CN206107559U - Unmanned vehicles based on sharp infrared ray sensor decides highly - Google Patents
Unmanned vehicles based on sharp infrared ray sensor decides highly Download PDFInfo
- 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
- Authority
- 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
Links
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
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.
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
ID=58526595
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)
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 |
-
2016
- 2016-10-20 CN CN201621141237.2U patent/CN206107559U/en not_active Expired - Fee Related
Cited By (1)
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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103869819B (en) | A kind of ribbon conveyer automatic detecting method based on many rotor wing unmanned aerial vehicles | |
CN202071987U (en) | Unmanned helicopter for patrolling power transmission lines | |
RU2619160C2 (en) | Devices for critical surface state detection | |
WO2006085804A1 (en) | Line inspection | |
CN205554567U (en) | Take many rotors unmanned vehicles of buffer stop | |
CN110296845A (en) | A kind of coaxial double-oar unmanned plane dynamic test device | |
CN107037845A (en) | One kind is taken photo by plane UAV Flight Control System | |
CN206107559U (en) | Unmanned vehicles based on sharp infrared ray sensor decides highly | |
CN106828890B (en) | A kind of UAV system of patrolling power transmission lines | |
CN104514686B (en) | A kind of device and method of real-time monitoring blower fan tower barrel running status | |
CN205203409U (en) | Unmanned helicopter descending positioning system | |
US20160122010A1 (en) | Aerial vehicle | |
CN201952753U (en) | Sensor | |
CN205656309U (en) | Small -size infrared distance measuring device | |
CN112750316A (en) | Intelligent induction and agglomerate fog detection device, system and method | |
CN105228294A (en) | Lighting device regulates the method for brightness, lighting device and illuminator | |
CN205861918U (en) | A kind of road surfaces knot ice detecting device | |
CN202092633U (en) | Laser ranging and positioning system | |
CN108313277A (en) | A kind of patrol unmanned machine of monitoring | |
CN108592810A (en) | A kind of airscrew pyramidal angle and paddle distance measurement system of helicopter | |
CN108238272A (en) | A kind of UAV system for being used to monitor air quality | |
CN204615733U (en) | Solar cell system and aircraft | |
CN206095290U (en) | Environmental information collection system based on four rotor crafts | |
CN205734876U (en) | Portable Flexible Building Structures measuring robots | |
CN110171417A (en) | Constant-speed cruising device based on laser radar |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
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 |