane on lower house 1, RPB assembly 6 is connected with antenna module 4, and RPB assembly 6 may be used for auxiliary operation unmanned plane.
It addition, controller 3 is panel computer or mobile phone, by directly carrying out operation on panel computer or mobile phone can control unmanned plane.
It addition, the left and right sides of lower house 1 is additionally provided with handle 7, bottom lower house 1, it is additionally provided with multiple louvre 8.
It is different from prior art, the collapsible unmanned controller of the present invention, it is possible to manipulate unmanned plane by RPB and control panel simultaneously, simple in construction, easy to use, safe and reliable.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every equivalent structure utilizing description of the invention content to be made or equivalence flow process conversion; or directly or indirectly it is used in other relevant technical field, the most in like manner it is included in the scope of patent protection of the present invention.
Claims (5)
1. a collapsible unmanned controller, it is characterized in that, including lower house and the upper shell being hinged on lower house, described upper shell is rotated up opening lower house or rotating down to close lower house, the controller for controlling unmanned plane it is mounted in described lower house and upper shell, being also equipped with the antenna module for accepting and launch signal inside described lower house, described controller is connected with antenna module.
Collapsible unmanned controller the most according to claim 1, it is characterised in that in the mounting groove body that described antenna module is hinged on lower house, described antenna module rotates to be installed cell body to depart from or is recovered to install cell body.
Collapsible unmanned controller the most according to claim 2, it is characterised in that be additionally provided with the RPB assembly for controlling unmanned plane on described lower house, described RPB assembly is connected with antenna module.
4. according to the arbitrary described collapsible unmanned controller of claim 1-3, it is characterised in that described controller is panel computer or mobile phone.
Collapsible unmanned controller the most according to claim 4, it is characterised in that the left and right sides of described lower house is additionally provided with handle, is additionally provided with multiple louvre bottom described lower house.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201610546927.4A CN106023560A (en) | 2016-07-13 | 2016-07-13 | Folding type unmanned aerial vehicle remote controller |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201610546927.4A CN106023560A (en) | 2016-07-13 | 2016-07-13 | Folding type unmanned aerial vehicle remote controller |
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CN106023560A true CN106023560A (en) | 2016-10-12 |
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Family Applications (1)
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CN201610546927.4A Pending CN106023560A (en) | 2016-07-13 | 2016-07-13 | Folding type unmanned aerial vehicle remote controller |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
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WO2018171014A1 (en) * | 2017-03-21 | 2018-09-27 | 深圳市大疆创新科技有限公司 | Remote control |
WO2018191982A1 (en) * | 2017-04-21 | 2018-10-25 | 深圳市大疆创新科技有限公司 | Antenna, ground control system of unmanned aerial vehicle, and unmanned aerial vehicle system |
WO2019033562A1 (en) * | 2017-08-17 | 2019-02-21 | 深圳市大疆创新科技有限公司 | Remote control |
WO2019128383A1 (en) * | 2017-12-27 | 2019-07-04 | 深圳市道通智能航空技术有限公司 | Remote controller |
WO2021062659A1 (en) * | 2019-09-30 | 2021-04-08 | 深圳市大疆创新科技有限公司 | Bracket structure and movable platform |
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CN105519246A (en) * | 2014-11-28 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Fastening assembly, fastening mechanism, rack using fastening mechanism and remote control |
CN205899785U (en) * | 2016-07-13 | 2017-01-18 | 无锡觅睿恪科技有限公司 | Foldable unmanned aerial vehicle remote controller |
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Patent Citations (8)
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US20140207311A1 (en) * | 2008-02-12 | 2014-07-24 | Katherine C. Stuckman | Radio controlled aircraft, remote controller and methods for use therewith |
CN204170423U (en) * | 2014-10-25 | 2015-02-25 | 杜超 | A kind of remote controller with flexible display screen |
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Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
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WO2018171014A1 (en) * | 2017-03-21 | 2018-09-27 | 深圳市大疆创新科技有限公司 | Remote control |
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WO2018191982A1 (en) * | 2017-04-21 | 2018-10-25 | 深圳市大疆创新科技有限公司 | Antenna, ground control system of unmanned aerial vehicle, and unmanned aerial vehicle system |
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WO2021062659A1 (en) * | 2019-09-30 | 2021-04-08 | 深圳市大疆创新科技有限公司 | Bracket structure and movable platform |
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Application publication date: 20161012 |