CN203414817U - A remote control system and an aircraft control system thereof - Google Patents
A remote control system and an aircraft control system thereof Download PDFInfo
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- CN203414817U CN203414817U CN201320339656.7U CN201320339656U CN203414817U CN 203414817 U CN203414817 U CN 203414817U CN 201320339656 U CN201320339656 U CN 201320339656U CN 203414817 U CN203414817 U CN 203414817U
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Abstract
The utility model discloses a remote control system and an aircraft control system thereof. The remote control system comprises an intelligent terminal module and a control unit. The intelligent terminal module includes a second communication chip. The control unit comprises a control data collector and a first communication chip. The control data collector is used for acquiring flight control data controlling a model aircraft. The second communication chip receives the video data of the model aircraft. The first communication chip of the control unit transmits received flight status data of the model aircraft to the intelligent terminal module. The aircraft control system also comprises a model aircraft and the above remote control system. While achieving high flight control precision and good operability, the remote control system utilizes the high performance and the multiple achieving modes of the intelligent terminal module so as to achieve a control scheme with high performance.
Description
Technical field
The utility model relates to a kind of telechirics and flight control system thereof, particularly relates to a kind of for controlling telechirics 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.Telepilot contains operating grip and controls expelling plate etc.Telepilot, 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.So described scheme is difficult to improve operator's use sense.
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 reduced 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 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 is in order to overcome the defect of the poor and function singleness of the remote control mode operability of model aerial vehicle of prior art, a kind of telechirics and flight control system thereof are provided, the utility model is by the combination of intelligent terminal module and professional telepilot handle, thereby realizes high performance control program.
The utility model solves above-mentioned technical matters by following technical proposals:
The utility model provides a kind of telechirics, be characterized in comprising an intelligent terminal module, described intelligent terminal module comprises a second communication chip, described telechirics also comprises a control module, described control module comprises that one for gathering control data acquisition unit and one first communication chip of the flight control data of controlling a model aerial vehicle, and described second communication chip receives the video data of described model aerial vehicle; The first communication chip of described control module is also sent to described intelligent terminal module by the Flight Condition Data of the described model aerial vehicle receiving.
Preferably, described control data acquisition unit comprises a processor, a plurality of remote-control lever and a plurality of teleswitch;
Data are controlled in the flight that wherein said processor gathers user's input by described remote-control lever and described teleswitch.
Preferably, described the first communication chip is 2.4G/5.8G ISM FSK transceiver.
Preferably, described control module is by a USART interface, a USB interface, an I
2c interface or a SPI interface are sent to described intelligent terminal module by described Flight Condition Data.
Preferably, described intelligent terminal module also comprises that one for showing the display screen of Flight Condition Data and/or video data.
Preferably, described second communication chip is WIFI communication chip, 3G communication chip or 4G communication chip.
Preferably, in described intelligent terminal module, 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 load module of the parameter of input.
Preferably, in described intelligent terminal module, 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 intelligent terminal module, 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 utility model also provides a kind of flight control system, it comprises a model aerial vehicle, described model aerial vehicle comprise for gather described model aerial vehicle Flight Condition Data one fly to control plate and for gathering a video acquisition plate of video data, be characterized in that described flight control system also comprises a telechirics as above, wherein saidly fly to control plate and also comprise a third communication chip, described in fly to control plate by described third communication chip and described telechirics interaction data;
Described video acquisition plate also comprises one the 4th communication chip, and described video acquisition plate is by described the 4th communication chip and described telechirics interaction data;
When the communication link of described third communication chip and described telechirics disconnects, described in fly to control plate by the 4th communication chip of described video acquisition plate and the second communication chip interaction data of described telechirics.
Preferably, described third communication chip is 2.4G ISM FSK transceiver, and described the 4th communication chip is WIFI communication chip, 3G communication chip or 4G communication chip.
Preferably, described video acquisition plate by a serial communication interface with described in fly to control plate interaction data.
Preferably, described serial communication interface is USART interface, SPI interface, RS232 interface or RS485 interface.
That is to say, the utility model provides a kind of telechirics, be characterized in, comprise an intelligent terminal module, described intelligent terminal module comprises a second communication chip, described telechirics also comprises a control module, and described control module comprises that one for gathering control data acquisition unit and one first communication chip of the flight control data of controlling a model aerial vehicle, and described second communication chip receives the video data of described model aerial vehicle; The first communication chip of described control module is also sent to described intelligent terminal module by the Flight Condition Data of the described model aerial vehicle receiving.
Wherein, described control data acquisition unit comprises a processor, a plurality of remote-control lever and a plurality of teleswitch;
Data are controlled in the flight that wherein said processor gathers user's input by described remote-control lever and described teleswitch.
Wherein, described the first communication chip is also for receiving Flight Condition Data.
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.
Wherein, described the first communication chip is 2.4G/5.8G ISM(Industrial Scientific Medical Band industry scientific research medicine frequency range) FSK(frequency shift keying) transceiver.
Wherein, described control module is by USART(universal synchronous/asynchronous serial reception/transmitter) interface, a USB(USB (universal serial bus)) interface, an I
2c interface (Inter-Integrated Circuit, twin wire universal serial bus) or a SPI interface (high-speed synchronous serial port) are sent to described intelligent terminal module by described Flight Condition Data.
Wherein, described intelligent terminal module also comprises a display screen; Described display screen shows described Flight Condition Data and/or video data.
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.
Wherein, described intelligent terminal module is also for generating a state of flight configuration parameter;
Described control module receives described state of flight configuration parameter, and by the first communication chip, described state of flight configuration parameter and flight control data is sent to model aerial vehicle jointly.
The configuration parameter of state of flight described in the utility model can be user pass through that intelligent terminal module inputs to flight control the supplementary parameter data of data, the supplemental characteristic of state of flight of allocation models aircraft, the supplemental characteristic of user preset or for the state of flight based on model aerial vehicle by supplemental characteristics such as experimental formulas.In the utility model, do not limit the content of described state of flight configuration parameter, the cognitive relevant parameter such as any and flight attitude, state and control of those skilled in the art all can be used as described state of flight configuration parameter of the present utility model.
Wherein, described second communication chip is WIFI(wireless fidelity Wireless Fidelity) communication chip, the 3G(third generation communication technology) communication chip or 4G(the 4th generation communication technology) communication chip etc.
The utility model also provides a kind of flight control system, it comprises a model aerial vehicle, described model aerial vehicle comprise for gather described model aerial vehicle Flight Condition Data one fly to control plate and for gathering a video acquisition plate of video data, be characterized in, described flight control system also comprises a telechirics as above, wherein saidly fly to control plate and also comprise a third communication chip, described in fly to control the described flight that described telechirics that plate receives by described third communication chip sends and control data;
Described video acquisition plate also comprises one the 4th communication chip, and described video acquisition plate is delivered to described telechirics by described the 4th communication chip by described video data transmitting.
Described in the utility model, fly to control the third communication chip of plate and the first communication chip of telechirics establishes the link relation, the second communication chip of the 4th communication chip of described video acquisition plate and the intelligent terminal module of telechirics establishes the link relation.So flight is controlled data and only transferred to third communication chip by the first communication chip, same video data also only transfers to second communication chip by the 4th communication chip.
Wherein, describedly fly to control plate and also by described third communication chip, described Flight Condition Data is sent to described telechirics, described third communication chip also receives by described the first communication chip the state of flight that state of flight configuration parameter that described intelligent terminal module generates is controlled model aerial vehicle.
Wherein, describedly fly to control plate and also by described third communication chip, described Flight Condition Data be sent to described telechirics, described in fly to control plate and also by the 4th communication chip of described video acquisition plate, receive the state of flight configuration parameter that described intelligent terminal module generates.
Flight Condition Data described in the utility model and flight filling configuration parameter can transmit by above-mentioned any one link path.
And of the present utility modelly fly to control plate and not only can control based on control signal the state of flight of model aerial vehicle, can also collection model aircraft in the duty of all parts.
Preferably, when described third communication chip cannot receive described flight and controls data, described in fly to control four communication chip of plate by described video acquisition plate and send request information to described telechirics;
Described telechirics receives after described request information, and the flight that described remote control system generates described control data acquisition unit is controlled the state of flight configuration parameter that data and intelligent terminal module generate and is sent to described video acquisition plate by second communication chip;
Describedly fly to control four communication chip of plate by described video acquisition plate and receive described flight and control data and state of flight configuration parameter, and also by described the 4th communication chip, send described Flight Condition Data to described intelligent terminal module.
In the utility model when described in fly to control plate and control communication link between data acquisition unit while disconnecting, when the link between the first communication chip and third communication chip disconnects, the flight of transmitting can be controlled to the data such as data by the link transmission of setting up in the middle of described video acquisition plate and intelligent terminal module in described link.
Because the first communication chip transmission range of described control data acquisition unit is generally smaller, so in the utility model when model aerial vehicle exceeds described the first communication chip transmission range, utilize the long feature of transmission range of third communication chip in intelligent terminal module to guarantee that model aerial vehicle can obtain all the time flight and control data etc., thereby model aerial vehicle is all the time under user control.
Wherein, described third communication chip is 2.4G ISM FSK transceiver, and described the 4th communication chip is WIFI communication chip, 3G communication chip or 4G communication chip etc.
Wherein, described video acquisition plate by a serial communication interface with described in fly to control plate interaction data.
Wherein, described serial communication interface is USART interface, SPI interface, RS232 interface or RS485 interface (the asynchronous transmission standard interface that EIA formulates) etc.
Flying in flight control system of the present utility model controlled plate, video acquisition plate, intelligent terminal module and telechirics all have communication chip, now, data are controlled in described flight, Flight Condition Data, state of flight configuration parameter can transmit arbitrarily between described each communication chip, as long as fly to control plate described in described flight control data and state of flight configuration parameter finally transfer to, described Flight Condition Data finally transfers to intelligent terminal module, in addition described video data only can transmit between described video acquisition plate and the communication chip of intelligent terminal module.
Wherein, in intelligent terminal module as above, also comprise a video processing module, a memory module, a load module He Yi land station data cache module;
Wherein said video processing module exports described display screen to for described Flight Condition Data and/or described video data are converted into display;
Described memory module is used for storing described Flight Condition Data and/or described video data;
Described load module is used for reading in the parameter of input, and generates described state of flight configuration parameter based on described parameter;
The flight path data that described land station data cache module sends for buffer memory land station, flight attitude are adjusted data, state of flight is adjusted data, locator data and map datum etc.
Described land station of the present utility model data cache module can adopt the mode of buffer to be added in intelligent terminal module, because the data volume of land station's data is very large, so avoid taking the storer of a large amount of intelligent terminal modules in the utility model by set up independent land station's data cache module in intelligent terminal module.
Wherein, in described intelligent terminal module, also comprise a voice synthetic module and a loudspeaker, for described Flight Condition Data is converted into voice signal, and export by loudspeaker.
Wherein, in described intelligent terminal module, also comprise a sound identification module and a microphone, the voice control signal that described sound identification module gathers based on described microphone, generates supplemental characteristic, and described load module also generates described 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 intelligent terminal module of prior art equally, so be no longer described in detail herein.
For convenience of description, in the utility model, described intelligent terminal module 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 combination in any, obtains each preferred embodiments of the utility model.
Positive progressive effect of the present utility model is:
The advantage of telechirics of the present utility model and flight control system thereof is the operating grip of the telepilot of existing specialty, have again and utilize the multi-functional of intelligent terminal module, so flight control accuracy is high having realized, in the time of good operability, utilize high-performance and the multiple realization of intelligent terminal module, thereby realized high performance 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 intelligent terminal module 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.
Fig. 4 is the structural representation of the embodiment 2 of flight control system of the present utility model.
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 telechirics 1 and a model of an airplane 2, and wherein said telechirics 1 comprises a control module and an intelligent terminal module 12.Described control module comprises a control data acquisition unit 11 and a 2.4G ISM FSK transceiver 114.
And as shown in Figure 2, the described control data acquisition unit 11 of the present embodiment comprises a processor 111, 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 described user generates the operation of described remote-control lever 112 and described teleswitch 113 has formed the flight control data of controlling the model of an airplane.
The ISM of 2.4G described in the present embodiment FSK transceiver 114 is for carrying out data interaction with the model of an airplane 2.
In addition the quantity of described remote-control lever 112 and teleswitch 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 intelligent terminal module 12 of the present embodiment as shown in Figure 3, comprises a video processing module 121a, a display screen 121b, a memory module 122, a load module 123, a voice synthetic module 125, a loudspeaker 126, a sound identification module 127, a microphone 128 and a WIFI communication chip 1211.
Wherein said video processing module 121a is for being converted into by Flight Condition Data the display screen 121b that display exports described intelligent terminal module 12 to, and described display screen 121b correspondingly shows.Described memory module 122 is for storing described Flight Condition Data.Described load module 125 is for reading in the parameter of input, and generates state of flight configuration parameter based on described parameter.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 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 1211 is for carrying out data interaction with the model of an airplane 2.
Wherein the intelligent terminal module 2 of the present embodiment adopts iOS, Android(Android), Symbian(Saipan) etc. intelligent system, and correspondingly configure intelligent terminal module 2 described in rear formation the present embodiment.
As shown in Figure 1, the described model of an airplane 2 comprises that one flies to control plate 21, wherein saidly fly to control plate and comprise a 2.4G ISM FSK transceiver 212, described 2.4G ISM FSK transceiver 212 mates with described 2.4G ISM FSK transceiver 114 and carries out corresponding data interaction, between described 2.4G ISM FSK transceiver 212 and described 2.4G ISM FSK transceiver 114, 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 the model of an airplane 2 of the flight control system of the present embodiment, also comprise a video acquisition plate 22, wherein said video acquisition plate 22 comprises a WIFI communication chip 222, between described WIFI communication chip 222 and described WIFI communication chip 1211, set up data link, and the data such as transmitting video data.And the communication chip that also can adopt 3G or 4G etc. in described video acquisition plate 22 and intelligent terminal module 12 is realized the transmission of data.
Wherein said video acquisition plate 22 is for gathering video data, such as the flight image of camera collection in the model of an airplane 2 etc.
Described in the present embodiment, control data acquisition unit 11 and carry out data transmission by USART interface and intelligent terminal module 12.In addition described in the present embodiment, control data acquisition unit 11 and intelligent terminal module 12 can also adopt USART interface, USB interface, I
2the communication modes such as C interface or SPI interface carry out data transmission.
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 acquisition unit 11 gathers the flight control data that user generates the operation of described remote-control lever 112 and described teleswitch 113.
Then described 2.4G ISM FSK transceiver 114 is controlled data by described flight and is flown to control plate 21 described in being sent to, or described processor 111 receives the common state of flight configuration parameter generating of described intelligent terminal module 12 modules by USART interface, and by described 2.4G ISM FSK transceiver 114, described flight is controlled to data and state of flight configuration parameter and fly to control plate 21 described in being sent to.
After this fly to control the flight of plate 21 based on 212 receptions of 2.4G ISM FSK transceiver and control the flare maneuver that data or flight control data and state of flight configuration parameter are controlled the model of an airplane 2, meanwhile, described in, fly to control plate 21 and also by described 2.4G ISM FSK transceiver 212, the Flight Condition Data of the model of an airplane is sent to the described 2.4G ISM FSK transceiver 114 mating with it.
Finally, the 2.4G ISM FSK transceiver 114 of described control data acquisition unit 11 receives described Flight Condition Data, and transfer to intelligent terminal module 12 by USB interface, after this intelligent terminal module 12 video processing module 121a are converted into by Flight Condition Data the display screen 121b that display exports described intelligent terminal module 12 to, and then described display screen 121b correspondingly shows.
When above-mentioned flow process is carried out, described video acquisition plate 22 is sent to video data the WIFI communication chip 1211 of intelligent terminal module 12 all the time by WIFI communication chip 222, and the video data that the video processing module 121a of described intelligent terminal module 12 receives WIFI communication chip 1211 is converted into the display screen 121b that display exports described intelligent terminal module 12 to, then described display screen 121b correspondingly shows.
Embodiment 2:
In the present embodiment and the difference of embodiment 1 flight control system be: the plate of video acquisition described in the present embodiment 22 and described in fly to control the mode by SPI interface between plate 21 and carry out data transmission.In addition user can also adopt other serial communication interfaces, and such as USART interface, RS232 interface or RS485 interface etc. transmitted described flight control data.
And in the present embodiment, improved the data transmission flow process of embodiment 1.So as shown in Figure 4, the flow process of the data transmission 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 teleswitch 113.
Then described 2.4G ISM FSK transceiver 114 is controlled data by described flight and is flown to control plate 21 described in being sent to, and fly to control plate 21 described in described flight control data being sent to by described 2.4G ISM FSK transceiver 114, meanwhile, the WIFI communication chip 1211 of described intelligent terminal module 12 is sent to video frequency collection card 22 by the common state of flight configuration parameter generating of modules.
The WIFI communication chip 222 of described video frequency collection card 22 receives described state of flight configuration parameter, and is transferred to and flown to control plate 21 by SPI interface.
After this fly to control the flare maneuver that data and the state of flight configuration parameter control model of an airplane 2 are controlled in the flight of plate 21 based on receiving, meanwhile, described in, fly to control plate 21 and also by described 2.4G ISM FSK transceiver 212, the Flight Condition Data of the model of an airplane is sent to the described 2.4G ISM FSK transceiver 114 mating with it.
Finally, the 2.4G ISM FSK transceiver 114 of described control data acquisition unit 11 receives described Flight Condition Data, and transfer to intelligent terminal module 12 by USB interface, after this intelligent terminal module 12 video processing module 121a are converted into by Flight Condition Data the display screen 121b that display exports described intelligent terminal module 12 to, and then described display screen 121b correspondingly shows.
When above-mentioned flow process is carried out, described video acquisition plate 22 is sent to video data the WIFI communication chip 1211 of intelligent terminal module 12 all the time by WIFI communication chip 222, and the video data that the video processing module 121a of described intelligent terminal module 12 receives WIFI communication chip 1211 is converted into the display screen 121b that display exports described intelligent terminal module 12 to, then described display screen 121b correspondingly shows.
Embodiment 3:
The present embodiment is the further improvement based on embodiment 2, between the FSK of 2.4G ISM described in embodiment 2 transceiver 114 and 2.4G ISM FSK transceiver 212, set up communication linkage, equally, between described WIFI communication chip 1211 and WIFI communication chip 222, also set up communication connection.
Because the signal transmission distance of 2.4G ISM FSK transceiver is less than WIFI communication chip, and in embodiment 2, fly to control the flight control signal that plate 21 receives and all by 2.4G ISM FSK transceiver, complete, so when the distance between the model of an airplane and telechirics surpasses the transmission range of 2.4G ISM FSK transceiver, the model of an airplane is by out of hand, and WIFI communication chip has farther communication distance, so utilize the WIFI communication chip 222 of video acquisition plate 22 and the communication link of WIFI communication chip 1211 to continue to transmit flight in the present embodiment, control data etc., thereby can continue to control the flight of the model of an airplane, and expanded the remote control distance of the model of an airplane.
So the workflow in the present embodiment in the time can also communicating between described 2.4G ISM FSK transceiver 114 and 2.4G ISM FSK transceiver 212 is identical with embodiment 2, so be no longer described in detail herein.
When communication linkage between described 2.4G ISM FSK transceiver 114 and 2.4G ISM FSK transceiver 212 disconnects, the principle of work of described flight control system is as follows:
When flying to control the 2.4G ISM FSK transceiver 212 of plate 21 cannot receive described flight that described 2.4G ISM FSK transceiver 114 sends and control data time, described in fly to control the WIFI communication chip 222 of plate 21 by described video acquisition plate 22 and send request information to described telechirics 1.
Described telechirics 1 receives after described request information, and the flight that described telechirics 1 generates described control data acquisition unit 11 is controlled state of flight configuration parameter that data and intelligent terminal module 12 the generate WIFI communication chip 1211 by intelligent terminal module 12 and is sent to described video acquisition plate 22.
Describedly fly to control the WIFI communication chip 222 of plate 21 by described video acquisition plate 22 and receive described flight and control data and state of flight configuration parameter, and also by described WIFI communication chip 222, send extremely described intelligent terminal module 12 of described Flight Condition Data.
After this intelligent terminal module 12 video processing module 121a are converted into by Flight Condition Data the display screen 121b that display exports described intelligent terminal module 12 to, and then described display screen 121b correspondingly shows.
And the flow process that those skilled in the art will recognize that the data transmission of embodiment 1, embodiment 2 and embodiment 3 can and deposit and same flight control system, flight control system can need to adopt the flow process of different data transmission according to the transmission of self.
Embodiment 4:
The present embodiment is the further improvement based on embodiment 1, the plate of video acquisition described in the present embodiment 22 and described in fly to control the mode by SPI interface between plate 21 and carry out data transmission.In addition user can also adopt other serial communication interfaces, and such as USART interface, RS232 interface or RS485 interface etc. transmitted described flight control data.The flow process of the data transmission 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 teleswitch 113.
Then described 2.4G ISM FSK transceiver 114 is controlled data by described flight and is flown to control plate 21 described in being sent to, and fly to control plate 21 described in described flight control data being sent to by described 2.4G ISM FSK transceiver 114, meanwhile, the WIFI communication chip 1211 of described intelligent terminal module 12 is sent to video frequency collection card 22 by the common state of flight configuration parameter generating of modules.
The WIFI communication chip 222 of described video frequency collection card 22 receives described state of flight configuration parameter, and is transferred to and flown to control plate 21 by SPI interface.
After this fly to control the flight of plate 21 based on receiving and control the flare maneuver that data and state of flight configuration parameter are controlled the model of an airplane 2, meanwhile, described in fly to control plate 21 and also the Flight Condition Data of the model of an airplane be sent to video frequency collection card 22 by SPI interface.
After this described video acquisition plate 22 is sent to described Flight Condition Data by WIFI communication chip 222 the WIFI communication chip 1211 mating with it.
Finally, the Flight Condition Data that the video processing module 121a of described intelligent terminal module 12 receives WIFI communication chip 1211 is converted into the display screen 121b that display exports described intelligent terminal module 12 to, and then described display screen 121b correspondingly shows.
When above-mentioned flow process is carried out, described video acquisition plate 22 is sent to video data the WIFI communication chip 1211 of intelligent terminal module 12 all the time by WIFI communication chip 222, and the video data that the video processing module 121a of described intelligent terminal module 12 receives WIFI communication chip 1211 is converted into the display screen 121b that display exports described intelligent terminal module 12 to, then described display screen 121b correspondingly shows.
Embodiment 5:
In the present embodiment, be with the difference of embodiment 4 flight control systems: described in the present embodiment, control data acquisition unit 11 and carry out data transmission by USART interface and intelligent terminal module 12.In addition described in the present embodiment, control data acquisition unit 11 and intelligent terminal module 12 can also adopt USART interface, USB interface, I
2the communication modes such as C interface or SPI interface carry out data transmission.
And in the present embodiment, improved the data transmission flow process of embodiment 4.The flow process of the data transmission 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 teleswitch 113.
Then described 2.4G ISM FSK transceiver 114 is controlled data by described flight and is flown to control plate 21 described in being sent to, or described processor 111 receives the common state of flight configuration parameter generating of described intelligent terminal module 12 modules by USB interface, and by described 2.4G ISM FSK transceiver 114, described flight is controlled to data and state of flight configuration parameter and fly to control plate 21 described in being sent to.
After this fly to control the flight of plate 21 based on 212 receptions of 2.4G ISM FSK transceiver and control the flare maneuver that data or flight control data and state of flight configuration parameter are controlled the model of an airplane 2, meanwhile, described in, fly to control plate 21 and also the Flight Condition Data of the model of an airplane is sent to video frequency collection card 22 by SPI interface.
After this described video acquisition plate 22 is sent to described Flight Condition Data by WIFI communication chip 222 the WIFI communication chip 1211 mating with it.
Finally, the Flight Condition Data that the video processing module 121a of described intelligent terminal module 12 receives WIFI communication chip 1211 is converted into the display screen 121b that display exports described intelligent terminal module 12 to, and then described display screen 121b correspondingly shows.
When above-mentioned flow process is carried out, described video acquisition plate 22 is sent to video data the WIFI communication chip 1211 of intelligent terminal module 12 all the time by WIFI communication chip 222, and the video data that the video processing module 121a of described intelligent terminal module 12 receives WIFI communication chip 1211 is converted into the display screen 121b that display exports described intelligent terminal module 12 to, then described display screen 121b correspondingly shows.
Embodiment 6:
The present embodiment is the further improvement based on embodiment 5, between the FSK of 2.4G ISM described in embodiment 5 transceiver 114 and 2.4G ISM FSK transceiver 212, set up communication linkage, equally, between described WIFI communication chip 1211 and WIFI communication chip 222, also set up communication connection.
Because the signal transmission distance of 2.4G ISM FSK transceiver is less than WIFI communication chip, and in embodiment 2, fly to control the flight control signal that plate 21 receives and all by 2.4G ISM FSK transceiver, complete, so when the distance between the model of an airplane and telechirics surpasses the transmission range of 2.4G ISM FSK transceiver, the model of an airplane is by out of hand, and WIFI communication chip has farther communication distance, so utilize the WIFI communication chip 222 of video acquisition plate 22 and the communication link of WIFI communication chip 1211 to continue to transmit flight in the present embodiment, control data etc., thereby can continue to control the flight of the model of an airplane, and expanded the remote control distance of the model of an airplane.
So the workflow in the present embodiment in the time can also communicating between described 2.4G ISM FSK transceiver 114 and 2.4G ISM FSK transceiver 212 is identical with embodiment 2, so be no longer described in detail herein.
When communication linkage between described 2.4G ISM FSK transceiver 114 and 2.4G ISM FSK transceiver 212 disconnects, the principle of work of described flight control system is as follows:
When flying to control the 2.4G ISM FSK transceiver 212 of plate 21 cannot receive described flight that described 2.4G ISM FSK transceiver 114 sends and control data time, described in fly to control the WIFI communication chip 222 of plate 21 by described video acquisition plate 22 and send request information to described telechirics 1.
Described telechirics 1 receives after described request information, and the flight that described telechirics 1 generates described control data acquisition unit 11 is controlled state of flight configuration parameter that data and intelligent terminal module 12 the generate WIFI communication chip 1211 by intelligent terminal module 12 and is sent to described video acquisition plate 22.
Describedly fly to control the WIFI communication chip 222 of plate 21 by described video acquisition plate 22 and receive described flight and control data and state of flight configuration parameter, and also by described WIFI communication chip 222, send extremely described intelligent terminal module 12 of described Flight Condition Data.
After this intelligent terminal module 12 video processing module 121a are converted into by Flight Condition Data the display screen 121b that display exports described intelligent terminal module 12 to, and then described display screen 121b correspondingly shows.
And the flow process that those skilled in the art will recognize that the data transmission of embodiment 4, embodiment 5 and embodiment 6 can and deposit and same flight control system, flight control system can need to adopt the flow process of different data transmission according to the transmission of self.
Each embodiment in this instructions all adopts the mode of going forward one by one to describe, between each embodiment identical similar part mutually referring to, each embodiment stresses is the difference with other embodiment.
Although more than described 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 (13)
1. a telechirics, it is characterized in that, comprise an intelligent terminal module, described intelligent terminal module comprises a second communication chip, described telechirics also comprises a control module, described control module comprises that one for gathering control data acquisition unit and one first communication chip of the flight control data of controlling a model aerial vehicle, and described second communication chip receives the video data of described model aerial vehicle; The first communication chip of described control module is also sent to described intelligent terminal module by the Flight Condition Data of the described model aerial vehicle receiving.
2. telechirics as claimed in claim 1, is characterized in that, described control data acquisition unit comprises a processor, a plurality of remote-control lever and a plurality of teleswitch;
Data are controlled in the flight that wherein said processor gathers user's input by described remote-control lever and described teleswitch.
3. telechirics as claimed in claim 2, is characterized in that, described the first communication chip is 2.4G/5.8G ISM FSK transceiver.
4. telechirics as claimed in claim 3, is characterized in that, described control module is by a USART interface, a USB interface, an I
2c interface or a SPI interface are sent to described intelligent terminal module by described Flight Condition Data.
5. telechirics as claimed in claim 3, is characterized in that, described intelligent terminal module also comprises that one for showing the display screen of Flight Condition Data and/or video data.
6. telechirics as claimed in claim 3, is characterized in that, described second communication chip is WIFI communication chip, 3G communication chip or 4G communication chip.
7. the telechirics as described in any one in claim 3-6, it is characterized in that, in described intelligent terminal module, 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 load module of the parameter of input.
8. telechirics as claimed in claim 7, 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 intelligent terminal module.
9. telechirics as claimed in claim 7, is characterized in that, also comprises that a microphone and is for being converted into the voice signal of described microphone collection the sound identification module of supplemental characteristic in described intelligent terminal module.
10. a flight control system, it comprises a model aerial vehicle, described model aerial vehicle comprise for gather described model aerial vehicle Flight Condition Data one fly to control plate and for gathering a video acquisition plate of video data, it is characterized in that, described flight control system also comprises just like the telechirics described in any one in claim 1-9, wherein saidly fly to control plate and also comprise a third communication chip, described in fly to control plate by described third communication chip and described telechirics interaction data;
Described video acquisition plate also comprises one the 4th communication chip, and described video acquisition plate is by described the 4th communication chip and described telechirics interaction data;
When the communication link of described third communication chip and described telechirics disconnects, described in fly to control plate by the 4th communication chip of described video acquisition plate and the second communication chip interaction data of described telechirics.
11. flight control systems as claimed in claim 10, is characterized in that, described third communication chip is 2.4G ISM FSK transceiver, and described the 4th communication chip is WIFI communication chip, 3G communication chip or 4G communication chip.
12. flight control systems as claimed in claim 11, is characterized in that, described video acquisition plate by a serial communication interface with described in fly to control plate interaction data.
13. flight control systems as claimed in claim 12, is characterized in that, described serial communication interface is USART interface, SPI interface, RS232 interface or RS485 interface.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320339656.7U CN203414817U (en) | 2013-06-13 | 2013-06-13 | A remote control system and an aircraft control system thereof |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201320339656.7U CN203414817U (en) | 2013-06-13 | 2013-06-13 | A remote control system and an aircraft control system thereof |
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| CN203414817U true CN203414817U (en) | 2014-01-29 |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104155904A (en) * | 2014-08-20 | 2014-11-19 | 张小雷 | Four-rotor aircraft remote controller based on gyroscope and embedded flight control system |
| WO2014198188A1 (en) * | 2013-06-13 | 2014-12-18 | Tian Yu | Aircraft control system |
| WO2014198189A1 (en) * | 2013-06-13 | 2014-12-18 | Tian Yu | Smart display remote control and flight control system |
| CN104238564A (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 |
| CN104867259A (en) * | 2015-05-13 | 2015-08-26 | 零度智控（北京）智能科技有限公司 | Unmanned aircraft remote controller light warning system |
| CN105000170A (en) * | 2015-07-15 | 2015-10-28 | 何春旺 | Touch screen controller and control method of driving device |
| WO2016095793A1 (en) * | 2014-12-15 | 2016-06-23 | 优利科技有限公司 | Remote control |
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2013
- 2013-06-13 CN CN201320339656.7U patent/CN203414817U/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014198188A1 (en) * | 2013-06-13 | 2014-12-18 | Tian Yu | Aircraft control system |
| WO2014198189A1 (en) * | 2013-06-13 | 2014-12-18 | Tian Yu | Smart display remote control and flight control system |
| CN104238564A (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 |
| CN104238564B (en) * | 2013-06-13 | 2017-03-01 | 优利科技有限公司 | Remote control systems and its flight control system |
| CN104155904A (en) * | 2014-08-20 | 2014-11-19 | 张小雷 | Four-rotor aircraft remote controller based on gyroscope and embedded flight control system |
| WO2016095793A1 (en) * | 2014-12-15 | 2016-06-23 | 优利科技有限公司 | Remote control |
| CN104867259A (en) * | 2015-05-13 | 2015-08-26 | 零度智控（北京）智能科技有限公司 | Unmanned aircraft remote controller light warning system |
| CN105000170A (en) * | 2015-07-15 | 2015-10-28 | 何春旺 | Touch screen controller and control method of driving device |
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