CN204945801U - A kind of based on voice-operated flight control system - Google Patents
A kind of based on voice-operated flight control system Download PDFInfo
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- CN204945801U CN204945801U CN201520637457.3U CN201520637457U CN204945801U CN 204945801 U CN204945801 U CN 204945801U CN 201520637457 U CN201520637457 U CN 201520637457U CN 204945801 U CN204945801 U CN 204945801U
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Abstract
The utility model relates to a kind of based on voice-operated flight control system, comprises intelligent terminal controller subsystem and aircraft side controller subsystem.The utility model by being arranged on software simulating on intelligent terminal to the Voice command of long-range unmanned vehicle, simultaneously can compatible driving lever operation, body sense operation and path forms program operation.Pass through speech control module, the various operations to aircraft can be realized, simultaneously, because voice just can control the operation of aircraft, therefore the both hands of operator can farthest be liberated, achieve the simplification of flying vehicles control, safe and variation, enhance the interactive capability of aircraft.
Description
Technical field
The utility model relates to a kind of flight control system field, more specifically, relates to unmanned aerial vehicle control system, aeromodelling aerocraft control system and toy aircraft control system.
Background technology
Aircraft in the market comprises unmanned plane, aeromodelling aerocraft and toy aircraft, driving lever operation (as shown in Figure 1) or body sense operation can only be carried out by telepilot, human-computer interaction can not be carried out, setting, complicated operation, be unfavorable for the universal of popular application, in case of emergency easily maloperation occur simultaneously, bring danger, in addition, be unfavorable for that manual manipulation has the user of obstacle to use.
Summary of the invention
The utility model, for above-mentioned defect of the prior art, it is main for intelligent terminal have employed based on Voice command, and driving lever operation, body sense operation or stroke planning operation can be selected to control flight control simultaneously.Open up the man-machine interaction epoch of flying vehicles control, reduced the difficulty of flying vehicles control, improve the science and technology-oriented, recreational of flying vehicles control, add the security of flying vehicles control.
The technical solution of the utility model is as follows:
A kind of based on voice-operated flight control system, comprise intelligent terminal controller subsystem and aircraft side controller subsystem.Described intelligent terminal controller subsystem comprises speech control module, body sense control module, stroke planning control module, virtual rocking bar control module, mobile terminal main control unit MCU module, body propagated sensation sensor, microphone, video/information display module and radio receiving transmitting module.Described speech control module comprises voice activated module, voice memory unit, voice comparing unit, phonetic order output unit, instruction database map unit.Described aircraft side controller subsystem comprises aircraft end main control unit MCU, sensor unit, video acquisition processing module, wireless output module, motor output module, steering wheel output module.Described sensor unit comprises the various application sensors such as compass sensor, angular-rate sensor, acceleration transducer, barometer sensor and temperature sensor, humidity sensor, smoke transducer, gas sensor.
Accompanying drawing explanation
Fig. 1 is that conventional remote controls controls aircraft frame schematic diagram;
Fig. 2 is intelligent terminal controller subsystem frame principle;
Fig. 3 is aircraft side controller subsystem frame principles;
Fig. 4 is sound identification module workflow diagram.
Embodiment
Below in conjunction with accompanying drawing, embodiment of the present utility model is elaborated.
As shown in Figure 2, a kind of flight control system field of the present utility model, described intelligent terminal controller subsystem end, is made up of software section and hardware components.
Preferably, described software section is made up of speech control module, body sense control module, stroke planning control module, virtual rocking bar control module, manipulates main interface and video display module forms.Described hardware components is made up of main control unit MCU, body propagated sensation sensor cell, radio receiving transmitting module and display module.
Manipulate in main interface and can select different control models, and the instruction under corresponding control model is sent to unmanned plane subsystem end by wireless communication protocol, realize the remote wireless control to unmanned plane.Manipulate main interface also the video data of aircraft end control subsystem collection and aircraft sensing data to be presented on intelligent terminal display screen in real time simultaneously, facilitate manipulator to understand the state of the real-time picture of aircraft end and aircraft itself.
Under Voice command pattern, instructions such as " start, rise, decline, turn left, turn right, land, roll, take pictures, open video recording, close video recording, make a return voyage and force-land " that manipulator can send, aircraft, according to receiving phonetic order, operates aircraft in real time.
Under body sense control model, described body sense control module is by the real-time status of body propagated sensation sensor, and synchronized transmission is to aircraft end, and aircraft synchronously changes according to the change of intelligent terminal controller attitude, in conjunction with Throttle Opening Control lifting, realizes the body sense manipulation of unmanned plane.
Under stroke planning control model, the path flight that can set on intelligent terminal according to manipulator.Aircraft can be realized automatically fly by path.
Under virtual driving lever pattern, intelligent terminal screen there is the four-way driving lever of analog telecommand, be respectively throttle, lifting, aileron, direction, can touch-screen driving lever be passed through, realize the straighforward operation to aircraft.
Further, as shown in Figure 4, described speech control module simplification workflow is as follows.
1, speech control module opening voice trigger element, detects speech input information in real time, when the acoustic information meeting certain decibel being detected, and triggering voice storage unit, otherwise continue to detect.
2, after speech trigger starts, call voice memory unit, voice messaging is stored.
3, after phonetic storage completes, voice comparison link is entered.Phonetic order in storage unit and phonetic order storehouse are compared, eligible, export comparison result, ineligible, then Identification display mistake, enters speech trigger flow process.
4, voice messaging correct for comparison is converted to the literal order of ASCII fromat by Audio Processing Unit, sends into command mappings unit.
5, the voice ASCII instruction that will receive of command mappings unit, is mapped to corresponding binary flight steering order, and Output rusults, call transmission for main control interface.
As shown in Figure 3, a kind of flight control system field of the present utility model, described aircraft side controller subsystem comprises aircraft main control unit MCU, sensors inputs divides, video acquisition load module, wireless receiving and dispatching communication module, motor output unit, steering wheel output unit.
Further, described aircraft main control unit MCU, is made up of in the embedded software of Master control chip Master control chip and burning.Aircraft main control unit MCU is by reading various kinds of sensors data, judge attitude, height and speed residing for current flight device, the control information that combined with intelligent control terminal is sent, export different control signals to motor output unit and steering wheel output unit, realize controlling the stabilized flight of aircraft.Aircraft main control unit MCU is also responsible for the video flowing of video acquisition module and the image data of application sensors, by wireless communication module, is sent to control of intelligent terminal.
Preferably, described Sensor section comprises compass sensor, angular-rate sensor, acceleration transducer, barometer sensor and sector application sensor as humidity sensor, temperature sensor, smoke transducer etc.
Further, described radio communication transceiver module can select WIFI communication module, 3G communication module and 4G communication module, and the utility model realizes based on WIFI communication module at present.
Described video acquisition module, is responsible for gathering high clear video image information, under aircraft main control unit MCU controls, is sent to intelligent terminal control by wireless communication module.
Described motor output unit is responsible for exporting motor control signal, for controlling aircraft CD-ROM drive motor.According to different aircraft classification, motor output unit output channel quantity is different.Four motor output channels as corresponding in quadrotor, corresponding two the motor output channels of helicopter.
Described steering wheel output unit is responsible for exporting servos control signal, controls as The Cloud Terrace, camera etc. for the control of Fixed Wing AirVehicle steering wheel and other passages of aircraft.
Above-described embodiment of the present invention, does not form limiting the scope of the present invention.Any amendment done within the spirit and principles in the present invention, equivalent replacement and improvement etc., all should be included within claims of the present invention.
Claims (6)
1., based on a voice-operated flight control system, comprise intelligent terminal controller subsystem and aircraft side controller subsystem, described intelligent terminal controller subsystem comprises speech control module, body sense control module, stroke planning control module, virtual rocking bar control module, mobile terminal main control unit MCU module, body propagated sensation sensor, microphone, display module and radio receiving transmitting module, described speech control module comprises speech trigger unit, voice memory unit, voice comparing unit, phonetic order output unit, instruction database map unit, described aircraft side controller subsystem comprises aircraft end main control unit MCU, sensor unit, video acquisition processing module, wireless output module, motor output module, steering wheel output module, described sensor unit comprises compass sensor, angular-rate sensor, acceleration transducer, barometer sensor and application sensors, described application sensors comprises temperature sensor, humidity sensor, smoke transducer and gas sensor.
2. as claimed in claim 1 based on voice-operated flight control system, it is characterized in that: described intelligent terminal controller subsystem, by the phonetic order received, control the various flight operations of aircraft.
3. as claimed in claim 1 based on voice-operated flight control system, it is characterized in that: described intelligent terminal controller subsystem, IOS, android operating system and windows system can be adopted.
4. as claimed in claim 1 based on voice-operated flight control system, it is characterized in that: described intelligent terminal controller subsystem, can Voice command be passed through, the operation of virtual driving lever, body sense operation or stroke planning operation can also be switched to.
5. as claimed in claim 1 based on voice-operated flight control system, it is characterized in that: described intelligent terminal controller subsystem can receive from the real-time video information of described aircraft side controller subsystem, attitude of flight vehicle information and application sensors information.
6. as claimed in claim 1 based on voice-operated flight control system, it is characterized in that: described aircraft side controller subsystem can be loaded on fixed-wing, helicopter and rotor craft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520637457.3U CN204945801U (en) | 2015-08-24 | 2015-08-24 | A kind of based on voice-operated flight control system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520637457.3U CN204945801U (en) | 2015-08-24 | 2015-08-24 | A kind of based on voice-operated flight control system |
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| CN204945801U true CN204945801U (en) | 2016-01-06 |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105620737A (en) * | 2016-02-26 | 2016-06-01 | 厦门大学嘉庚学院 | Voice remote control system used for helicopter type aircraft and helicopter type remote control aircraft |
| CN105652889A (en) * | 2016-04-12 | 2016-06-08 | 谭圆圆 | Remote control device of unmanned aerial vehicle and control method of remote control device |
| CN105679322A (en) * | 2016-03-29 | 2016-06-15 | 普宙飞行器科技（深圳）有限公司 | Airborne voice control-based unmanned aerial vehicle system and control method |
| CN105827260A (en) * | 2016-04-15 | 2016-08-03 | 上海理工大学 | Voice control unmanned aerial vehicle |
| CN106020214A (en) * | 2016-08-11 | 2016-10-12 | 上海与德通讯技术有限公司 | Unmanned aerial vehicle interaction control device and system |
| CN108122553A (en) * | 2017-12-20 | 2018-06-05 | 深圳市道通智能航空技术有限公司 | A kind of unmanned aerial vehicle (UAV) control method, apparatus, remote control equipment and UAV system |
| CN108776490A (en) * | 2018-04-23 | 2018-11-09 | 西安电子科技大学 | A kind of aircraft script control method based on semantic analysis |
| CN109979459A (en) * | 2019-02-28 | 2019-07-05 | 西安爱生技术集团公司 | A kind of four-rotor aircraft control system based on signer-independent sign language recognition |
| CN110377053A (en) * | 2016-12-02 | 2019-10-25 | 广州亿航智能技术有限公司 | The flight control method and device of unmanned plane |
| CN111031202A (en) * | 2019-11-25 | 2020-04-17 | 长春理工大学 | Four-rotor-based intelligent photographing UAV, intelligent photographing system and method thereof |
| CN119400175A (en) * | 2024-12-31 | 2025-02-07 | 深圳市富斯科技有限公司 | A voice control system and method based on remote controller |
-
2015
- 2015-08-24 CN CN201520637457.3U patent/CN204945801U/en not_active Expired - Fee Related
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105620737A (en) * | 2016-02-26 | 2016-06-01 | 厦门大学嘉庚学院 | Voice remote control system used for helicopter type aircraft and helicopter type remote control aircraft |
| CN105679322A (en) * | 2016-03-29 | 2016-06-15 | 普宙飞行器科技（深圳）有限公司 | Airborne voice control-based unmanned aerial vehicle system and control method |
| CN105652889A (en) * | 2016-04-12 | 2016-06-08 | 谭圆圆 | Remote control device of unmanned aerial vehicle and control method of remote control device |
| CN105827260A (en) * | 2016-04-15 | 2016-08-03 | 上海理工大学 | Voice control unmanned aerial vehicle |
| CN106020214A (en) * | 2016-08-11 | 2016-10-12 | 上海与德通讯技术有限公司 | Unmanned aerial vehicle interaction control device and system |
| CN110377053A (en) * | 2016-12-02 | 2019-10-25 | 广州亿航智能技术有限公司 | The flight control method and device of unmanned plane |
| CN108122553B (en) * | 2017-12-20 | 2020-12-08 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle control method and device, remote control equipment and unmanned aerial vehicle system |
| CN108122553A (en) * | 2017-12-20 | 2018-06-05 | 深圳市道通智能航空技术有限公司 | A kind of unmanned aerial vehicle (UAV) control method, apparatus, remote control equipment and UAV system |
| US11487302B2 (en) | 2017-12-20 | 2022-11-01 | Autel Robotics Co., Ltd. | Unmanned aerial vehicle control method and apparatus, remote control device, and unmanned aerial vehicle system |
| CN108776490A (en) * | 2018-04-23 | 2018-11-09 | 西安电子科技大学 | A kind of aircraft script control method based on semantic analysis |
| CN109979459A (en) * | 2019-02-28 | 2019-07-05 | 西安爱生技术集团公司 | A kind of four-rotor aircraft control system based on signer-independent sign language recognition |
| CN111031202A (en) * | 2019-11-25 | 2020-04-17 | 长春理工大学 | Four-rotor-based intelligent photographing UAV, intelligent photographing system and method thereof |
| CN119400175A (en) * | 2024-12-31 | 2025-02-07 | 深圳市富斯科技有限公司 | A voice control system and method based on remote controller |
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| C14 | Grant of patent or utility model | ||
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160106 Termination date: 20190824 |