CN207173963U - It is a kind of new based on cell phone intelligent APP Voice command aerocraft systems - Google Patents

It is a kind of new based on cell phone intelligent APP Voice command aerocraft systems Download PDF

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Publication number
CN207173963U
CN207173963U CN201720571534.9U CN201720571534U CN207173963U CN 207173963 U CN207173963 U CN 207173963U CN 201720571534 U CN201720571534 U CN 201720571534U CN 207173963 U CN207173963 U CN 207173963U
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China
Prior art keywords
cell phone
aircraft
module
mkl26
voice command
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Expired - Fee Related
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CN201720571534.9U
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Chinese (zh)
Inventor
颜宋宋
王文武
徐勇
李紫薇
汪锐
孙甲丽
钱佳佳
毕健
李顺
张颉
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Anhui Normal University
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Anhui Normal University
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Priority to CN201720571534.9U priority Critical patent/CN207173963U/en
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Publication of CN207173963U publication Critical patent/CN207173963U/en
Expired - Fee Related legal-status Critical Current
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Abstract

The utility model discloses the utility model discloses a kind of new based on cell phone intelligent APP Voice command aerocraft systems,Including four-axle aircraft,The four-axle aircraft MKL26 main control modules,The four-axle aircraft MKL26 main control modules are connected with human-computer interaction module,Fan control module,GPS module,Power module and sensor assembly,The human-computer interaction module uses cell phone application as flight controller,Voice order is precisely identified using the speech identifying function of mobile phone,The operation of the four-axle aircraft MKL26 master control module controls fan control modules,The sensor assembly is used for acquisition angles,Distance,Humiture and image recognition information,The four-axle aircraft MKL26 main control modules use No. four electric machine controllers,Integrate multiple sensors,The major function of aircraft is realized using the MCU single-chip microcomputer MKL26Z256VLL4 singlechip microcontrollers of cheap function admirable,Design aircraft model machine,And establish simplified model,Six axle flying vehicles control flight attitudes of innovative design.

Description

It is a kind of new based on cell phone intelligent APP Voice command aerocraft systems
Technical field
Four-axle aircraft technical field is the utility model is related to, it is specially a kind of new based on cell phone intelligent APP voices Control aerocraft system.
Background technology
Present Development of UAV is flourishing as never before, and unmanned plane is divided into two kinds, fixed-wing unmanned plane and rotary wings unmanned plane.Four axles Aircraft just belongs to the latter, and compared with fixed-wing unmanned plane, four-axle aircraft has and can flown backward, VTOL and in sky The function of middle hovering, the requirement for take-off venue is very low, and also very flexibly, application aspect is also very extensive for control.So for four The research of axle aircraft is also highly significant.Present unmanned plane has been obtained for very extensive application.
Military aspect, unmanned plane is put into already under battle conditions in use, unmanned plane can implement battlefield investigation, mesh in war Demarcate position, unit tracking, the electronic interferences even task such as fire support.Agriculturally, unmanned plane be used to spray insecticide, and survey Determine crops health status.In life, unmanned plane is used for the transmission of express delivery, and four-axle aircraft is liked by the limit now Good person's likes, because four-axle aircraft can follow the trail of shooting, this is that other shooting machines can not be accomplished.And unmanned plane exists Highly, speed and the advantage of flexibility, its extraordinary potential under the occasions such as public security, the disaster relief has been achieved.But four current axles Aircraft cost is high, is not easy to large-scale promotion, and the four-axle aircraft General portable designed at present is poor, stability not Foot.
The content of the invention
In order to overcome the shortcomings of prior art, the utility model provides a kind of new based on cell phone intelligent APP languages Sound control aerocraft system, using smart mobile phone APP as the remote control of aircraft, using the speech identifying function of mobile phone The accurate identification to voice order is realized so as to more convenient control aircraft flight action, while reduces and makes remote control in kind Cost also simplify the difficulty of manipulation.
Technical scheme is used by the utility model solves its technical problem:It is a kind of new based on cell phone intelligent APP Voice command aerocraft system, including four-axle aircraft MKL26 main control modules, the four-axle aircraft MKL26 main control modules connect Human-computer interaction module, fan control module, GPS module, power module and sensor assembly are connected to, the human-computer interaction module makes By the use of cell phone application as flight controller, voice order is precisely identified using the speech identifying function of mobile phone, four axle flies The operation of row device MKL26 master control module controls fan control modules, the sensor assembly are used for acquisition angles, distance, warm and humid Degree and image recognition information, the four-axle aircraft MKL26 main control modules use No. four electric machine controllers, integrate multiple sensings Device.
As a kind of preferable technical scheme of the utility model, the fan control module is using the mixing decay of advanced dynamic Technical controlling four-axle aircraft rotor.
As a kind of preferable technical scheme of the utility model, the four-axle aircraft MKL26 main control modules are also integrated with ESP8266 wireless modules, for coordinating the cell phone application of independent development as the remote control of aircraft.
As a kind of preferable technical scheme of the utility model, the sensor assembly uses MS5611-01BA air pressure transmissions Sensor realizes that aerial autonomous hovering function is realized in aircraft altitude collection.
As a kind of preferable technical scheme of the utility model, the GPS module uses S1216F8-BD modules.
As a kind of preferable technical scheme of the utility model, the sensor assembly is sensed by angular transducer, ranging Device, Temperature Humidity Sensor and imaging sensor composition.
As a kind of preferable technical scheme of the utility model, the ESP8266 wireless modules are integrated with duplexer, work( Rate amplifier, low noise amplifier, filter and power management module.
Compared with prior art, the beneficial effects of the utility model are:The utility model uses smart mobile phone APP conducts The remote control of aircraft, realize that the accurate identification to voice order is controlled so as to more convenient using the speech identifying function of mobile phone Aircraft flight processed action, while coordinate multiple sensors to realize autonomous hovering functions, using GPS/ Big Dipper bimodulus locating modules, Make positioning more precisely rapid, realize that dropout makes a return voyage automatically, the function such as fixed point flight, shoot the real-time passback of video photography And a kind of inexpensive, high performance six axles aircraft that the multiple functions such as avoidance flight are integrated in flight way, reduce simultaneously The cost of making remote control in kind, also simplify the difficulty of manipulation, using the MCU single-chip microcomputers of cheap function admirable MKL26Z256VLL4 singlechip microcontrollers realize the major function of aircraft, design aircraft model machine, and establish simplified mould Type, six axle flying vehicles control flight attitudes of innovative design.
Brief description of the drawings
Fig. 1 is the utility model structure diagram.
Fig. 2 is the utility model baroceptor circuit diagram.
Fig. 3 is the utility model GPS module and single-chip microcomputer connection diagram.
In figure:1- four-axle aircraft MKL26 main control modules;2- human-computer interaction modules;3- fan control modules;The axles of 4- tetra- fly Row device rotor;5-GPS modules;6- power modules;7- sensor assemblies;8-ESP8266 wireless modules.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made The every other embodiment obtained, belong to the scope of the utility model protection.
Embodiment:
As shown in Figure 1, Figure 2 and Figure 3, the utility model provides a kind of new based on cell phone intelligent APP Voice commands Aerocraft system, including four-axle aircraft MKL26 main control modules 1, the four-axle aircraft MKL26 main control modules 1 connect someone Machine interactive module 2, fan control module 3, GPS module 5, power module 6 and sensor assembly 7, the human-computer interaction module 2 make By the use of cell phone application as flight controller, voice order is precisely identified using the speech identifying function of mobile phone, four axle flies Row device MKL26 main control modules 1 control the operation of fan control module 3, and the sensor assembly 7 is passed by angular transducer, ranging Sensor, Temperature Humidity Sensor and imaging sensor composition, the sensor assembly 7 are used for acquisition angles, distance, humiture and figure As identification information, the four-axle aircraft MKL26 main control modules 1 use No. four electric machine controllers, integrate multiple sensors, described Fan control module 3 more can closely track input electricity using advanced dynamic mixing decay technique control four-axle aircraft rotor Stream, it is achieved thereby that the high efficiency motor control under high speed conditions, wherein supporting market using advanced dynamic mixing decay technique The digital motor controller of upper common PWM drivings, such as the electric machine controller that HBQ2811, DSE5110 etc. are conventional, the electricity Machine controller uses three-phase hybrid stepping motor, and low speed operates steadily, and hyper tape load torque is big, simple to operate, and stability is high.
The four-axle aircraft MKL26 main control modules 1 are also integrated with ESP8266 wireless modules 8, for coordinating independent development Remote control of the cell phone application as aircraft, the accurate knowledge to voice order is realized using the speech identifying function of mobile phone Not so as to more convenient control aircraft flight action, the interactive operation of human-computer interaction module 2 is realized, while it is in kind to reduce making The cost of remote control also simplify the difficulty of manipulation.
The sensor assembly 7 includes the pressure sensor of high linearity and 24 Σ moulds of a super low-power consumption Number converter, realize that aerial autonomous hovering function is realized in aircraft altitude collection using MS5611-01BA baroceptors, it is described MS5611-01BA baroceptors are integrated with SPI and I2C EBIs, MS5611 provide an accurate 24 bit digital pressure Force value and temperature value and different operator schemes, conversion speed can be improved and optimize current drain.High-resolution temperature Output can realize altimeter/thermometer function without additional sensors.It can be connected with substantially any microcontroller.Communication protocol Simply, without being programmed in device interior register.MS5611 pressure sensors only have 5.0 millimeters × 3.0 millimeters × 1.0 millimeters Small size can integrate in a mobile device, and there is high stability and low-down pressure signal to lag.
The GPS module 5 can be entered using S1216F8-BD modules, compact, excellent performance, GPS module by serial ports Row various parameters are set, and can be stored in internal FLASH, easy to use, and carry IPX interface, can connect various active days Line, it is proposed that connection GPS/ Big Dipper bimodulus active antennas, module compatibility 3.3V/5V level is convenient to connect various SCM systems, in fact Read referring now to positional information, realize that dropout makes a return voyage automatically, the function such as fixed point flight, the passback of collection live-pictures, avoidance fly Row function is in one.The ESP8266 wireless modules are built-in with TensilicaL10632 positions microcontroller, ESP8266EX It is that integrated level highest Wi-Fi chips, minimum package dimension are only 5mmx5mm in the industry, ESP8266 wireless modules also highly collect Into duplexer, radio frequency balun, power amplifier, low noise amplifier, filter and power management module, it is only necessary to seldom Peripheral circuit, shared PCB space can be preferably minimized, ESP8266EX aims at mobile device, wearable electronic product and Internet of Things Using and design, lowest power consumption is realized by multinomial proprietary technology.ESP8266EX has three kinds of operational modes:Activation pattern, sleep Sleep mode and deep sleep mode, battery life can be extended.
The utility model uses remote controls of the smart mobile phone APP as aircraft, using the speech recognition work(of mobile phone The accurate identification to voice order can be realized so as to more convenient control aircraft flight action, while coordinate multiple sensors to realize Autonomous hovering function, using GPS/ Big Dipper bimodulus locating modules, make positioning more precisely rapid, realize that dropout returns automatically The function such as boat, fixed point flight, shoot the multiple functions such as avoidance flight in real-time passback and the flight way of video photography and be integrated A kind of inexpensive, high performance six axles aircraft, while reduce the cost for making remote control in kind, also simplify manipulation Difficulty, the master of aircraft is realized using the MCU single-chip microcomputer MKL26Z256VLL4 singlechip microcontrollers of cheap function admirable Want function, design aircraft model machine, and establish simplified model, six axle flying vehicles control flight attitudes of innovative design.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and And in the case of without departing substantially from spirit or essential attributes of the present utility model, it can realize that this practicality is new in other specific forms Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation Involved claim.

Claims (7)

  1. It is 1. a kind of new based on cell phone intelligent APP Voice command aerocraft systems, it is characterised in that:Including four-axle aircraft MKL26 main control modules (1), the four-axle aircraft MKL26 main control modules (1) are connected with human-computer interaction module (2), air-blower control Module (3), GPS module (5), power module (6) and sensor assembly (7), the human-computer interaction module (2) use cell phone application As flight controller, voice order, the four-axle aircraft MKL26 are precisely identified using the speech identifying function of mobile phone The operation of main control module (1) control fan control module (3), the sensor assembly (7) are used for acquisition angles, distance, warm and humid Degree and image recognition information, the four-axle aircraft MKL26 main control modules (1) use No. four electric machine controllers, integrate multiple biographies Sensor.
  2. A kind of new existed 2. according to claim 1 based on cell phone intelligent APP Voice command aerocraft systems, its feature In:The fan control module (3) is using advanced dynamic mixing decay technique control four-axle aircraft rotor (4).
  3. A kind of new existed 3. according to claim 1 based on cell phone intelligent APP Voice command aerocraft systems, its feature In:The four-axle aircraft MKL26 main control modules (1) are also integrated with ESP8266 wireless modules (8), for coordinating independent development Remote control of the cell phone application as aircraft.
  4. A kind of new existed 4. according to claim 1 based on cell phone intelligent APP Voice command aerocraft systems, its feature In:The sensor assembly (7) realizes that autonomous in the air hang is realized in aircraft altitude collection using MS5611-01BA baroceptors Stop function.
  5. A kind of new existed 5. according to claim 1 based on cell phone intelligent APP Voice command aerocraft systems, its feature In:The GPS module (5) uses S1216F8-BD modules.
  6. A kind of new existed 6. according to claim 1 based on cell phone intelligent APP Voice command aerocraft systems, its feature In:The sensor assembly (7) is made up of angular transducer, distance measuring sensor, Temperature Humidity Sensor and imaging sensor.
  7. A kind of new existed 7. according to claim 3 based on cell phone intelligent APP Voice command aerocraft systems, its feature In:The ESP8266 wireless modules (8) are integrated with duplexer, power amplifier, low noise amplifier, filter and power supply pipe Manage module.
CN201720571534.9U 2017-05-22 2017-05-22 It is a kind of new based on cell phone intelligent APP Voice command aerocraft systems Expired - Fee Related CN207173963U (en)

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CN201720571534.9U CN207173963U (en) 2017-05-22 2017-05-22 It is a kind of new based on cell phone intelligent APP Voice command aerocraft systems

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112114540A (en) * 2019-06-19 2020-12-22 上海胤珀信息科技有限公司 Data synchronization linkage method and system of integrated multi-type sensor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112114540A (en) * 2019-06-19 2020-12-22 上海胤珀信息科技有限公司 Data synchronization linkage method and system of integrated multi-type sensor

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Granted publication date: 20180403

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