CN205620554U - A device for recovering unmanned aerial vehicle that falls - Google Patents
A device for recovering unmanned aerial vehicle that falls Download PDFInfo
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- CN205620554U CN205620554U CN201521111617.7U CN201521111617U CN205620554U CN 205620554 U CN205620554 U CN 205620554U CN 201521111617 U CN201521111617 U CN 201521111617U CN 205620554 U CN205620554 U CN 205620554U
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Abstract
The utility model discloses a device for recovering unmanned aerial vehicle that falls, the device is including setting up on unmanned aerial vehicle and interconnect's air crash monitoring module and the power module that has the locate function, air crash monitoring module and unmanned aerial vehicle's drivetrain parts is connected, whether a control signal to power module is exported in unusual control to be used for real -time supervision drivetrain parts, power module supplies power to unmanned aerial vehicle, cut off the unmanned aerial vehicle power supply and start the locate function when receiving a control signal and send current positional information, the utility model has the advantages of simple structure, required with low costs, can retrieve fast and fall unmanned aerial vehicle and retrieve the rate of accuracy height.
Description
Technical field
This utility model relates to unmanned air vehicle technique field, particularly relates to a kind of device for recovering the unmanned plane that falls.
Background technology
Along with developing rapidly of unmanned air vehicle technique, various types of unmanned planes continue to bring out, unmanned plane is also widely used in various environment, such as, perform various special shooting task by unmanned plane or lift-launch ultra high-definition photographic head carries out specialty and takes photo by plane, it is possible to provide the user the precious the resources of movie & TV of various visual angles；By equipping the police type unmanned plane of Infrared pod, then can assist to perform investigation tasks, reduction scene of a crime etc., the video data being now stored on unmanned plane also tends to as important evidentiary material.
Owing to the technology of unmanned plane is the most limited, its stability is the highest, is frequently present of the problems such as misoperation in addition, thus the situation of unmanned plane " missing ", " air crash " etc. emerges in an endless stream in practical flight.Although existing unmanned plane is generally all equipped with alignment system; can in flight course the position of real-time positioning unmanned plane; but when there is air crash; the power supply of unmanned plane would generally be excessive or short-circuit and burn out due to internal current; thus each system typically each cannot normally work in unmanned plane, the position of unmanned plane more cannot be navigated to by the alignment system of the original lift-launch of unmanned plane.And once unmanned plane generation air crash cannot be recovered, being stored in carry-on precious television data etc. and all will be unable to recover, cause the loss of data information, the most generally price comparison of unmanned plane is expensive, the most also can cause certain economic loss.
Utility model content
The technical problems to be solved in the utility model be that for prior art exist technical problem, this utility model provide a kind of simple in construction, with low cost, can quickly recover and fall unmanned plane and recover the device for recovering the unmanned plane that falls that accuracy rate is high.
For solving above-mentioned technical problem, the technical scheme that the utility model proposes is:
A kind of device for recovering the unmanned plane that falls, including being arranged on unmanned plane and interconnective air crash monitoring module and there is the power module of positioning function, described air crash monitoring module is connected with the power section of unmanned plane, for in real time monitoring described power section whether exception and controlling to export first and control signal to described power module, described power module, for powering to unmanned plane, cuts off the power supply to unmanned plane and starts positioning function transmission current location information when receiving described first control signal.
Further improvement as this utility model device: described power module is the battery module being integrated with GPS positioning unit, by described GPS positioning unit positioning position information and be transmitted.
Further improvement as this utility model device: described battery module includes battery core unit, the first switch element and the GPS positioning unit being sequentially connected with, described GPS positioning unit controls to access described battery core unit by described first switch element；The first switch K1 that described first switch element includes being connected in series and second switch K2, described first switch K1 for receiving the second control signal and execution is cut-off are connected with described air crash monitoring module.
Further improvement as this utility model device: described battery module also includes that the network service end unit for being transmitted by network by positional information, described network service end unit are connected with described GPS positioning unit.
Further improvement as this utility model device: described air crash monitoring module is connected by second switch unit with described power module, controls the power supply to unmanned plane of the described power module by described second switch unit.
Further improvement as this utility model device: described air crash monitoring module is adjusted with the motor in unmanned plane power section and/or electricity and is connected.
Compared with prior art, the utility model has the advantage of:
1) this utility model monitors the power section of unmanned plane in real time by air crash monitoring module, the possibility of air crash is determined whether with the flight operating mode of monitoring unmanned plane in real time, if monitor power section exception, then control power module and cut off the power supply of outside unmanned plane, can with effective guarantee power module will not due to during air crash produce big electric current or UAS internal short circuits and burn out, start the positioning function in power module simultaneously, the position that unmanned plane falls can be accurately positioned, the unmanned plane fallen then can be quickly recovered according to the position navigated to, reduce the loss caused by air crash, efficiently solve the problem that unmanned plane recovers difficulty because the reasons such as artificial air crash or non-artificial machine of delaying cause positional information to be lost；
2) this utility model is by configuring the power module with positioning function, in conjunction with the real-time monitoring to air crash operating mode of the air crash monitoring module, when nominal situation, power module is that unmanned plane is powered, then started positioning function when air crash operating mode to position the position of the unmanned plane fallen, it is capable of intelligent power supply and intelligent positioning function, it is ensured that while being accurately positioned during air crash operating mode, reduce required power consumption；
3) whether this utility model air crash monitoring module produces abnormal torque by the motor of monitoring unmanned plane in real time further, the electricity of unmanned plane adjusts whether monitor unmanned plane without output electric current, is all capable of effective monitoring for artificial air crash or non-artificial machine operating mode of delaying；After once monitoring abnormal torque or curent change, by output control signal control cut off the electricity supply immediately module external all power supply, it is ensured that power module is not burned such that it is able to be actuated for location；
4) this utility model GPS positioning unit controls to access battery core unit by the first switch element further, such that it is able to control the unlatching of positioning function, closedown easily, when being in nominal situation, the first switch element disconnects so that be held in position function closed mode to reduce kwh loss；When being in air crash operating mode, the first switch element Guan Bi positions to drive, it is achieved the intelligent positioning of unmanned plane air crash operating mode；
5) this utility model the first switch element controls to start the positioning function of power module further by the first switch K1 and second switch K2 being connected in series, the first control signal exported by air crash monitoring module controls the first switch K1 Guan Bi, second switch K2 then is controlled to cut-off state by the second control signal, only switch K1 when first, the positioning function of power module could be started when second switch K2 all closes, arranged by the redundancy combining two switches, the intelligent starting of positioning function can be realized in real time according to the monitoring result of air crash monitoring module, can control the most easily to close positioning function to reduce self power consumption of power module as far as possible simultaneously.
Accompanying drawing explanation
Fig. 1 is that the present embodiment is for recovering the structural representation of the device of the unmanned plane that falls.
Fig. 2 is the present embodiment realizes principle schematic for recover the unmanned plane that falls.
Fig. 3 is that this utility model applies workflow schematic diagram in a particular embodiment for the device recovering the unmanned plane that falls.
Marginal data: 1, air crash monitoring module；2, power module；21, battery core unit；22, the first switch element；23, GPS positioning unit；24, network service end unit；3, second switch unit.
Detailed description of the invention
Below in conjunction with Figure of description and concrete preferred embodiment, this utility model is further described, but the most therefore limits protection domain of the present utility model.
As shown in Figure 1, 2, the present embodiment is for recovering the device of the unmanned plane that falls, including being arranged on unmanned plane and interconnective air crash monitoring module 1 and there is the power module 2 of positioning function, air crash monitoring module 1 is connected with the power section of unmanned plane, output first controls signal to power module 2 in real time monitoring power section whether exception and when controlling exception, power module 2, for powering to unmanned plane, cuts off the power supply to unmanned plane upon receiving the first control signal and starts positioning function transmission current location information.
The present embodiment monitors the power section of unmanned plane in real time by air crash monitoring module 1, the possibility of air crash is determined whether there is with the flight operating mode of monitoring unmanned plane in real time, if monitor power section exception, then air crash monitoring module 1 exports first and controls signal to power module 2, after power module 2 receives, cut off outside to the power supply of unmanned plane, such that it is able to effective guarantee power module 2 will not due to during air crash produce big electric current or UAS internal short circuits and burn out, start the positioning function in power module 2 simultaneously, the position that unmanned plane falls can be accurately positioned, the unmanned plane fallen then can be quickly recovered according to the position navigated to, reduce the loss caused by air crash, efficiently solve the problem that unmanned plane recovers difficulty because the reasons such as artificial air crash or non-artificial machine of delaying cause positional information to be lost.
The present embodiment is by configuring the power module 2 with positioning function, in conjunction with the air crash monitoring module 1 real-time monitoring to air crash operating mode, when nominal situation, power module 2 is powered for unmanned plane, is then started positioning function when air crash operating mode to position the position of the unmanned plane fallen, it is capable of intelligent power supply and intelligent positioning function, it is ensured that while being accurately positioned during air crash operating mode, reduce required power consumption.
In the present embodiment, power module 2 is the battery module being integrated with GPS positioning unit 23, by GPS positioning unit 23 positioning position information and be transmitted；GPS positioning unit 23 specifically includes GPS locator unit and coordinate position sends subelement, GPS locator cell location gps coordinate positional information, sends subelement by coordinate position and is transmitted.The present embodiment unmanned plane is using battery as power supply, and battery module specifically can use the form of battery case, at battery case built-in GPS positioning unit 23；Battery module gets final product positioning GPS coordinate position by starting built-in GPS positioning unit 23, thus the co-ordinate position information sent according to feedback can quickly recover the unmanned plane fallen.The most in other embodiments, power module 2 may be used without other location modes such as Internet location, or use the mode of multiple positioning modes combination to improve positioning precision further.
As it is shown in figure 1, the present embodiment battery module includes battery core unit the 21, first switch element 22 and GPS positioning unit 23 being sequentially connected with, GPS positioning unit 23 controls to access battery core unit 21 by the first switch element 22.When being in nominal situation, the first switch element 22 disconnects, and i.e. disconnects the connection of GPS positioning unit 23 and battery core unit 21 so that be held in position function closed mode, reduces kwh loss；When being in air crash operating mode, when i.e. air crash monitoring module 1 monitors power section exception, first switch element 22 closes, in-line power is carried out for GPS positioning unit 23 by battery core unit 21, GPS positioning unit 23 is driven to be actuated for location, location is transmitted after getting unmanned plane current location information, it is achieved the intelligent positioning of unmanned plane air crash operating mode.
In the present embodiment, the first switch element 22 specifically includes the first switch K1 being connected in series and is connected with air crash monitoring module 1 for the second switch K2 receiving the second control signal and execution is cut-off, the first switch K1；During original state, first to switch K1 be off-state, the first control signal exported by air crash monitoring module 1 controls the first switch K1 Guan Bi, second switch K2 then is controlled to cut-off state by the second control signal, second control signal can be manual switching signal or external input control signal etc., only could close GPS positioning unit 23 when the first switch K1, second switch K2 all closes and start the positioning function of power module 2.First switch element 22 is arranged by the redundancy combining two switches, the intelligent starting of positioning function can be realized in real time according to the monitoring result of air crash monitoring module 1, can control the most easily to close positioning function to reduce self power consumption of power module 2 as far as possible simultaneously.Second switch K2 specifically can use manual physical control to switch, open and close by controlling positioning function manually, when power module 2 when storage stage or unmanned plane do not carry out aerial mission also or air crash risk can undertake and during without enabling positioning function, can manually disconnect second switch K2, it is to avoid cause power module 2 self to produce too much power consumption；When unmanned plane needs execution task and needs the positioning function enabling power module 2, manual closing second switch K2 in advance, the positioning function making power module 2 built-in in conjunction with the first switch K1 can normally work.
The present embodiment is that the GPS positioning unit 23 being built-in by power module 2 is powered, the most in other embodiments, it is also possible to arranging independent stand-by power supply according to demand is that GPS positioning unit 23 is powered, and is further ensured that the power supply reliability of GPS positioning unit 23.
In the present embodiment, battery module also includes the network service end unit 24 for being transmitted by positional information by network, network service end unit 24 is connected with GPS positioning unit 23, by network service end unit 24, the positional information that GPS positioning unit 23 navigates to is uploaded to network, it is possible to facilitate user to acquire the unmanned plane positional information of location in time.The present embodiment network service end unit 24 specifically uses communication card, communication card is built in battery module and is connected to the outfan of GPS positioning unit 23, after GPS positioning unit 23 navigates to co-ordinate position information, Internet is connected by driving built-in communication to link, the co-ordinate position information of acquisition can be uploaded in the server of appointment IP, thus user can get desired position information from the server specifying IP easily.The positional information that obtains of location, it is also possible to use in power module built-in several leaflets unit to be transmitted passing the mode such as earth station or other remote terminals back.
In the present embodiment, air crash monitoring module 1 is connected by second switch unit 3 with power module 2, controls power module 2 by second switch unit 3 and powers to unmanned plane.Second switch unit 3 is connected with the feeder ear of unmanned plane, and during unmanned plane nominal situation, second switch unit 3 closes, and power module 2 is to unmanned plane normal power supply；When being in air crash operating mode, when i.e. air crash monitoring module 1 monitors power section exception, disconnect the second switch unit 3 externally fed with deenergization module 2 immediately, it is ensured that power module 2 is not burned；After the externally fed of module of cutting off the electricity supply 2, the built-in system of power module 2 can be started working.Second switch unit 3 specifically can be arranged on power module 2 or separately positioned with power module 2 etc. according to the actual requirements.
As shown in Figure 2, in the present embodiment, air crash monitoring module 1 is adjusted with the motor in unmanned plane power section and electricity and is connected, transfer to monitor the air crash operating mode of unmanned plane by motor and electricity in monitoring unmanned plane power section, by monitoring the state that in unmanned plane power section, motor and electricity are adjusted simultaneously, with combine electric mechanical, electrical tune state change improve monitoring accuracy further, certain air crash monitoring module 1 also can more simply by monitoring motor or electricity transfer monitor unmanned plane.When unmanned plane air crash moment, motor can be made to produce abnormal torque owing to barrier stops propeller；When the system malfunctions of unmanned plane and during motor stall aloft, certain electricity in unmanned plane then can be made to adjust without output electric current, whether the present embodiment air crash monitoring module 1 produces abnormal torque by the motor of monitoring unmanned plane in real time, the electricity of unmanned plane adjusts whether monitor unmanned plane without output electric current, is all capable of effective monitoring for artificial air crash or non-artificial machine operating mode of delaying；After once monitoring abnormal torque or curent change, by output control signal control cut off the electricity supply immediately module 2 external all power supply, it is ensured that power module 2 is not burned such that it is able to be actuated for location.Certainly the most in other embodiments, air crash monitoring module 1 also can monitor in unmanned plane machine except electric mechanical, electrical tune in addition to other Power Components to monitor the air crash operating mode of unmanned plane further, or directly monitors the simplest monitoring mode of realization such as output electric current of power module 2.
As it is shown on figure 3, power module 2 uses the battery case being built-in with GPS positioning unit 23, battery inside circuit structure is as shown in Figure 1；When there is air crash in UAV targets, moment air crash monitoring module 1 in air crash can detect that motor produces abnormal torque or electricity is adjusted without output electric current, air crash monitoring module 1 exports the first control signal, disconnection second switch unit 3 controls power module 2 and disconnects externally fed immediately, it is closed at the first switch element 22 of battery inside to open battery inside system power supply, GPS positioning unit 23 is actuated for location after closing power supply, obtain present co-ordinate position information, and be uploaded to specify the server of IP by network service end unit 24；User side can recover the unmanned plane fallen after getting elements of a fix positional information, Orientation on map etc. specifically can be applied according to coordinate position to navigate to the position of unmanned plane, the fastest route looked for an opportunity further according to the position calculation navigated to, it is simple to quickly recover unmanned plane.
Above-mentioned simply preferred embodiment of the present utility model, not makees any pro forma restriction to this utility model.Although this utility model is disclosed above with preferred embodiment, but it is not limited to this utility model.Therefore, every content without departing from technical solutions of the utility model, according to this utility model technical spirit to any simple modification made for any of the above embodiments, equivalent variations and modification, all should fall in the range of technical solutions of the utility model are protected.
Claims (6)
1. the device being used for recovering the unmanned plane that falls, it is characterized in that including being arranged on unmanned plane and interconnective air crash monitoring module (1) and there is the power module (2) of positioning function, described air crash monitoring module (1) is connected with the power section of unmanned plane, described power section is monitored the most extremely in real time, and output first controls signal to described power module (2) when controlling exception, described power module (2) is for powering to unmanned plane, cut off the power supply to unmanned plane when receiving described first control signal and start positioning function transmission current location information.
Device for recovering the unmanned plane that falls the most according to claim 1, it is characterised in that: described power module (2) is the battery module being integrated with GPS positioning unit (23), by described GPS positioning unit (23) positioning position information and be transmitted.
Device for recovering the unmanned plane that falls the most according to claim 2, it is characterized in that: described battery module includes battery core unit (21), the first switch element (22) and the GPS positioning unit (23) being sequentially connected with, described GPS positioning unit (23) controls to access described battery core unit (21) by described first switch element (22)；The first switch K1 that described first switch element (22) includes being connected in series and second switch K2, described first switch K1 for receiving the second control signal and execution is cut-off are connected with described air crash monitoring module (1).
Device for recovering the unmanned plane that falls the most according to claim 3, it is characterized in that: described battery module also includes that the network service end unit (24) for being transmitted by network by positional information, described network service end unit (24) are connected with described GPS positioning unit (23).
5. according to the device for recovering the unmanned plane that falls described in any one in Claims 1 to 4, it is characterized in that: described air crash monitoring module (1) is connected by second switch unit (3) with described power module (2), controls described power module (2) to the power supply of unmanned plane by described second switch unit (3).
6. according to the device for recovering the unmanned plane that falls described in any one in Claims 1 to 4, it is characterised in that: described air crash monitoring module (1) is adjusted with the motor in unmanned plane power section and/or electricity and is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521111617.7U CN205620554U (en) | 2015-12-29 | 2015-12-29 | A device for recovering unmanned aerial vehicle that falls |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521111617.7U CN205620554U (en) | 2015-12-29 | 2015-12-29 | A device for recovering unmanned aerial vehicle that falls |
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| CN205620554U true CN205620554U (en) | 2016-10-05 |
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| CN201521111617.7U Expired - Fee Related CN205620554U (en) | 2015-12-29 | 2015-12-29 | A device for recovering unmanned aerial vehicle that falls |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105487093A (en) * | 2015-12-29 | 2016-04-13 | 湖南云顶智能科技有限公司 | Device and method for searching fallen unmanned plane |
| CN109383831A (en) * | 2018-09-30 | 2019-02-26 | 安徽煜丰农业机械制造有限公司 | A kind of plant protection drone for automatic positioning of falling |
-
2015
- 2015-12-29 CN CN201521111617.7U patent/CN205620554U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105487093A (en) * | 2015-12-29 | 2016-04-13 | 湖南云顶智能科技有限公司 | Device and method for searching fallen unmanned plane |
| CN105487093B (en) * | 2015-12-29 | 2018-04-13 | 湖南云顶智能科技有限公司 | For recovering the device and method for the unmanned plane that falls |
| CN109383831A (en) * | 2018-09-30 | 2019-02-26 | 安徽煜丰农业机械制造有限公司 | A kind of plant protection drone for automatic positioning of falling |
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| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| 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: 20161005 Termination date: 20211229 |