CN206107559U - Unmanned vehicles based on sharp infrared ray sensor decides highly - Google Patents

Unmanned vehicles based on sharp infrared ray sensor decides highly Download PDF

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Publication number
CN206107559U
CN206107559U CN201621141237.2U CN201621141237U CN206107559U CN 206107559 U CN206107559 U CN 206107559U CN 201621141237 U CN201621141237 U CN 201621141237U CN 206107559 U CN206107559 U CN 206107559U
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CN
China
Prior art keywords
infrared ray
aircraft
sharp
ray sensor
control module
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 - Fee Related
Application number
CN201621141237.2U
Other languages
Chinese (zh)
Inventor
姚锦玮
冯世通
叶彦斐
郑源
王园云
刘睿琛
付士凤
陈荣杰
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Hohai University HHU
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Hohai University HHU
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hohai University HHU filed Critical Hohai University HHU
Priority to CN201621141237.2U priority Critical patent/CN206107559U/en
Application granted granted Critical
Publication of CN206107559U publication Critical patent/CN206107559U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model relates to a high device of aircraft control, specifically speaking relate to one kind to decide high unmanned aerial vehicle aircraft based on infrared sensor. Unmanned vehicles based on sharp infrared ray sensor decides highly, including the aircraft body, the aircraft includes the base, the base is equipped with flight actuating mechanism to the rotor support of outside extension on the rotor support, be equipped with sharp infrared ray sensor on the aircraft, single -chip computer control module links to each other with sharp infrared ray sensor, and sharp infrared ray sensor gives the height finding signal transmission flight height of single -chip computer control module, single -chip computer control module control aircraft body. The utility model provides an unmanned vehicles based on sharp infrared ray sensor decides highly, this aircraft adoption sharp infrared ray sensor confirms flight height's mode, owing to infrared ray sensor is small, light in weight's advantage, can make the bearing capacity of aircraft require to reduce, and the while is owing to that the infrared ray sensor utilization is light detection distance for the CCD detector detects infrared signal sooner, has shortened unmanned vehicles and has decided high processing time, has improved the speed of altitude conversion.

Description

It is a kind of that high unmanned vehicle is determined based on sharp infrared ray sensors
Technical field
This utility model is to be related to a kind of flying vehicles control height devices, is concretely related to a kind of based on infrared biography The fixed high unmanned plane during flying device of sensor.
Background technology
Infrared Sensor System is that with the measuring system that infrared ray is medium, current infrared sensor technology is in the modern times The fields such as science and technology, national defence and industrial or agricultural obtain a wide range of applications.Infrared sensor is radiationless, low-power consumption, it is strong disguised and Inexpensive the characteristics of, causes infrared sensor to be fully used with communication system in infrared distance measurement.
Unmanned plane has been widely used at present traffic scheduling, and logistics distribution, geology detecting, disaster prospecting, rescue refers to Wave, agricultural and building industry etc..Due to its have without personnel's damage risk, deployment flexibly and fast, respond it is timely the features such as in information Scout, the aspect such as safety precaution receives much concern, and civilian unmanned plane market and gradually forms.
Utility model content
This utility model is for above-mentioned deficiency there is provided a kind of based on the fixed high unmanned flight of sharp infrared ray sensors Device.
This utility model is adopted the following technical scheme that:
It is described in the utility model that high unmanned vehicle, including aircraft body are determined based on sharp infrared ray sensors, Aircraft includes pedestal, and the rotor support that pedestal extends laterally, rotor support is provided with flight drive mechanism;Also include Sharp infrared ray sensors, single chip control module;Aircraft is provided with sharp infrared ray sensors, Single-chip Controlling mould Block is connected with sharp infrared ray sensors, and altitude signal is passed to single chip control module by sharp infrared ray sensors, single Piece machine control module controls the flying height of aircraft body.
It is described in the utility model that high unmanned vehicle is determined based on sharp infrared ray sensors.The infrared ray sensing Device is sharp infrared ray sensors, and sharp infrared ray sensors include infrared transmitter and CCD-detector, and its middle infrared (Mid-IR) is sent out Emitter is arranged on aircraft bottom middle position with CCD-detector, and RF transmitter is earthward launched by certain inclination angle Infrared ray, using principle of reflection, by infrared reflection to CCD-detector, CCD-detector is received and produce after infrared ray one Side-play amount, then side-play amount is sent to into single chip control module carries out height computing.
It is described in the utility model that high unmanned vehicle, the Single-chip Controlling are determined based on sharp infrared ray sensors Module includes flight-control computer and motor;The drive module includes rotor and support;The power module includes electric power storage Pond and Voltage stabilizing module.The support is made using PA66+30% ultrastrength materials, and flight-control computer is gold-plated by high intensity Compound PCB composition, extends the life-span of aircraft, enhances the resistance to ability of falling, more environmentally-friendly.
Beneficial effect
What this utility model was provided determines high unmanned vehicle based on sharp infrared ray sensors;The aircraft is adopted Sharp infrared ray sensors determine the mode of flying height, due to infrared ray sensor small volume, lightweight advantage, can make The weight capacity of aircraft requires to reduce, simultaneously because what infrared ray sensor utilized is light detecting distance so that CCD-detector Infrared signal is faster detected, unmanned vehicle is shortened and is determined the high disposal time, improve the speed of altitude conversion.
Description of the drawings
Fig. 1 is top view of this utility model based on the fixed high unmanned plane during flying device of sharp infrared ray sensors;
Fig. 2 is top view of this utility model based on the fixed high unmanned plane during flying device of sharp infrared ray sensors;
Fig. 3 is that this utility model is highly surveyed based on the fixed high unmanned plane during flying device infrared ray of sharp infrared ray sensors Amount schematic diagram.
In figure:1 be rotor, 2 be flight-control computer, 3 be rotor support, 4 be motor one, 5 be motor two, 6 be electricity Machine three, 7 is that motor four, 8 is RF transmitter, 9 is CCD-detector, 10 is battery.
Specific embodiment
To make the purpose and technical scheme of this utility model embodiment clearer, implement below in conjunction with this utility model The accompanying drawing of example, is clearly and completely described to the technical scheme of this utility model embodiment.Obviously, described embodiment It is a part of embodiment of the present utility model, rather than the embodiment of whole.Based on described embodiment of the present utility model, The every other embodiment that those of ordinary skill in the art are obtained on the premise of without the need for creative work, belongs to this practicality Novel protected scope:
It is a kind of as shown in the figure that high unmanned vehicle, including aircraft body, flight are determined based on sharp infrared ray sensors Device includes pedestal, and sharp infrared ray sensors 8, the rotor support 3 that pedestal extends laterally, rotor support 3 is provided with flight Drive mechanism, mid-stent body lays respectively from top to bottom flight-control computer, battery and infrared ray sensor, is flight The main executable portion of device;Aircraft is provided with sharp infrared ray sensors, single chip control module and sharp infrared ray Sensor is connected, and altitude signal is passed to single chip control module, single chip control module control by sharp infrared ray sensors The flying height of aircraft body.Four structures, material, radius identical rotors are equipped with four bracket ends of aircraft, symmetrically It is distributed in the four direction around of body and positioned at same level;Four motors are symmetrically mounted on aircraft parking stand end End
Infrared ray sensor, respectively positioned at body middle part both sides, is divided by RF transmitter 8 and CCD-detector 9 into symmetrical Cloth.
RF transmitter launches light beam according to certain angle, runs into light beam behind ground and reflexes to CCD-detector, CCD inspections Surveying device will obtain side-play amount L, and side-play amount L is sent to into flight-control computer, and flight-control computer is by transmitting The height D of aircraft is calculated after angle [alpha], side-play amount L, centre-to-centre spacing X and focal length f, carries out dynamic regulation to control flight Device flies in certain altitude.
The PA66 that this utility model is related to is nylon polyamide, and polyamide is by amide groups(-CONH-)In high polymer main chain Repeat a kind of high crystalline, the linear type condensation polymer for constituting, with preferably drawing-off intensity, wear resistence be good, chemicals-resistant, The speciality such as self lubricity, PA66 is mechanical strength highest, most widely used kind in PA serial, because its degree of crystallinity it is high, heat-resisting Property is all higher.PA66+30%GF refers to that most unique physical property performance is good mechanical strength, more specifically containing 30% glass Then include obdurability, oil resistivity, self lubricity, the advantages of coefficient of friction is little.
The gold-plated compound PCB of high intensity, Au-plated board high cost for silver-plated, but non-oxidizability By force, conduct electricity very well, anti-wear performance is good, it is ensured that service life.
The above, only this utility model preferably specific embodiment, but protection domain of the present utility model is not This is confined to, any those familiar with the art can readily occur in the technical scope that this utility model is disclosed Change or replacement, all should cover within protection domain of the present utility model.Therefore, protection domain of the present utility model should It is defined by scope of the claims.

Claims (4)

1. a kind of that high unmanned vehicle, including aircraft body are determined based on sharp infrared ray sensors, aircraft includes base Seat, the rotor support that pedestal extends laterally, rotor support is provided with flight drive mechanism;It is characterized in that:Also include sharp Infrared ray sensor, single chip control module;Aircraft is provided with sharp infrared ray sensors, single chip control module with Sharp infrared ray sensors are connected, and altitude signal is passed to single chip control module, single-chip microcomputer by sharp infrared ray sensors Control module controls the flying height of aircraft body.
2. according to claim 1 based on the fixed high unmanned vehicle of sharp infrared ray sensors, it is characterised in that:Institute The sharp infrared ray sensors stated include infrared transmitter, CCD-detector;Described infrared transmitter is arranged with CCD-detector In the bottom of aircraft.
3. according to claim 1 based on the fixed high unmanned vehicle of sharp infrared ray sensors, it is characterised in that:Institute The single chip control module stated includes flight-control computer and motor;Motor is arranged on rotor support, Motor drive rotor Rotation, flight-control computer is used for controlled motor.
4. according to claim 1 based on the fixed high unmanned vehicle of sharp infrared ray sensors, it is characterised in that:Institute The flight controller stated is using gold-plated compound PCB composition.
CN201621141237.2U 2016-10-20 2016-10-20 Unmanned vehicles based on sharp infrared ray sensor decides highly Expired - Fee Related CN206107559U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201621141237.2U CN206107559U (en) 2016-10-20 2016-10-20 Unmanned vehicles based on sharp infrared ray sensor decides highly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201621141237.2U CN206107559U (en) 2016-10-20 2016-10-20 Unmanned vehicles based on sharp infrared ray sensor decides highly

Publications (1)

Publication Number Publication Date
CN206107559U true CN206107559U (en) 2017-04-19

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201621141237.2U Expired - Fee Related CN206107559U (en) 2016-10-20 2016-10-20 Unmanned vehicles based on sharp infrared ray sensor decides highly

Country Status (1)

Country Link
CN (1) CN206107559U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109383776A (en) * 2017-08-02 2019-02-26 百润红科技有限公司 H.D unmanned plane is determined with air pressure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109383776A (en) * 2017-08-02 2019-02-26 百润红科技有限公司 H.D unmanned plane is determined with air pressure

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GR01 Patent grant
GR01 Patent grant
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: 20170419

Termination date: 20191020