CN203483857U - Remote control system and flight control system thereof - Google Patents
Remote control system and flight control system thereof Download PDFInfo
- Publication number
- CN203483857U CN203483857U CN201320338104.4U CN201320338104U CN203483857U CN 203483857 U CN203483857 U CN 203483857U CN 201320338104 U CN201320338104 U CN 201320338104U CN 203483857 U CN203483857 U CN 203483857U
- Authority
- CN
- China
- Prior art keywords
- control system
- flight
- remote control
- mobile terminal
- communication chip
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title claims abstract description 25
- 238000004891 communication Methods 0.000 claims abstract description 37
- 238000012545 processing Methods 0.000 claims description 8
- 230000000153 supplemental effect Effects 0.000 claims description 6
- 230000007474 system interaction Effects 0.000 claims description 2
- 230000008901 benefit Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 230000002650 habitual effect Effects 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 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
- 230000015572 biosynthetic process 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
- 230000013011 mating Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a remote control system and a flight control system thereof. The remote control system comprises a mobile terminal, wherein the mobile terminal comprises a first communication chip, the remote control system also comprises a control data acquisition unit, and the control data acquisition unit comprises a processor, a plurality of remote control rods and a plurality of remote control switches; and the processer acquires flight control data input by a user by the remote control rods and the remote control switches, the control data acquisition unit transmits the flight control data to the mobile terminal and the first communication chip transmits the flight control data to external equipment. The flight control system comprises a model flight vehicle and the remote control system. According to the utility model, flight control has high accuracy and good operability. In addition, high performances and many kinds of realization of relevant resources of the existing mobile terminal are applied in order to realize a high-performance and low-cost control scheme.
Description
Technical field
The utility model relates to a kind of remote control system and flight control system thereof, particularly relates to a kind of for controlling remote control system and the flight control system thereof of the state of flight of model aerial vehicle.
Background technology
Current 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.Remote controller contains operating grip and controls expelling plate etc.Remote controller, due to the restriction of volume and cost, does not generally have or only has several simple lampions or very little instruction screen to carry out the duty of display remote controller, and remote-transmitter plate generally also only has simple single-chip microcomputer support performance.Thereby result of use is restricted.Even 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 remote controller is very expensive.
Wherein smart mobile phone or panel computer combination model aircraft scheme utilize existing smart mobile phone etc. to use as the remote controller of model aerial vehicle, and its advantage is that cost is low, and this is owing to directly using existing smart mobile phone, so reduced the cost of remote controller; 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 controlling aircraft, owing to there is no professional remote-control handle, all far short of what is expected to the performance accuracy of aircraft and operability.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 operator's use sense.
Utility model content
The technical problems to be solved in the utility model be for overcome prior art model aerial vehicle remote control mode otherwise cost is high, otherwise the defect that operability is poor, a kind of remote control system and flight control system thereof are provided, the utility model has utilized the related resource of existing mobile terminal, added professional remote controller handle simultaneously, thereby realize high-performance, cheaply control program.
The utility model solves above-mentioned technical problem by following technical proposals:
The utility model provides a kind of remote control system, comprise a mobile terminal, described mobile terminal comprises one first communication chip, be characterized in, described remote control system also comprises a control data acquisition unit, described control data acquisition unit comprises a processor, a plurality of remote-control levers and a plurality of remote control switch, data are controlled in the flight that wherein said processor gathers user's input by described remote-control lever and described remote control switch, wherein said control data acquisition unit is controlled data by a blue tooth interface by described flight and is sent to described mobile terminal, the first communication chip of described mobile terminal is controlled data by described flight and is sent to external equipment.
It is in prior art, to control the frequently-used data instruction of flight attitude or the state of model aerial vehicle that data are controlled in flight described in the utility model, is just no longer described in detail herein.
Preferably, described control data acquisition unit is by USART(universal synchronous/asynchronous serial reception/transmitter) interface, an I
2c interface (Inter-Integrated Circuit, twin wire universal serial bus) or a USB(USB) interface replaces described blue tooth interface and described flight is controlled to data is sent to described mobile terminal.
In the utility model, can also no longer adopt blue tooth interface and adopt USART interface, I
2c interface or USB interface send flight and control data.
Preferably, described mobile terminal also comprises that one for showing the display screen of the Flight Condition Data that described the first communication chip receives.
Flight Condition Data described in the utility model is model aerial vehicle collection for the signal data of the state of flight of characterization model aircraft in prior art.
Preferably, described the 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 utility model can be that mobile phone or the computer at random in prior art with communication chip form, so the mobile terminal in the utility model 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.
The utility model also provides a kind of flight control system, it comprises a model aerial vehicle, described model aerial vehicle comprise for control described model aerial vehicle state of flight one fly to control plate, be characterized in, described flight control system also comprises a remote control system as above, wherein saidly fly to control plate and also comprise a third communication chip, described in fly to control plate also by described third communication chip and described remote control system interaction data.
Wherein saidly fly to control the state of flight that model aerial vehicle described in Data Control is controlled in described flight that plate receives by described third communication chip.Describedly 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 remote control system.
Flying in the utility model controlled plate not only can control based on control signal the state of flight of model aerial vehicle, 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 utility model, only mobile terminal is as carrying out mutual equipment with external device, and all flight is controlled data and all first transferred to mobile terminal, then transfers to external equipment.
Preferably, in mobile terminal as above, also comprise one for described Flight Condition Data and/or described video data are converted into video processing module that display exports described display screen to, for the memory module and of storing described Flight Condition Data and/or described video data for reading in the input module of the parameter of input.
Wherein said video processing module exports described display screen to for Flight Condition Data and/or video data are converted into display.
Described memory module is used for storing described Flight Condition Data and/or described video data.
Described input module is used for reading in the parameter of input, and generates state of flight configuration parameter based on described parameter, and is sent to external equipment by described the first communication chip.
Video processing module described in the utility model, memory module and input module are parts habitual in mobile terminal, so it is no longer described in detail herein.
Preferably, in described mobile terminal, also comprise that one for being converted into described Flight Condition Data the voice synthetic module of voice signal and the loudspeaker of the described voice signal of an output.
Preferably, in described mobile terminal, also comprise that one for being converted into the voice signal of described microphone collection sound identification module and a microphone of supplemental characteristic.The voice control signal that wherein said sound identification module gathers based on described microphone, generates supplemental characteristic, and described input module also generates state of flight configuration parameter based on described supplemental characteristic.
Voice synthetic module described in the utility model, loudspeaker, sound identification module and microphone are habitual 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 utility model, described mobile terminal is divided into various modules according to function and describes respectively, so when implementing the utility model, the function of each module can be realized in same or a plurality of software and/or hardware.
Meeting on the basis of this area general knowledge, above-mentioned each optimum condition, can be combined, and obtains each preferred embodiments of the utility model.
Positive progressive effect of the present utility model is:
The advantage of control data acquisition unit of the present utility model, remote control system and flight control system thereof is the operating grip of the remote controller of existing specialty, there is again the related resource that utilizes mobile terminal, so flight control accuracy is high having realized, high-performance and the multiple realization of the related resource of existing mobile terminal in the time of good operability, have been utilized, thereby realized high-performance, cheaply control program.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment 1 of flight control system of the present utility model.
Fig. 2 is the structural representation of the mobile terminal of embodiment 1 of the present utility model.
Fig. 3 is the structural representation of the control data acquisition unit of embodiment 1 of the present utility model.
The specific embodiment
Mode below by embodiment further illustrates the utility model, but therefore the utility model is not limited among described scope of embodiments.
Embodiment 1:
Flight control system described in the present embodiment as shown in Figure 1, comprises a remote control system 1 and a model aerial vehicle 2, and wherein said remote control system 1 comprises a control data acquisition unit 11 and a mobile terminal 12.
And as shown in Figure 2, the described control data acquisition unit 11 of the present embodiment comprises a processor 111 and two remote-control levers 112 and two remote control switches 113.
Wherein said processor 111 gathers the operation of user to described remote-control lever 112 and described remote control switch 113, and the signal that described user generates the operation of described remote-control lever 112 and described remote control switch 113 has formed the flight control data of controlling model aerial vehicle.
In addition the quantity of described remote-control lever 112 and remote control switch 113 can arrange arbitrarily by the needs based on realistic model aircraft control command, 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, a memory module 122, an input module 123, a voice synthetic module 125, a loudspeaker 126, a sound identification module 127, a microphone 128 and a WIFI communication chip 129.
Wherein said video processing module 121a is for being converted into by Flight Condition Data 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 input module 125 is for reading in the parameter of input, and generates state of flight configuration parameter based on described parameter, then by described WIFI communication chip 129, is sent to model aerial vehicle.The configuration parameter of state of flight described in the present embodiment is for adjusting and supplement Flight Condition Data.
Described voice synthetic module 125 is for Flight Condition Data being converted into voice signal and exporting outside to by loudspeaker 126, thereby user can hear the voice signal of the content that comprises Flight Condition Data.
The voice control signal that described sound identification module 127 gathers based on described microphone 128, generates supplemental characteristic, and described input 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 iphone mobile phone or the ipad panel computer of the Apple that comprises above-mentioned module, can adopt in addition and there is iOS, Android(Android), Symbian(Saipan) etc. mobile phone or the panel computer of intelligence system, and correspondingly configure mobile terminal 2 described in rear formation the present embodiment.
As shown in Figure 1, described model aerial vehicle 2 comprises that one flies to control plate 21, wherein saidly fly to control plate and comprise a WIFI communication chip 211, described WIFI communication chip 211 mates and carries out corresponding data interaction with the WIFI communication chip 129 in mobile terminal 12, between described WIFI communication chip 211 and described WIFI communication chip 129, sets up data link.Wherein said flying controlled the flare maneuver that data control model aircraft 2 is controlled in the flight of plate 21 based on receiving, and the Flight Condition Data that correspondingly status data of all parts of collection model aircraft 2 forms.
In addition between mobile terminal described in the present embodiment 12 and described control data acquisition unit 11, by a blue tooth interface transmission flight, control data, user can also adopt the high speed data transmission interfaces such as USB interface to transmit described flight and control data in addition.
As shown in Figure 1, the flow process of the transfer of data of the present embodiment is as follows:
The described processor 111 of first described control data acquisition unit 11 gathers the flight control data that user generates the operation of described remote-control lever 112 and described remote control switch 113.
Then described processor 111 is controlled data by described flight and is transferred to mobile terminal 12 by blue tooth interface.Meanwhile, in described mobile terminal 12, input module 123, voice synthetic module 125, loudspeaker 126, sound identification module 127 and the common cooperation of microphone 128 generate state of flight configuration parameter.
After this WIFI communication chip 129 of described mobile terminal 12 sends described flight and controls data or flight control data and state of flight configuration parameter to the WIFI communication chip 211 that flies to control plate 21 of the model aerial vehicle 2 of coupling.
Then described in, fly to control the flight of plate 21 based on receiving and control the flare maneuver that data or flight control data and state of flight configuration parameter are controlled model aerial vehicle 2, meanwhile, described in, fly to control plate 21 and also by described WIFI communication chip 211, the Flight Condition Data of model aerial vehicle is sent to the WIFI communication chip 129 mating with it.
Finally, the Flight Condition Data that the video processing module 121a of described mobile terminal 12 receives described WIFI communication chip 129 is converted into the display screen 121b that display exports described mobile terminal 12 to, and then described display screen 121b correspondingly shows.
Although more than described the specific embodiment of the present utility model, it will be understood by those of skill in the art that these only illustrate, protection domain of the present utility model is limited by appended claims.Those skilled in the art is not deviating under the prerequisite of principle of the present utility model and essence, can make various changes or modifications to these embodiments, but these changes and modification all fall into protection domain of the present utility model.
Claims (10)
1. a remote control system, comprise a mobile terminal, described mobile terminal comprises one first communication chip, it is characterized in that, described remote control system also comprises a control data acquisition unit, and described control data acquisition unit comprises a processor, a plurality of remote-control lever and a plurality of remote control switch;
Data are controlled in the flight that wherein said processor gathers user's input by described remote-control lever and described remote control switch; Described control data acquisition unit is controlled data by a blue tooth interface by described flight and is sent to described mobile terminal, and described the first communication chip is controlled data by described flight and is sent to external equipment.
2. remote control system as claimed in claim 1, is characterized in that, described control data acquisition unit is by a USART interface, I
2c interface or a USB interface replace described blue tooth interface described flight control data are sent to described mobile terminal.
3. remote control system as claimed in claim 1, is characterized in that, described mobile terminal also comprises that one for showing the display screen of the Flight Condition Data that described the first communication chip receives.
4. remote control system as claimed in claim 1, is characterized in that, described the first communication chip is WIFI communication chip.
5. remote control system as claimed in claim 1, is characterized in that, described mobile terminal is mobile phone or panel computer.
6. the remote control system as described in any one in claim 1-5, it is characterized in that, in described mobile terminal, also comprise one for described Flight Condition Data and/or a video data are converted into video processing module that display exports described display screen to, for the memory module and of storing described Flight Condition Data and/or described video data for reading in the input module of the parameter of input.
7. remote control system as claimed in claim 6, is characterized in that, also comprises that one for being converted into described Flight Condition Data the voice synthetic module of voice signal and the loudspeaker of the described voice signal of an output in described mobile terminal.
8. remote control system as claimed in claim 6, is characterized in that, also comprises that a microphone and is converted into the sound identification module of supplemental characteristic by the voice signal of described microphone collection in described mobile terminal.
9. a flight control system, it comprises a model aerial vehicle, described model aerial vehicle comprise for control described model aerial vehicle state of flight one fly to control plate, it is characterized in that, described flight control system also comprises just like the remote control system described in claim 1-8 any one, wherein saidly fly to control plate and also comprise a third communication chip, described in fly to control plate also by described third communication chip and described remote control system interaction data.
10. flight control system as claimed in claim 9, 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 |
|---|---|---|---|
| CN201320338104.4U CN203483857U (en) | 2013-06-13 | 2013-06-13 | Remote control system and flight control system thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320338104.4U CN203483857U (en) | 2013-06-13 | 2013-06-13 | Remote control system and flight control system thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203483857U true CN203483857U (en) | 2014-03-19 |
Family
ID=50254720
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320338104.4U Expired - Lifetime CN203483857U (en) | 2013-06-13 | 2013-06-13 | Remote control system and flight control system thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203483857U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103977569A (en) * | 2014-05-16 | 2014-08-13 | 苏州云远网络技术有限公司 | Mobile phone vertical lifting aircraft |
| WO2014198189A1 (en) * | 2013-06-13 | 2014-12-18 | Tian Yu | Smart display remote control and flight control system |
| CN104238382A (en) * | 2013-06-13 | 2014-12-24 | 昊翔电能运动科技(昆山)有限公司 | Remote control system and aircraft control system thereof |
| CN104958915A (en) * | 2014-07-04 | 2015-10-07 | 株式会社万代 | Show output toy |
-
2013
- 2013-06-13 CN CN201320338104.4U patent/CN203483857U/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014198189A1 (en) * | 2013-06-13 | 2014-12-18 | Tian Yu | Smart display remote control and flight control system |
| CN104238382A (en) * | 2013-06-13 | 2014-12-24 | 昊翔电能运动科技(昆山)有限公司 | Remote control system and aircraft control system thereof |
| CN103977569A (en) * | 2014-05-16 | 2014-08-13 | 苏州云远网络技术有限公司 | Mobile phone vertical lifting aircraft |
| CN104958915A (en) * | 2014-07-04 | 2015-10-07 | 株式会社万代 | Show output toy |
| CN104958915B (en) * | 2014-07-04 | 2017-05-10 | 株式会社万代 | Show output toy |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104238382A (en) | Remote control system and aircraft control system thereof | |
| CN203414817U (en) | A remote control system and an aircraft control system thereof | |
| CN203350718U (en) | Remote control system and aircraft control system thereof | |
| CN108459982B (en) | Communication equipment and switching method of USB and serial port | |
| CN104238564A (en) | Remote control system and aircraft control system thereof | |
| CN102314764B (en) | Remote terminal, method for realizing remote control and system | |
| CN104238469A (en) | Flight vehicle control system | |
| CN203414782U (en) | An aircraft control system | |
| CN203483857U (en) | Remote control system and flight control system thereof | |
| CN102637353A (en) | System and method for home appliance wireless remote control based on mobile terminal | |
| CN104238551A (en) | Intelligent display remote control and flight control system | |
| CN203490821U (en) | Intelligent display remote controller and flight control system | |
| CN103607658A (en) | Method for inputting character into application software of intelligent television by utilizing mobile terminal | |
| CN104238561A (en) | Remote control system and aircraft control system thereof | |
| WO2019129229A1 (en) | Data aggregation and transmission device for mobile terminal | |
| CN209149566U (en) | Unmanned controller based on android system | |
| CN202472276U (en) | Environment-friendly data acquisition instrument based on Linux operating system | |
| CN204992154U (en) | Smart jack and system with wireless interactive function | |
| CN205751226U (en) | Learning type infrared remote control device based on intelligent mobile terminal | |
| CN204155123U (en) | A kind of mobile phone shields synchronous device together with automobile wireless is interconnected | |
| CN202654719U (en) | Remote control toy device | |
| CN206164757U (en) | Touch display device and screen transmission system | |
| CN203490829U (en) | Intelligent infrared integration control terminal equipment | |
| CN202679350U (en) | Onboard ultrashort wave radio station simulation training device | |
| CN203416248U (en) | A wireless display terminal |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: YOULI TECHNOLOGY CO., LTD. Free format text: FORMER OWNER: YUNEEC INTERNATIONAL CO.,LTD. Effective date: 20150708 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20150708 Address after: Hongkong Hongguang Road No. 1, Kowloon Bay China billion centre 10 floor Patentee after: YUNEEC TECHNOLOGY Co.,Ltd. Address before: Jinxi town Wei Road in Kunshan city Suzhou city Jiangsu province 215324 No. 388 Patentee before: HAOXIANG ELECTRIC ENERGY (KUNSHAN) Co.,Ltd. |
|
| CX01 | Expiry of patent term |
Granted publication date: 20140319 |
|
| CX01 | Expiry of patent term |