CN204679772U - Terminal remote control device - Google Patents
Terminal remote control device Download PDFInfo
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- CN204679772U CN204679772U CN201520076007.1U CN201520076007U CN204679772U CN 204679772 U CN204679772 U CN 204679772U CN 201520076007 U CN201520076007 U CN 201520076007U CN 204679772 U CN204679772 U CN 204679772U
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- 238000000034 method Methods 0.000 claims description 9
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 11
- 238000006073 displacement reaction Methods 0.000 description 7
- 230000005611 electricity Effects 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
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- 230000000694 effects Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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Abstract
The utility model embodiment provides a kind of terminal remote control device, not only there is the operating grip of the telechiric device of specialty, there is again multi-functional intelligent terminal module, when controlling aircraft, achieve flight control accuracy high, simultaneously by the locating module of this terminal remote control device, by the positional information of the locating module collection by telechiric device send to aircraft fly control plate, the positional information of the locating module collection of telechiric device flown control plate effectively utilize time, aircraft is in conjunction with self positional information, aircraft is made to have the function of automatically following movement to telechiric device.Drastically increase the use sense of operator like this.
Description
Technical field
The utility model relates to a kind of terminal remote control device, particularly, relates to a kind of terminal remote control device for controlling aircraft.
Background technology
At present on the market, unpiloted model aerial vehicle (such as fixed wing aircraft, rotor craft comprises helicopter), be widely used, such as in detecting, search and rescue, there is a lot of application the aspects such as model of an airplane amusement, the daily shooting of wedding.
Manipulation for aircraft is realized by terminal remote control device (also claiming " telechiric device ") by user usually, manipulator moves in operate aircraft, as in the process of unmanned vehicle, because unmanned vehicle average physique is less, when flying far away, (as four or five hundred meters) are with the naked eye difficult to see clearly, during because of manipulator's operate aircraft, himself usually can move, such manipulator can be absorbed in display screen, the last position that also may cause not making clear that unmanned vehicle is current, cause getting lost and even fly to lose in this case, or manipulator need move a segment distance to pick up unmanned vehicle, such Consumer's Experience is had a greatly reduced quality.Be difficult to the use sense improving operator.
Utility model content
In order to overcome the defect of the remote control mode operability function singleness of the aircraft of prior art, provide a kind of terminal remote control device: by the combination of intelligent terminal module with the telechiric device handle of specialty, thus realize the use sense improving operator.
For achieving the above object, the utility model embodiment adopts following scheme:
A kind of terminal remote control device, is characterized in that: have
For controlling the parts of aircraft movement; Master control board; Described master control board is provided with the processor for the treatment of data; Described terminal remote control device also has: FSK transceiver; Locating module; Data acquisition module; The current location information of locating module described in described data collecting module collected sends to described FSK transceiver by described processor process.
Preferably, the above-mentioned parts for controlling aircraft movement are handle or button.
Preferably, above-mentioned terminal remote control device also comprises the 5.8G WiFi module for receiving and sending messages, and above-mentioned FSK transceiver is the FSK transceiver adopting 2.4G.
Preferably, the information of the above-mentioned locating module of collection that above-mentioned data acquisition module is real-time.And the information gathered is sent to aircraft by (time interval is determined by program setting) of the timing of FSK transceiver.
Preferably, above-mentioned locating module is used for accepting gps signal, Beidou navigation signal and/or GLONASS signal.
Further, above-mentioned locating module is built in above-mentioned remote terminal.
Further, said apparatus makes lip pencil, rectangular shape is carried with for operator.
Preferably, said apparatus also includes the height sensor for measuring height.
Further, above-mentioned height sensor is baroceptor.
Preferably, described remote terminal also comprises intelligent terminal module, and the Flight Condition Data of the described aircraft received is sent to described intelligent terminal module by described control data collector.
Further, described intelligent terminal module also comprises display screen; Described display screen shows described state of flight information.
Beneficial effect:
The terminal remote control device provided by the utility model embodiment, not only there is the operating grip of the telechiric device of specialty, there is again the multi-functional of intelligent terminal module, when controlling aircraft, achieve flight control accuracy high, simultaneously by the locating module of this terminal remote control device, by the positional information of the locating module collection by telechiric device send to aircraft fly control plate, the positional information of the locating module collection of telechiric device flown control plate effectively utilize time, aircraft is in conjunction with self positional information, aircraft is made to have the function of automatically following movement to telechiric device.Drastically increase the use sense of operator like this.
Accompanying drawing explanation
Below in conjunction with specific embodiment, such scheme is described further.Should be understood that these embodiments are not limited to for illustration of the utility model limit scope of the present utility model.The implementation condition adopted in embodiment specifically can do further adjustment according to the condition of producer, and not marked implementation condition is generally the condition in normal experiment.
Fig. 1 is the Facad structure schematic diagram of the terminal remote control device of embodiment of the present utility model.
Fig. 2 is the structure schematic diagram of the terminal remote control device of embodiment of the present utility model.
Fig. 3 is the partial enlarged drawing of the back side A of the terminal remote control device of embodiment of the present utility model.
Fig. 4 is the Facad structure schematic diagram of the terminal remote control device of another 1 embodiment of the present utility model.
Fig. 5 is the Electricity Functional module diagram of the terminal remote control device of embodiment of the present utility model.
The terminal remote control device that Fig. 6 is embodiment of the present utility model and the Electricity Functional module diagram of aircraft controlled.
The terminal remote control device that Fig. 7 is embodiment of the present utility model and the another 1 Electricity Functional module diagram of aircraft controlled.
Embodiment
Below in conjunction with specific embodiment, such scheme is described further.Should be understood that these embodiments are not limited to for illustration of the utility model limit scope of the present utility model.The implementation condition adopted in embodiment can do further adjustment according to the condition of concrete producer, and not marked implementation condition is generally the condition in normal experiment.In embodiment scheme, terminal remote control device is referred to as " telechiric device ".
Embodiment:
Fig. 1 is the Facad structure schematic diagram of telechiric device, and Fig. 2 is the structure schematic diagram of telechiric device; Composition graphs 1,2 describes the structure of the telechiric device of this programme, and telechiric device has: for controlling the handle 1 of aircraft movement, intelligent terminal module 2; Master control board 3; FSK transceiver 4; And locating module 5; Master control board 3 is provided with processor, data acquisition module, cache module (not shown); Data acquisition module will pass through the outside transmission (time interval is determined by program) of FSK transceiver 4 timing after the positional information treated device process of the locating module 5 gathered, FSK transceiver 4 can be used for the Flight Condition Data receiving aircraft (not shown), and transferring to intelligent terminal module 2, this intelligent terminal module 2 shows the flight information of aircraft.
Be illustrated in figure 3 the partial enlarged drawing of locating module 5 in Fig. 2, can find out that the built-in mode of locating module 5 is fixed on telechiric device from figure.
As shown in Figure 4, the Facad structure schematic diagram of the telechiric device of another 1 embodiment of utility model, distinguishes with scheme above and is, the mode inserted by the groove 6 on telechiric device for locating module 5 is connected on telechiric device.
In such scheme, locating module 5 is support the independence of GPS (GPS) and GLONASS (Global Navigation Satellite System) (GLONASS) signal or the synchronous module received.
As the distortion of such scheme, locating module 5 is only GPS module and also can.
In such scheme, telechiric device can be made into lip pencil and carries with for operator.
In such scheme, handle can be replaced button and also can realize moving control aircraft.
Composition graphs 5,6; For telechiric device and the principle assumption diagram controlling aircraft thereof,
The current location information (longitude and latitude and translational speed) of the collection locating module 5 that the data acquisition unit of telechiric device is real-time, and by after the treated device process of positional information that gathers, send to controlled aircraft by FSK transceiver;
When the positional information that aircraft response FSK transceiver sends; The master control borad module that aircraft self carries simulates the mobile message of terminal remote control device by computing, simultaneously by the GPS module that aircraft carries, obtain the positional information that aircraft is current; Aircraft in conjunction with self current positional information, calculates target location according to the displacement information of telechiric device, and controls aircraft and move to target location.
As the distortion of Fig. 5,6 schemes,
Telechiric device is also provided with height sensor, current location information (the longitude and latitude of the collection locating module that the data acquisition unit of telechiric device is real-time, translational speed) and the upper and lower displacement amount relative to place reference field of remote control equipment, and by after the treated device process of positional information of collection, send to controlled aircraft by FSK transceiver;
When the positional information that aircraft response FSK transceiver sends; The master control borad that aircraft self carries simulates the mobile message (horizontal direction of terminal remote control device by computing, the displacement of vertical direction), simultaneously by the GPS module that aircraft carries, and height sensor obtains the current positional information of aircraft; Aircraft in conjunction with self current positional information, calculates target location according to the displacement information of telechiric device, and controls aircraft and move to target location.What also can realize aircraft follows object.
Fig. 7 is the another kind distortion of prior art scheme:
Fig. 7 is telechiric device and the Electricity Functional module diagram of the aircraft controlled.
Telechiric device is provided with locating module, height sensor; Aircraft is equipped with GPS module, height sensor and monopod video camera; The monopod video camera that aircraft carries makes its camera lens aim at telechiric device all the time;
Current location information (the longitude and latitude of the collection locating module that the data acquisition unit of telechiric device is real-time, translational speed) and the upper and lower displacement amount relative to place reference field of remote control equipment, and by after the treated device process of positional information of collection, send to controlled aircraft by FSK transceiver;
When the positional information that aircraft response FSK transceiver sends; The master control borad that aircraft self carries simulates the mobile message (horizontal direction of terminal remote control device by computing, the displacement of vertical direction), simultaneously by the GPS module that aircraft carries, and height sensor obtains the current positional information of aircraft; The displacement information of aircraft foundation telechiric device is in conjunction with self current positional information, and the target location of calculating aircraft and the anglec of rotation of camera lens, control aircraft moves to target location and makes platform-lens point to telechiric device simultaneously.
Technology illustrates:
Adopt 2.4G FSK transceiver to carry out information exchange between telechiric device and aircraft in such scheme.In such scheme, the positional information that aircraft response FSK transceiver sends refers to and performs the positional information that aircraft effectively utilizes FSK transceiver and sends aircraft and follow telechiric device.
Locating module in such scheme can be used for accepting gps signal, Beidou navigation signal and/or GLONASS signal.
Technique effect:
Technique scheme be based in operator's hand/locating module carried with, positional information can be issued controlled aircraft by FSK transceiver by this locating module, the order that what aerocraft real performed is " flying to here ".So namely, achieve unmanned vehicle to follow operator and move, greatly improve the experience sense of operator.
Above-mentioned example, only for technical conceive of the present utility model and feature are described, its object is to person skilled in the art can be understood content of the present utility model and implement according to this, can not limit protection domain of the present utility model with this.All equivalent transformations of doing according to the utility model Spirit Essence or modification, all should be encompassed within protection domain of the present utility model.
Claims (10)
1. a terminal remote control device, is characterized in that: have
For controlling the parts of aircraft movement; Master control board; Described master control board is provided with the processor for the treatment of data; Described terminal remote control device also has: FSK transceiver; Locating module; Data acquisition module; The current location information of locating module described in described data collecting module collected sends to described FSK transceiver by described processor process.
2. device as claimed in claim 1, is characterized in that:
Be handle or button for controlling the described parts of aircraft movement.
3. device as claimed in claim 1, is characterized in that:
Described FSK transceiver is the FSK transceiver adopting 2.4GHz.
4. device as claimed in claim 1, is characterized in that:
The information of the described locating module of collection that described data acquisition module is real-time, sends to controlled aircraft by the timing of described FSK transceiver.
5. device as claimed in claim 1, is characterized in that: described locating module is used for accepting gps signal, Beidou navigation signal and/or GLONASS signal.
6. device as claimed in claim 1, is characterized in that:
Described locating module is built in described terminal remote control device.
7. device as claimed in claim 1, is characterized in that:
Described locating module makes lip pencil or USB flash disk shape is external in described terminal remote control device.
8. device as claimed in claim 1, is characterized in that:
Described device is made and is carried with lip pencil, cuboid for operator.
9. device as claimed in claim 1, is characterized in that:
Described device also includes the height sensor for measuring height.
10. device as claimed in claim 1, is characterized in that:
Described remote terminal also comprises intelligent terminal module, and the Flight Condition Data of the described aircraft received is sent to described intelligent terminal module by described control data collector.
Priority Applications (1)
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CN201520076007.1U CN204679772U (en) | 2015-02-03 | 2015-02-03 | Terminal remote control device |
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CN201520076007.1U CN204679772U (en) | 2015-02-03 | 2015-02-03 | Terminal remote control device |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104656482A (en) * | 2015-02-03 | 2015-05-27 | 昆山优力电能运动科技有限公司 | Terminal remote control device |
CN104808686A (en) * | 2015-04-28 | 2015-07-29 | 零度智控(北京)智能科技有限公司 | System and method enabling aircraft to be flied along with terminal |
-
2015
- 2015-02-03 CN CN201520076007.1U patent/CN204679772U/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104656482A (en) * | 2015-02-03 | 2015-05-27 | 昆山优力电能运动科技有限公司 | Terminal remote control device |
CN104808686A (en) * | 2015-04-28 | 2015-07-29 | 零度智控(北京)智能科技有限公司 | System and method enabling aircraft to be flied along with terminal |
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Effective date of registration: 20160720 Address after: Jinxi town foxlink Kunshan road 215324 Suzhou City, Jiangsu province No. 388 Patentee after: KUNSHAN YOUNI ELECTRIC ENERGY SPORTS TECHNOLOGY CO., LTD. Address before: Hongkong Hongguang Road No. 1, Kowloon Bay China billion centre 10 floor Patentee before: You Li Science and Technology Ltd. |