CN108622431A - Practical vehicle-mounted UAV system - Google Patents
Practical vehicle-mounted UAV system Download PDFInfo
- Publication number
- CN108622431A CN108622431A CN201710199704.XA CN201710199704A CN108622431A CN 108622431 A CN108622431 A CN 108622431A CN 201710199704 A CN201710199704 A CN 201710199704A CN 108622431 A CN108622431 A CN 108622431A
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- China
- Prior art keywords
- unmanned plane
- remote control
- unmanned
- vehicle
- engine room
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- 238000000034 method Methods 0.000 claims abstract description 6
- 230000005611 electricity Effects 0.000 claims description 3
- 206010039203 Road traffic accident Diseases 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/12—Target-seeking control
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Mechanical Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The present invention provides a kind of vehicle-mounted UAV system of practicality, which is made of unmanned engine room, unmanned plane, remote control panel three parts.Unmanned plane determines the position of cabin by the signal of positioning signal transmitter, accuracy higher, it can be achieved that unmanned plane fixed point precision approach, accurately return in cabin.After unmanned plane takes off, positioning signal transmitter sends out positioning signal at any time, it can be achieved that unmanned plane automatic synchronization accompanying flying in vehicle travel process, accompanying flying distance can arbitrarily regulate and control, it is not necessary to which hard ground manual operation does not have to worry that unmanned plane is lost.No matter vehicle is in traveling or halted state, and unmanned plane can accurately return to cabin under positioning signal guide.When contingency occurs in vehicle, system starts emergency mode automatically by impact switch.Under emergency mode, unmanned plane is raised to automatically above the scene of the accident or scene of the accident rear certain distance, and warning lamp is opened in hovering, and accident spot is indicated for rescue personnel, and warning front vehicle pays attention to avoiding, in order to avoid cause second accident.
Description
Technical field
The invention belongs to auto parts machinery and unmanned plane application fields, and in particular to a kind of vehicle-mounted UAV system of practicality.
Background technology
As unmanned plane function is increasing, its application in people's lives is more and more wider.There are some vehicle-mounted nothings at present
The research of man-machine aspect, but be only related to mostly with Navigation of Pilotless Aircraft, detection periphery situation etc..Existing unmanned plane passes through GPS
Or the satellite positionings such as Big Dipper, it is limited by positioning accuracy, pinpoint lands when cannot accomplish to make a return voyage, and is especially unable to precision approach
On vehicle under steam.When traffic accident occurs, it is that rescue personnel indicates accident spot by unmanned plane, is front vehicle
The scene of the accident is warned, avoids second accident, these see using temporary end is related to.
Invention content
The present invention provides a kind of vehicle-mounted UAV system of practicality, and the system is by unmanned engine room, unmanned plane, remote control panel three
Part forms.
The unmanned engine room, it is characterized in that：It is connect by nacelle, hatchcover, positioning signal transmitter, electromagnetism bottom plate, remote signal
Receiving apparatus, charging interface composition.
The nacelle of the unmanned engine room, it is characterized in that：Nacelle is that can accommodate the interior empty box like structure of unmanned plane, is located at roof
The hatchcover of inside, upper end is shared with roof corresponding part, makes unmanned engine room and roof one；As another embodiment, cabin
Body is respectively independent with vehicle, and nacelle can be fixed on to vehicle roof, hood or case cover etc. by existing interconnection technique
Position, nacelle are detachable.
The hatchcover of the unmanned engine room, it is characterized in that：The opening and closing of hatchcover are controlled by the signal that remote control panel is sent out.
The positioning signal transmitter of the unmanned engine room, it is characterized in that：Positioning signal transmitter is located at nacelle bottom centre,
It is a wireless signal transmitter, emits the signal of specific frequency, is connect with the signal of positioning signal reception device on unmanned plane
It is identical to receive frequency.
The electromagnetism bottom plate of the unmanned engine room, it is characterized in that：Electromagnetism bottom plate is located at nacelle lower end, is that the landing of unmanned plane is flat
Platform；Under energized state, electromagnetism bottom plate generates magnetic force and unmanned plane is sucked with fixation, and under off-position, electromagnetism bottom plate does not generate magnetic force
It takes off convenient for unmanned plane.
The remote control signal receiver of the unmanned engine room, it is characterized in that：Remote control signal receiver and remote control panel
Hatchcover switch button corresponds to, and receives the signal of remote control panel hatchcover switch, miscellaneous equipment is sent out accordingly into cabin by data line
Instruction；Specifically, when receiving the signal that hatchcover switch button is opened on remote control panel, remote control signal receiver is into cabin
The instruction that equipment is sent out is：Hatchcover is opened, and positioning signal transmitter is opened, the power-off of electromagnetism bottom plate；When receiving on remote control panel
When the signal that hatchcover switch button is closed, the control instruction that remote control signal receiver is sent out to below deck equipment is：Hatchcover is closed,
Positioning signal transmitter is closed, and electromagnetism bottom plate is powered.
The charging interface of the unmanned engine room, it is characterized in that：Charging interface is the charging connector of unmanned plane, charging wire and cabin
Interior equipment power cord is connected with a vehicle-mounted power supply, and provides electricity.
The unmanned plane, it is characterized in that：There are one accident review lamps on the basis of existing unmanned plane.
The unmanned plane, it is characterized in that：There are one positioning signal reception device, its signals on the basis of existing unmanned plane
Receives frequency is identical as the signal frequency for positioning signal projector transmitting in unmanned engine room.
The remote control panel, it is characterized in that：On the basis of existing no-manned machine distant control panel, there are one hatchcover switch button,
The signal that the button control is sent out can be received by the remote control signal receiver in unmanned engine room, be identified.
The remote control panel, it is characterized in that：On the basis of existing no-manned machine distant control panel, there are one emergency mode switches to press
Button, the button can start the emergency mode in remote control panel.
The remote control panel, it is characterized in that：On the basis of existing no-manned machine distant control panel, there are one emergency modes, specifically
, remote control panel is sent out from trend unmanned engine room and unmanned plane as given an order when the emergency mode：Hatchcover is opened, positioning signal
Transmitter is opened, and the power-off of electromagnetism bottom plate, unmanned plane accident review lamp is bright, 0.5~30 meter of unmanned plane rising, and unmanned plane retrogressing 0~
100 meters, unmanned plane hovering.
The remote control panel, it is characterized in that：On the basis of existing no-manned machine distant control panel, there are one impact switches, are feeling
When should arrive great collision, impact switch starts the emergency mode in remote control panel automatically immediately.
The beneficial effects of the invention are as follows：Unmanned engine room is installed on vehicle, is carried when people being made to go on a journey, is more square using unmanned plane
Just.Unmanned plane determines the position of cabin by the signal of positioning signal transmitter, more true by GPS or Big Dipper satellite signal than existing
Surely an accuracy higher of making a return voyage, it can be achieved that unmanned plane fixed point precision approach, accurately return in cabin.After unmanned plane takes off, positioning
Signal projector is all sending out positioning signal, it can be achieved that unmanned plane automatic synchronization accompanying flying in vehicle travel process, accompanying flying at any time
Distance can arbitrarily regulate and control, it is not necessary to which hard ground manual operation does not have to worry that unmanned plane is lost.No matter vehicle is travelling or is stopping shape
State, unmanned plane can accurately return to cabin under positioning signal guide.
When contingency occurs in vehicle, system starts emergency mode automatically by the inductor of impact switch.Urgent mould
Under formula, unmanned plane rises to automatically above the scene of the accident or scene of the accident rear certain distance, and hovering opens warning lamp, to rescue
It helps personnel and indicates accident spot, warning front vehicle pays attention to avoiding, in order to avoid cause second accident.
Description of the drawings
Fig. 1 is unmanned engine room cross-sectional view of the structure in the present invention.
Fig. 2 is the schematic diagram of unmanned engine room installation site on vehicle in the present invention.
Fig. 3 is the schematic diagram of unmanned engine room installation site another embodiment on vehicle in the present invention.
Wherein, 1- roofs, 2- hatchcovers, 3- nacelles, 4- below deck equipment power cords, 5- charging interfaces, the transmitting of 6- positioning signals
Device, 7- electromagnetism bottom plates, 8- remote control signal receivers, 9- data lines.
Specific implementation mode
The vehicle-mounted UAV system of practicality provided by the invention is made of unmanned engine room, unmanned plane, remote control panel three parts.
As shown in Figure 1, the unmanned engine room, by nacelle 3, hatchcover 2, positioning signal transmitter 6, electromagnetism bottom plate 7, remote control
Signal receiving device 8, charging interface 5 form, and include additionally necessary below deck equipment power cord 4 and data line 9.
As shown in Fig. 2, nacelle 3 is that can accommodate the interior empty box like structure of unmanned plane, it is located at 1 inside of roof, the hatchcover 2 of upper end
It is shared with 1 corresponding part of roof, make unmanned engine room and 1 one of roof；As shown in figure 3, as another embodiment, nacelle 3
It is respectively independent with vehicle, nacelle can be fixed on by existing interconnection technique by vehicle roof, hood or case cover equipotential
It sets, nacelle 3 is detachable.
The opening and closing of the hatchcover 2 are controlled by the signal that remote control panel is sent out, and specific opening and closing action can
It is achieved by the prior art, is such as realized using the mechanical device of existing vehicle dormer window.
The positioning signal transmitter 6 is located at 3 bottom centre of nacelle, it is a wireless signal transmitter, and transmitting is specific
The signal of frequency, it is identical as the frequency reception signal of positioning signal reception device on unmanned plane, avoid the interference of other signals.
The electromagnetism bottom plate 7 is located at 3 lower end of nacelle, is the landing platform of unmanned plane.Under energized state, electromagnetism bottom plate 7 produces
Unmanned plane is sucked with fixation in magnetisation power, and under off-position, electromagnetism bottom plate 7 does not generate magnetic force and takes off convenient for unmanned plane.
The remote control signal receiver 8 is corresponding with the hatchcover switch button of remote control panel, can receive remote control panel and send out
Wireless signal, and into cabin, miscellaneous equipment sends out command adapted thereto by data line 9；Specifically, when receiving on remote control panel
When the signal that hatchcover switch button is opened, the instruction that remote control signal receiver 8 is sent out to below deck equipment is：Hatchcover 2 is opened, fixed
Position signal projector 6 is opened, and electromagnetism bottom plate 7 powers off；It is distant when receiving the signal that hatchcover switch button is closed on remote control panel
Controlling the control instruction that signal receiving device 8 is sent out to below deck equipment is：Hatchcover 2 is closed, and positioning signal transmitter 6 is closed, electromagnetism
Bottom plate 7 is powered.
The charging interface 5 is that the charging connector of unmanned plane, charging wire and below deck equipment power cord 4 connect with vehicle power supply
It connects, electricity is provided for below deck equipment operation.
The unmanned plane installs an accident review lamp on the basis of existing unmanned plane；It is installed on the basis of existing unmanned plane
One positioning signal reception device, the signal frequency that it receives signal frequency with positioning signal projector 6 emits in unmanned engine room
It is identical.
The remote control panel is to increase a hatchcover switch button, the button on the basis of existing no-manned machine distant control panel
The signal sent out can be received by the remote control signal receiver 8 in unmanned engine room, be identified；On existing no-manned machine distant control panel basis
On, increase an emergency mode switch button, can start emergency mode in remote control panel by pressing the button；It is described urgent
Mode instruction string routine is as follows：Hatchcover 2 is opened, and positioning signal transmitter 6 is opened, and electromagnetism bottom plate 7 powers off, unmanned plane accident review
Lamp is bright, and unmanned plane rises 0.5~30 meter, and unmanned plane retreats 0~100 meter, unmanned plane hovering；In existing no-manned machine distant control panel base
On plinth, an impact switch is installed, the colliding sensor in switch starts remote control face automatically immediately when sensing great collision
Emergency mode in plate.
There is a this vehicle-mounted unmanned aerial vehicle system, when trip, unmanned plane is placed in unmanned engine room, by shaking control panel side
Just it is used.The real-time position signal sent out by positioning signal transmitter 6, unmanned function realize fixed point precision approach,
Accurately return in cabin；Unmanned plane automatic synchronization accompanying flying in vehicle travel process, the arbitrary regulation and control of accompanying flying distance, it is not necessary to take can be achieved
Strength ground manual operation is all being moved due to vehicle and unmanned plane without worrying, unmanned plane is caused to lose；No matter vehicle traveling or
Halted state, unmanned plane can accurately return to cabin.Traffic accident is occurring for emergency mode through the invention, unmanned function
When, it is raised to automatically above the scene of the accident or scene of the accident rear certain distance, hovering warns, with indicating accident for rescue personnel
Point, while front vehicle being warned to pay attention to avoiding, in order to avoid cause second accident.
Within the spirit and principles in the present invention, made by change, improve, should all be included in protection scope of the present invention it
It is interior.
Claims (14)
1. a kind of vehicle-mounted UAV system of practicality, it is characterized in that：It is made of unmanned engine room, unmanned plane, remote control panel three parts.
2. the unmanned engine room of practical vehicle-mounted UAV system according to claim 1, it is characterized in that：The unmanned engine room is by cabin
Body, hatchcover, positioning signal transmitter, electromagnetism bottom plate, remote control signal receiver, charging interface composition.
3. the nacelle of unmanned engine room according to claim 2, it is characterized in that：Nacelle is that can accommodate the interior sylphon shape knot of unmanned plane
Structure is located on the inside of roof, common to the hatchcover and roof corresponding part of upper end, makes unmanned engine room and roof one；As another
Kind of embodiment, nacelle is respectively independent with vehicle, by existing interconnection technique by nacelle be fixed on vehicle roof, hood or
The positions such as case cover, nacelle are detachable.
4. the hatchcover of unmanned engine room according to claim 2, it is characterized in that：The opening and closing of hatchcover are sent out by remote control panel
Signal control.
5. the positioning signal transmitter of unmanned engine room according to claim 2, it is characterized in that：Positioning signal transmitter is located at cabin
Body bottom centre, it is a wireless signal transmitter, emits the signal of specific frequency, is filled with positioning signal reception on unmanned plane
The frequency reception signal set is identical.
6. the electromagnetism bottom plate of unmanned engine room according to claim 2, it is characterized in that：Electromagnetism bottom plate is located at nacelle lower end, is nothing
Man-machine landing platform.
7. the remote control signal receiver of unmanned engine room according to claim 2, it is characterized in that：Remote control signal receiver with
The hatchcover switch button of remote control panel corresponds to, and receives the signal of remote control panel hatchcover switch, is set by the way that data line is other into cabin
Preparation goes out command adapted thereto；When receiving the signal that hatchcover switch button on remote control panel is opened, remote control signal receiver to
The instruction that below deck equipment is sent out is：Hatchcover is opened, and positioning signal transmitter is opened, the power-off of electromagnetism bottom plate；When the remote control face of receiving
When the signal that hatchcover switch button is closed on plate, the control instruction that remote control signal receiver is sent out to below deck equipment is：Hatchcover
It closes, positioning signal transmitter is closed, and electromagnetism bottom plate is powered.
8. the charging interface of unmanned engine room according to claim 2, it is characterized in that：Charging interface is the charging of unmanned plane
Head, charging wire and below deck equipment power cord are connected with a vehicle-mounted power supply, and provide electricity.
9. the unmanned plane of practical vehicle-mounted UAV system according to claim 1, it is characterized in that：The unmanned plane is in existing nothing
There are one accident review lamps on the basis of man-machine.
10. the unmanned plane of practical vehicle-mounted UAV system according to claim 1, it is characterized in that：On existing unmanned plane basis
It is upper that there are one positioning signal reception device, the signals of its frequency reception signal and positioning signal projector transmitting in unmanned engine room
Frequency is identical.
11. the remote control panel of practical vehicle-mounted UAV system according to claim 1, it is characterized in that：It is distant in existing unmanned plane
On the basis of controlling panel, there are one hatchcover switch buttons.
12. the remote control panel of practical vehicle-mounted UAV system according to claim 1, it is characterized in that：It is distant in existing unmanned plane
On the basis of controlling panel, there are one emergency mode switch button, which can start the emergency mode in remote control panel.
13. the remote control panel of practical vehicle-mounted UAV system according to claim 1, it is characterized in that：It is distant in existing unmanned plane
On the basis of controlling panel, there are one emergency mode, remote control panel is sent out from trend unmanned engine room and unmanned plane when the emergency mode
Such as give an order：Hatchcover is opened, and positioning signal transmitter is opened, and the power-off of electromagnetism bottom plate, unmanned plane accident review lamp is bright, on unmanned plane
0.5~30 meter is risen, unmanned plane retreats 0~100 meter, unmanned plane hovering.
14. the remote control panel of practical vehicle-mounted UAV system according to claim 1, it is characterized in that：It is distant in existing unmanned plane
On the basis of controlling panel, there are one impact switches, and when sensing great collision, impact switch starts in remote control panel automatically immediately
Emergency mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710199704.XA CN108622431A (en) | 2017-03-24 | 2017-03-24 | Practical vehicle-mounted UAV system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710199704.XA CN108622431A (en) | 2017-03-24 | 2017-03-24 | Practical vehicle-mounted UAV system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108622431A true CN108622431A (en) | 2018-10-09 |
Family
ID=63707898
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710199704.XA Withdrawn CN108622431A (en) | 2017-03-24 | 2017-03-24 | Practical vehicle-mounted UAV system |
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| Country | Link |
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| CN (1) | CN108622431A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111071162A (en) * | 2019-12-10 | 2020-04-28 | 苏州智加科技有限公司 | Sensor mounting and dismounting method and vehicle |
| CN111810368A (en) * | 2020-08-09 | 2020-10-23 | 西安热工研究院有限公司 | Unmanned aerial vehicle deployment device and method for wind power cabin |
| CN115384386A (en) * | 2022-09-26 | 2022-11-25 | 浙江吉利控股集团有限公司 | Vehicle-mounted unmanned aerial vehicle |
| CN115439767A (en) * | 2022-11-08 | 2022-12-06 | 深圳互酷科技有限公司 | Unmanned aerial vehicle accident evidence obtaining method and system, terminal equipment and medium |
| CN116071921A (en) * | 2023-01-10 | 2023-05-05 | 深圳市有方科技股份有限公司 | Traffic warning method and related device |
-
2017
- 2017-03-24 CN CN201710199704.XA patent/CN108622431A/en not_active Withdrawn
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111071162A (en) * | 2019-12-10 | 2020-04-28 | 苏州智加科技有限公司 | Sensor mounting and dismounting method and vehicle |
| CN111071162B (en) * | 2019-12-10 | 2021-07-30 | 苏州智加科技有限公司 | Sensor mounting and dismounting method and vehicle |
| CN111810368A (en) * | 2020-08-09 | 2020-10-23 | 西安热工研究院有限公司 | Unmanned aerial vehicle deployment device and method for wind power cabin |
| CN115384386A (en) * | 2022-09-26 | 2022-11-25 | 浙江吉利控股集团有限公司 | Vehicle-mounted unmanned aerial vehicle |
| CN115439767A (en) * | 2022-11-08 | 2022-12-06 | 深圳互酷科技有限公司 | Unmanned aerial vehicle accident evidence obtaining method and system, terminal equipment and medium |
| CN116071921A (en) * | 2023-01-10 | 2023-05-05 | 深圳市有方科技股份有限公司 | Traffic warning method and related device |
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| PB01 | Publication | ||
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Application publication date: 20181009 |