CN104238382A - Remote control system and aircraft control system thereof - Google Patents
Remote control system and aircraft control system thereof Download PDFInfo
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- CN104238382A CN104238382A CN201310234037.6A CN201310234037A CN104238382A CN 104238382 A CN104238382 A CN 104238382A CN 201310234037 A CN201310234037 A CN 201310234037A CN 104238382 A CN104238382 A CN 104238382A
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 41
- 238000004891 communication Methods 0.000 claims abstract description 38
- 238000012545 processing Methods 0.000 claims description 9
- 230000000153 supplemental effect Effects 0.000 claims description 6
- 230000008901 benefit Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 230000002776 aggregation Effects 0.000 description 1
- 238000004220 aggregation Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000001502 supplementing effect Effects 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
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Abstract
The invention discloses a remote control system and an aircraft control system of the remote control system. The remote control system comprises a mobile terminal. The mobile terminal comprises a first communication chip. The remote control system further comprises a control data acquisition unit. The control data acquisition unit comprises a processor, multiple remote control levers and multiple remote control switches, wherein the processor collects flight control data input by users through the remote control levers and the remote control switches. The control data acquisition unit transmits the flight control data to the mobile terminal. The first communication chip transmits the flight control data to an external device. The aircraft control system comprises a model aircraft and the remote control system. By the adoption of the remote control system and the aircraft control system, the flight control accuracy is high, the operability is good, and meanwhile the high performance and various achievements of resources related to an existing mobile terminal are utilized, so that a high-performance and low-cost control scheme is realized.
Description
Technical field
The present invention relates to a kind of telechirics and flight control system thereof, particularly relate to a kind of telechirics and flight control system thereof of the state of flight for Controlling model aircraft.
Background technology
At present model aerial vehicle on the market, main control mode is two kinds: the scheme of dedicated remote control combination model aircraft and smart mobile phone or panel computer combination model aircraft scheme.
Wherein the scheme of dedicated remote control aggregation model aircraft is the traditional control program of model aerial vehicle.Telepilot contains operating grip and controls expelling plate etc.Telepilot is due to the restriction of volume and cost, and generally not or only have several simple lampion or very little instruction screen to carry out the duty of display remote controller, remote-transmitter plate generally also only has simple single-chip microcomputer support performance.Thus result of use is restricted.Even if some high-end remote configuration high-resolution display and powerful CPU(central processing unit) even also built-in operating system.But the price of a whole set of telepilot is very expensive.
Wherein smart mobile phone or panel computer combination model aircraft scheme utilize existing smart mobile phone etc. to use as the telepilot of model aerial vehicle, and its advantage is that cost is low, and this is owing to directly using existing smart mobile phone, so decrease the cost of telepilot; And powerful, the operating system of smart mobile phone can complete various parameter designing, and can utilize existing smart mobile phone display screen.But its shortcoming is when manipulating aircraft, owing to there is no the remote-control handle of specialty, to the performance accuracy of aircraft and operability all far short of what is expected.And the performance accuracy of model aerial vehicle and operability are the use senses that aircraft personnel mainly pursue that uses a model, so described scheme seriously affects the use sense of operator.
Summary of the invention
The technical problem to be solved in the present invention is the remote control mode of model aerial vehicle in order to overcome prior art otherwise cost is high, otherwise the defect of operability difference, a kind of telechirics and flight control system thereof are provided, present invention utilizes the related resource of existing mobile terminal, add the remote control handset of specialty simultaneously, thus realize high-performance, the control program of low cost.
The present invention solves above-mentioned technical matters by following technical proposals:
The invention provides a kind of telechirics, comprise a mobile terminal, described mobile terminal comprises one first communication chip, be characterized in, described telechirics also comprises a control data collector, described control data collector comprises a processor, multiple remote-control lever and multiple teleswitch, wherein said processor gathers the flight control data of user's input by described remote-control lever and described teleswitch, described flight control data is sent to described mobile terminal by a blue tooth interface by wherein said control data collector, described flight control data is sent to external unit by the first communication chip of described mobile terminal.
Flight control data described in the present invention is the flight attitude of Controlling model aircraft in prior art or the frequently-used data instruction of state, is just no longer described in detail herein.
Preferably, described control data collector is by a USART(universal synchronous/asynchronous serial reception/transmitter) interface, an I
2c interface (Inter-Integrated Circuit, twin wire universal serial bus) or a USB(USB (universal serial bus)) interface replaces described blue tooth interface and described flight control data is sent to described mobile terminal.
Can also no longer adopt blue tooth interface and adopt USART interface, I in the present invention
2c interface or USB interface send flight control data.
Preferably, described mobile terminal also comprises a display screen, and described first communication chip is also for receiving Flight Condition Data, and described display screen shows described Flight Condition Data.
Flight Condition Data described in the present invention is model aerial vehicle collection the signal data of state of flight for characterization model aircraft in prior art.
Preferably, described first communication chip is WIFI(wireless fidelity, Wireless Fidelity) communication chip.
Preferably, described mobile terminal is mobile phone or panel computer.
Mobile terminal described in the present invention can be mobile phone or the computer formation at random in prior art with communication chip, so the mobile terminal in the present invention can be the iphone mobile phone of Apple, such as iphone4s mobile phone or iphone4 mobile phone etc., or the ipad panel computer of Apple or ipad2 panel computer.
Present invention also offers a kind of flight control system, it comprises a model aerial vehicle, described model aerial vehicle comprises one of state of flight for controlling described model aerial vehicle and flies to control plate, be characterized in, described flight control system also comprises a telechirics as above, the wherein said control plate that flies also comprises a third communication chip, described in fly to control the state of flight that described flight control data that plate also received by described third communication chip controls described model aerial vehicle.
Preferably, described in fly to control plate and also gather the Flight Condition Data of described model aerial vehicle, and by described third communication chip, described Flight Condition Data is sent to described telechirics.
The control plate that flies in the present invention not only can based on the state of flight of control signal Controlling model aircraft, the duty of all parts in all right collection model aircraft.
Preferably, described third communication chip is WIFI communication chip or 2.4G ISM FSK transceiver.
Now, in the present invention, only mobile terminal carries out mutual equipment as with external device, and all flight control data all first transfer to mobile terminal, then transfer to external unit.
Preferably, a video processing module, a memory module, a load module is also comprised in mobile terminal as above;
Wherein said video processing module is used for that Flight Condition Data and/or video data are converted into display and exports described display screen to;
Described memory module is for storing described Flight Condition Data and/or described video data;
Described load module for reading in the parameter of input, and generates state of flight configuration parameter based on described parameter, and is sent to external unit by described first communication chip.
Video processing module described in the present invention, memory module and load module are parts usual in mobile terminal, so be no longer described in detail it herein.
Preferably, also comprise a voice synthetic module and a loudspeaker in described mobile terminal, for Flight Condition Data is converted into voice signal, and exported by loudspeaker.
Preferably, a sound identification module and a microphone is also comprised in described mobile terminal, the audio controls that described sound identification module gathers based on described microphone, generates supplemental characteristic, and described load module also generates state of flight configuration parameter based on described supplemental characteristic.
Voice synthetic module described in the present invention, loudspeaker, sound identification module and microphone are usual parts or module in the mobile terminal of prior art equally, so be no longer described in detail herein.
For convenience of description, in the present invention, described mobile terminal is divided into various module according to function and describes respectively, so when implementing of the present invention, the function of each module can be realized in same or multiple software and/or hardware.
On the basis meeting this area general knowledge, above-mentioned each optimum condition, can combination in any, obtains the preferred embodiments of the invention.
Positive progressive effect of the present invention is:
The advantage of control data collector of the present invention, telechirics and flight control system thereof is the operating grip of the telepilot of existing specialty, there is again the related resource utilizing mobile terminal, so achieve flight control accuracy high, the high-performance of the related resource of existing mobile terminal and multiple realization is make use of while good operability, thus achieve high-performance, the control program of low cost.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment 1 of flight control system of the present invention.
Fig. 2 is the structural representation of the mobile terminal of embodiments of the invention 1.
Fig. 3 is the structural representation of the control data collector of embodiments of the invention 1.
Embodiment
Mode below by embodiment further illustrates the present invention, but does not therefore limit the present invention among described scope of embodiments.
Embodiment 1:
Flight control system described in the present embodiment as shown in Figure 1, comprises telechirics 1 and a model aerial vehicle 2, and wherein said telechirics 1 comprises control data collector 11 and a mobile terminal 12.
And as shown in Figure 2, the described control data collector 11 of the present embodiment comprises a processor 111 and two remote-control levers 112 and two teleswitches 113.
Wherein said processor 111 gathers the operation of user to described remote-control lever 112 and described teleswitch 113, and the signal that the operation of described user to described remote-control lever 112 and described teleswitch 113 generates constitutes the flight control data of Controlling model aircraft.
In addition the quantity of described remote-control lever 112 and teleswitch 113 can be arranged arbitrarily based on the needs of realistic model flying vehicles control order, is not limited in the quantity in the present embodiment.
The mobile terminal 12 of the present embodiment as shown in Figure 3, comprises a video processing module 121a, a display screen 121b, memory module 122, load module 123, voice synthetic module 125, loudspeaker 126, sound identification module 127, microphone 128 and a WIFI communication chip 129.
Wherein said video processing module 121a is used for Flight Condition Data to be converted into the display screen 121b that display exports described mobile terminal 12 to, and described display screen 121b correspondingly shows.Described memory module 122 is for storing described Flight Condition Data.Described load module 125 for reading in the parameter of input, and generates state of flight configuration parameter based on described parameter, is then sent to model aerial vehicle by described WIFI communication chip 129.The configuration parameter of state of flight described in the present embodiment is used for adjusting Flight Condition Data and supplementing.
Described voice synthetic module 125 is for being converted into voice signal by Flight Condition Data and exporting outside to by loudspeaker 126, thus user can hear the voice signal of the content comprising Flight Condition Data.
The audio controls that described sound identification module 127 gathers based on described microphone 128, generates supplemental characteristic, and described load module 123 also generates state of flight configuration parameter based on described supplemental characteristic.
The communication chip of WIFI described in the present embodiment 129 is for carrying out data interaction with model aerial vehicle 2.
Wherein the mobile terminal 2 of the present embodiment adopts the iphone mobile phone or the ipad panel computer that comprise the Apple of above-mentioned module, can adopt in addition and there is iOS, Android(Android), Symbian(Saipan) etc. the mobile phone of intelligent system or panel computer, and correspondingly configure mobile terminal 2 described in rear formation the present embodiment.
As shown in Figure 1, described model aerial vehicle 2 comprises one and flies to control plate 21, the wherein said control plate that flies comprises a WIFI communication chip 211, described WIFI communication chip 211 mates to the WIFI communication chip 129 in mobile terminal 12 and carries out corresponding data interaction, namely sets up data link between described WIFI communication chip 211 and described WIFI communication chip 129.Wherein said flying controls plate 21 based on the flare maneuver of the flight control data Controlling model aircraft 2 received, and the correspondingly Flight Condition Data that forms of the status data of all parts of collection model aircraft 2.
In addition mobile terminal 12 described in the present embodiment and transmit flight control data by a blue tooth interface between described control data collector 11, user can also adopt the high speed data transmission interfaces such as USB interface to transmit described flight control data in addition.
As shown in Figure 1, the flow process of the data transmission of the present embodiment is as follows:
The described processor 111 of first described control data collector 11 gathers the flight control data that the operation of user to described remote-control lever 112 and described teleswitch 113 generates.
Then described flight control data is transferred to mobile terminal 12 by blue tooth interface by described processor 111.Meanwhile, in described mobile terminal 12, load module 123, voice synthetic module 125, loudspeaker 126, sound identification module 127 and microphone 128 collaborate generate state of flight configuration parameter.
After this WIFI communication chip 129 of described mobile terminal 12 sends described flight control data or flight control data and the state of flight configuration parameter WIFI communication chip 211 flying to control plate 21 to the model aerial vehicle 2 of coupling.
Then fly described in control the flight control data of plate 21 based on reception or the flare maneuver of flight control data and state of flight configuration parameter Controlling model aircraft 2, meanwhile, fly control plate 21 described in and also by described WIFI communication chip 211, the Flight Condition Data of model aerial vehicle is sent to the WIFI communication chip 129 mated with it.
Finally, the Flight Condition Data that described WIFI communication chip 129 receives is converted into the display screen 121b that display exports described mobile terminal 12 to by the video processing module 121a of described mobile terminal 12, and then described display screen 121b correspondingly shows.
Although the foregoing describe the specific embodiment of the present invention, it will be understood by those of skill in the art that these only illustrate, protection scope of the present invention is defined by the appended claims.Those skilled in the art, under the prerequisite not deviating from principle of the present invention and essence, can make various changes or modifications to these embodiments, but these change and amendment all falls into protection scope of the present invention.
Claims (11)
1. a telechirics, comprise a mobile terminal, described mobile terminal comprises one first communication chip, it is characterized in that, described telechirics also comprises a control data collector, and described control data collector comprises a processor, multiple remote-control lever and multiple teleswitch;
Wherein said processor gathers the flight control data of user's input by described remote-control lever and described teleswitch; Described flight control data is sent to described mobile terminal by a blue tooth interface by described control data collector, and described flight control data is sent to external unit by described first communication chip.
2. telechirics as claimed in claim 1, is characterized in that, described control data collector is by a USART interface, I
2c interface or a USB interface replace described blue tooth interface and described flight control data are sent to described mobile terminal.
3. telechirics as claimed in claim 1, it is characterized in that, described mobile terminal also comprises a display screen, and described first communication chip is also for receiving Flight Condition Data, and described display screen shows described Flight Condition Data.
4. telechirics as claimed in claim 1, it is characterized in that, described first communication chip is WIFI communication chip.
5. telechirics as claimed in claim 1, it is characterized in that, described mobile terminal is mobile phone or panel computer.
6. the telechirics according to any one of claim 1-5, is characterized in that, also comprises a video processing module, a memory module and a load module in described mobile terminal;
Wherein said video processing module is used for that described Flight Condition Data and/or described video data are converted into display and exports described display screen to;
Described memory module is for storing described Flight Condition Data and/or described video data;
Described load module for reading in the parameter of input, and generates described state of flight configuration parameter based on described parameter, and is sent to external unit by described first communication chip.
7. telechirics as claimed in claim 6, be is characterized in that, also comprise a voice synthetic module and a loudspeaker in described mobile terminal, for described Flight Condition Data is converted into voice signal, and exported by loudspeaker.
8. telechirics as claimed in claims 6 or 7, it is characterized in that, a sound identification module and a microphone is also comprised in described mobile terminal, the audio controls that described sound identification module gathers based on described microphone, generate supplemental characteristic, described load module also generates described state of flight configuration parameter based on described supplemental characteristic.
9. a flight control system, it comprises a model aerial vehicle, described model aerial vehicle comprises one of state of flight for controlling described model aerial vehicle and flies to control plate, it is characterized in that, described flight control system also comprises just like the telechirics described in any one of claim 1-8, the wherein said control plate that flies also comprises a third communication chip, described in fly to control the state of flight that described flight control data that plate also received by described third communication chip controls described model aerial vehicle.
10. flight control system as claimed in claim 9, is characterized in that, described in fly to control the Flight Condition Data that plate also gathers described model aerial vehicle, and by described third communication chip, described Flight Condition Data is sent to described telechirics.
11. flight control systems as described in claim 9 or 10, it is characterized in that, described third communication chip is WIFI communication chip or 2.4G ISM FSK transceiver.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201310234037.6A CN104238382A (en) | 2013-06-13 | 2013-06-13 | Remote control system and aircraft control system thereof |
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| CN201310234037.6A CN104238382A (en) | 2013-06-13 | 2013-06-13 | Remote control system and aircraft control system thereof |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104714552A (en) * | 2015-03-11 | 2015-06-17 | 郑州航空工业管理学院 | Four-rotor aircraft based on mobile phone real-time monitoring |
| CN104765309A (en) * | 2015-04-08 | 2015-07-08 | 何春旺 | Remote controller, remote control driving device and remote control driving device control system and method thereof |
| CN104950771A (en) * | 2015-06-26 | 2015-09-30 | 哈瓦国际航空技术（深圳）有限公司 | Handheld ground station control system for UAV (unmanned aerial vehicle) |
| CN105446179A (en) * | 2015-11-05 | 2016-03-30 | 深圳市几米软件有限公司 | Automotive monitoring system and method based on CAN-BUS and intelligent vehicle-mounted equipment |
| CN107071327A (en) * | 2016-12-07 | 2017-08-18 | 国网山东省电力公司电力科学研究院 | A kind of programmable portable mobile wireless vision signal and Digital Signals all-in-one |
| CN108170156A (en) * | 2016-12-07 | 2018-06-15 | 广州亿航智能技术有限公司 | Flight state output method and device based on intelligent terminal |
| CN109445464A (en) * | 2019-01-08 | 2019-03-08 | 深圳市道通智能航空技术有限公司 | A kind of flight control method and flight control system |
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| CN108170156A (en) * | 2016-12-07 | 2018-06-15 | 广州亿航智能技术有限公司 | Flight state output method and device based on intelligent terminal |
| CN109445464A (en) * | 2019-01-08 | 2019-03-08 | 深圳市道通智能航空技术有限公司 | A kind of flight control method and flight control system |
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