CN206557391U - A kind of portable electric UAS - Google Patents
A kind of portable electric UAS Download PDFInfo
- Publication number
- CN206557391U CN206557391U CN201720235333.1U CN201720235333U CN206557391U CN 206557391 U CN206557391 U CN 206557391U CN 201720235333 U CN201720235333 U CN 201720235333U CN 206557391 U CN206557391 U CN 206557391U
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- aircraft
- control
- hand
- portable electric
- earth station
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Abstract
The utility model provides a kind of portable electric unmanned plane, including aircraft and hand-held control earth station；Wherein, the hand-held control earth station is used for mission planning, aircraft control and mission payload manipulation；The aircraft is built-in with avionics system, and the avionics system is used for control and the power management of airborne equipment of the aircraft and its mission payload；The aircraft is detachable flight carrier, including fuselage, the detachable wing positioned at the fuselage both sides and the detachable horizontal tail positioned at afterbody.The utility model single-person portable Drones for surveillance is easy to carry, it is not necessary to extra support vehicles and equipment, greatly reduces use cost.The utility model can realize quick assembling simultaneously, take off rapidly, and hand-held control earth station can carry out trajectory planning in real time according to field conditions, and much sooner, accurately live information is collected.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to a kind of portable electric UAS.
Background technology
Conventional unmanned plane is performing mountain region inspection, during the task such as city anti-terrorism, carries inconvenient, it is necessary to extra service truck
And equipment, considerably increase use cost, in real work, can not usually meet job requirements.
Therefore, prior art is further improved.
Utility model content
In view of this, the utility model be directed to it is a kind of can quickly assemble, portable investigation easy to carry nobody
Machine system, concrete scheme is as follows：
The utility model portable electric UAS includes：Including aircraft and hand-held control earth station；Wherein, institute
Stating hand-held control earth station is used for mission planning, aircraft control and mission payload manipulation；The aircraft is built-in with avionics system
System, the avionics system is used for control and the power management of airborne equipment of the aircraft and its mission payload；It is described to fly
Row device is detachable flight carrier, including fuselage, the detachable wing positioned at the fuselage both sides and positioned at afterbody
Detachable horizontal tail.
Further, in above-mentioned portable electric UAS, the avionics system includes：Flight control computer, avionics
System battery, gps antenna and connector；The flight control computer be used for according to it is described it is hand-held control earth station mission planning,
Aircraft control and mission payload are manipulated to be controlled to aircraft；The avionics system battery is used to calculate for the winged control
Machine, the gps antenna and the connector are powered；The gps antenna is used to position the aircraft；The connector is used for institute
State the connection of flight control computer and the hand-held control earth station communication link.
Further, in above-mentioned portable electric UAS, the flight control computer includes：Pressure-altitude sensor
Module, IMU modules, GPS/ big-dipper satellites locating module, digital signal processor module, I/O Signal-regulated kinases and power supply pipe
Manage module；The pressure-altitude sensor module, the IMU modules, the GPS/ big-dipper satellites locating module, I/O letters
Number conditioning module and the power management module are communicated to connect with the digital signal processor module.
Further, in above-mentioned portable electric UAS, the hand-held control earth station includes：Control device,
Two-way rocker regulation resistance, several physical buttons, display lamp, display screen and the control of hand-held ground electrically connected with the control device
Earth station's battery；The control device is used for the value collection of the rocker regulation resistance positional information and the physical button,
Telemetry simultaneously shows, the decoding of network image information and display, flies control parameter configuration, digital map navigation and data and image note
Address book stored.
Further, in above-mentioned portable electric UAS, the display screen is capacitance touch display screen.
Further, in above-mentioned portable electric UAS, the hand-held ground controls earth station to be lithium with battery
Battery.
Further, in above-mentioned portable electric UAS, the fuselage is the fuselage that composite is made.
Further, in above-mentioned portable electric UAS, the fuselage is the machine that Kev draws aramid fiber composite material
Body.
Further, in above-mentioned portable electric UAS, the fuselage is the machine that Kev draws aramid fiber composite material
Body.
Further, in above-mentioned portable electric UAS, the aircraft is the unmanned scout of single-person portable
Compared with prior art, the utility model passes through independent aircraft, avionics system and hand-held control earth station group
Into portable Drones for surveillance, also, aircraft is detachable flight carrier, that is to say, that all may be used the part such as wing, horizontal tail
It is put into progress dismounting as needed in knapsack, also, the fuselage main body of aircraft is made of composite（For example, Kev
Draw aramid fiber composite material）, only five kilograms of system gross weight, one, which bears, can perform task.Also, single-person portable investigates nothing
It is man-machine easy to carry, it is not necessary to extra support vehicles and equipment, greatly reduce use cost.
Further, since the utility model aircraft, avionics system and these discrete structures of hand-held control earth station can
Quick assembling is realized, is taken off rapidly, also, hand-held control earth station can carry out trajectory planning in real time according to field conditions, more
Plus in time, accurately live information is collected.
Brief description of the drawings
By reading the detailed description of hereafter preferred embodiment, various other advantages and benefit is common for this area
Technical staff will be clear understanding.Accompanying drawing is only used for showing the purpose of preferred embodiment, and is not considered as to this practicality
New limitation.And in whole accompanying drawing, identical part is denoted by the same reference numerals.In the accompanying drawings：
Fig. 1 is the structural representation of the utility model portable electric UAS embodiment；
Fig. 2 is the system block diagram of flight control computer in the utility model portable electric UAS embodiment.
Embodiment
The exemplary embodiment of the disclosure is more fully described below with reference to accompanying drawings.Although showing the disclosure in accompanying drawing
Exemplary embodiment, it being understood, however, that the disclosure is may be realized in various forms, without should be by embodiments set forth here
Limited.On the contrary, these embodiments are provided to facilitate a more thoroughly understanding of the present invention, and can be by the scope of the present disclosure
Complete conveys to those skilled in the art.
Reference picture 1, Fig. 1 is the structural representation of the utility model portable electric unmanned aerial vehicle example.
In this embodiment, portable electric UAS embodiment includes aircraft 1 and hand-held control earth station 2；
Hand-held control earth station 2 is used for mission planning, aircraft control and mission payload and manipulated；Aircraft 1 is built-in with avionics system 3,
The avionics system 3 is used for control and the power management of airborne equipment of aircraft 1 and its mission payload.
Aircraft 1 be detachable flight carrier, including composite fuselage 11, positioned at the detachable of the fuselage both sides
Wing 12 and the detachable horizontal tail 13 positioned at the afterbody of fuselage 11, motor 14, electricity adjust 15, propeller 16 and steering wheel 17.Avionics system
System 3 includes flight control computer 31, avionics system battery 32, gps antenna 33 and connector 34.Flight control computer 31 is used for according to hand
Mission planning, aircraft control and the mission payload manipulation for holding control earth station 3 are controlled to aircraft 1；Avionics system electricity
Pond 32 is used to power for flight control computer 31, gps antenna 33 and connector 34；Gps antenna 33 is used for positioning aircraft 1；Connection
Device 34 is used for the connection of flight control computer 31 and hand-held control earth station 3 communication link.
More particularly, as shown in Fig. 2 flight control computer 31 is to be carried for the hardware required for providing flight control
Body, including：Pressure-altitude sensor module 311, IMU modules 312, GPS/ big-dipper satellites locating module 313, Digital Signal Processing
Device module 314, I/O Signal-regulated kinases 315 and power management module 316；Pressure-altitude sensor module 311, IMU modules
312nd, GPS/ big-dipper satellites locating module 313, I/O Signal-regulated kinases 314 and power management module 316 with data signal
Manage the signal connection of device module 314.
Hand-held control earth station 2 includes hardware circuit 21, two-way rocker regulation resistance 22, touch display screen 23, system shell
24th, one piece of 12V high density lithiums battery 25, control device 26, several physical buttons 27 and highlighted LED display lamps 28.Control device
The 26 value collections for being used for the positional information of rocker regulation resistance 22 and physical button 27, telemetry and show, network image information
Decoding and display, winged control parameter configuration, digital map navigation, data and image record storage.It should be noted that in the present embodiment,
Touch display screen 23 uses one piece of seven cun of capacitance touch display screen, but the size of display screen is not limited, according to reality
Situation is selected.The type of display screen is not also limited, and the display screen outside capacitance touch screen is also protected of the present utility model
Within the scope of shield.In the present embodiment, hand-held ground controls earth station to be lithium battery with battery, but the utility model is not made to this
Limit.Other batteries outside lithium battery are also within protection domain of the present utility model.
Preferably, in the present embodiment, composite fuselage 11 can draw the fuselage of aramid fiber composite material for Kev.
The utility model aircraft body draws aramid fiber composite material material, weight good with pliability using Kev
Gently, it is anti-extrusion, the features such as drop resistant.Flight control system uses the minitype high-performance UAV Flight Control System based on double ARM frameworks,
Communication link is used based on the integral communication link of time-multiplexed ten kilometers of veneer number figures, is placed in by mother daughter board connector and is flown control plate
Top, overall dimension is less than 14cm × 7cm, highly no more than 2cm.Unmanned plane passes through ground using whole control flight before flight
Station software planned task course line with landing course line, hand throw it is winged, after taking off reach certain altitude be transferred to height-lock control automatically, hold
Row airline operation task, is finished automatic according to the landing of default landing course line, whole without any human intervention, autonomous to complete
Aerial mission.Hand-held control earth station is led to by RS422 and network interface with the integral communication link ground surface end of external ground number figure
Letter, ground station software built in hand held controller can plan that uploading course line, display flies data and the figure that control device is returned by link
Picture simultaneously carries out record storage, and only five kilograms of total system gross weight, armamentarium dismounting is finished and can be put into knapsack, and one can carry on the back
Negative execution task.
Preferably, portable Drones for surveillance is the unmanned scout of single-person portable.
Obviously, those skilled in the art can carry out various changes and modification without departing from this practicality to the utility model
New spirit and scope.So, if these modifications and variations of the present utility model belong to the utility model claim and
Within the scope of its equivalent technologies, then the utility model is also intended to comprising including these changes and modification.
Claims (9)
1. a kind of portable electric UAS, it is characterised in that including aircraft and hand-held control earth station；Wherein,
The hand-held control earth station is used for mission planning, aircraft control and mission payload and manipulated；
The aircraft is built-in with avionics system, the avionics system be used for the aircraft and its mission payload control and
The power management of airborne equipment；
The aircraft is detachable flight carrier, including fuselage, detachable wing, Yi Jiwei positioned at the fuselage both sides
In the detachable horizontal tail of afterbody.
2. portable electric UAS according to claim 1, it is characterised in that the avionics system includes：Fly
Control computer, avionics system battery, gps antenna and connector；
The flight control computer is used to be grasped according to mission planning, aircraft control and the mission payload of the hand-held control earth station
It is vertical that aircraft is controlled；
The avionics system battery is used to power for the flight control computer, the gps antenna and the connector；
The gps antenna is used to position the aircraft；
The connector is used for the connection of the flight control computer and the hand-held control earth station communication link.
3. portable electric UAS according to claim 2, it is characterised in that the flight control computer includes：
Pressure-altitude sensor module, IMU modules, GPS/ big-dipper satellites locating module, digital signal processor module, I/O signals are adjusted
Manage module and power management module；
The pressure-altitude sensor module, the IMU modules, the GPS/ big-dipper satellites locating module, the I/O signals are adjusted
Module and the power management module is managed to communicate to connect with the digital signal processor module.
4. portable electric UAS according to claim 3, it is characterised in that the hand-held control earth station bag
Include：Control device, the two-way rocker regulation resistance electrically connected with the control device, several physical buttons, display lamp, display screen and
Hand-held ground control earth station battery；
The control device is used for the value collection of the rocker regulation resistance positional information and the physical button, and telemetry is simultaneously
It has been shown that, the decoding of network image information and display, winged control parameter configuration, digital map navigation and data and image record storage.
5. portable electric UAS according to claim 4, it is characterised in that the display screen is capacitance touch
Display screen.
6. portable electric UAS according to claim 4, it is characterised in that the hand-held ground control ground
It is lithium battery to stand with battery.
7. portable electric UAS according to claim 1, it is characterised in that the fuselage is composite system
Into fuselage.
8. portable electric UAS according to claim 7, it is characterised in that the fuselage is that Kev draws aramid fiber
The fuselage of composite.
9. portable electric UAS according to claim 1, it is characterised in that the aircraft is portable for one
The unmanned scout of formula.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720235333.1U CN206557391U (en) | 2017-03-13 | 2017-03-13 | A kind of portable electric UAS |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720235333.1U CN206557391U (en) | 2017-03-13 | 2017-03-13 | A kind of portable electric UAS |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206557391U true CN206557391U (en) | 2017-10-13 |
Family
ID=60362913
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720235333.1U Expired - Fee Related CN206557391U (en) | 2017-03-13 | 2017-03-13 | A kind of portable electric UAS |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206557391U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111077899A (en) * | 2019-10-25 | 2020-04-28 | 中国航空无线电电子研究所 | Carrier-borne unmanned aerial vehicle wrist strap type handheld control system |
| CN111176322A (en) * | 2019-12-27 | 2020-05-19 | 西安羚控电子科技有限公司 | Outdoor swarm unmanned aerial vehicle confrontation test system |
-
2017
- 2017-03-13 CN CN201720235333.1U patent/CN206557391U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111077899A (en) * | 2019-10-25 | 2020-04-28 | 中国航空无线电电子研究所 | Carrier-borne unmanned aerial vehicle wrist strap type handheld control system |
| CN111176322A (en) * | 2019-12-27 | 2020-05-19 | 西安羚控电子科技有限公司 | Outdoor swarm unmanned aerial vehicle confrontation test system |
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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: 20171013 Termination date: 20210313 |