CN209814320U - Take-off and landing platform suitable for mooring unmanned aerial vehicle - Google Patents
Take-off and landing platform suitable for mooring unmanned aerial vehicle Download PDFInfo
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- CN209814320U CN209814320U CN201920405631.XU CN201920405631U CN209814320U CN 209814320 U CN209814320 U CN 209814320U CN 201920405631 U CN201920405631 U CN 201920405631U CN 209814320 U CN209814320 U CN 209814320U
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Abstract
The utility model discloses a take-off and landing platform suitable for mooring an unmanned aerial vehicle, which comprises a vehicle-mounted fixed platform, a middle adjusting platform and an unmanned aerial vehicle take-off and landing platform, wherein the middle adjusting platform is positioned above the vehicle-mounted fixed platform, and a first rotary adjusting piece is arranged between the middle adjusting platform and the vehicle-mounted fixed platform, the first rotary adjusting piece drives the middle adjusting platform to rotate in a vertical plane, the unmanned aerial vehicle take-off and landing platform is positioned above the middle adjusting platform, and install the second rotation regulation piece between unmanned aerial vehicle platform and the middle regulation platform, the second rotation regulation piece drives unmanned aerial vehicle platform at the vertical plane internal rotation that takes off and land, and the rotation plane at middle regulation platform place and the rotation plane mutually perpendicular at unmanned aerial vehicle platform place still include the industrial computer and install the gyroscope on unmanned aerial vehicle platform that takes off and land, industrial computer and gyroscope, first rotation regulation piece and the hookup of second rotation regulation piece signal. The lifting platform has the advantages of simple and reliable structure, capability of keeping horizontal self-stability in real time and capability of realizing safe and nondestructive lifting.
Description
Technical Field
The utility model mainly relates to the unmanned aerial vehicle field especially relates to a take off and land platform suitable for mooring unmanned aerial vehicle.
Background
With the deepening of informatization and networking degrees, the convenience brought by the network can be enjoyed in all aspects of life. At the same time, network dependence becomes a feature of this information society. The popularity of thumb culture makes the communication demand continuously rise, the communication guarantee capability shows a crucial role, and the necessity demand of emergency communication such as field operation, emergency rescue and the like is more prominent. Under the demand situation, the tethered rotor unmanned aerial vehicle as a high-altitude base station walks into eye curtains of people. Mooring unmanned aerial vehicle system is by many rotor unmanned aerial vehicle, mooring cable, ground take-off and landing platform are constituteed, unmanned aerial vehicle uses the long-time stagnation of ground power supply to hang and stop, simultaneously, data such as the high definition video of airborne equipment collection can be passed back to ground through the built-in optic fibre of mooring cable, have aerial long-time operation, the big advantage of data transmission bandwidth, but entire system stand alone type installation also can on-vehicle installation to can the vehicle movement is followed in automatic synchronization. At present, a tethered unmanned aerial vehicle on the market can supply power through a ground generator, 24-hour all-weather stagnation can be realized, the tethered unmanned aerial vehicle works continuously for 72 hours, and hovers at a fixed point of 200 meters, so that the tethered unmanned aerial vehicle is widely applied to a plurality of wide fields of disaster relief and rescue, border patrol, base safety, scenic spot monitoring, geological survey, field operation, forest fire prevention, emergency communication, public security anti-terrorism, traffic supervision, news interview, engineering monitoring, environment monitoring, movie and television shooting, scientific research, national defense war industry and the like.
The existing unmanned aerial vehicle technology has high requirement on the levelness of the take-off of the unmanned aerial vehicle, and the levelness is generally not more than 10 degrees; the unmanned aerial vehicle also has requirements on a landing surface when landing, and the landing surface which is rugged and inclined can influence the landing of the unmanned aerial vehicle and even cause damage; various road conditions can be met when the vehicle runs by the vehicle-mounted mooring unmanned aerial vehicle, and a stable horizontal take-off and landing platform solution is urgently needed.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to overcome prior art not enough, provide a simple structure reliable, can keep the level self-stabilization in real time, can realize safe harmless take off and land platform that is applicable to mooring unmanned aerial vehicle.
In order to solve the technical problem, the utility model discloses a following technical scheme:
a take-off and landing platform suitable for mooring an unmanned aerial vehicle, which comprises a vehicle-mounted fixed platform, a middle adjusting platform and an unmanned aerial vehicle take-off and landing platform, the middle adjusting platform is positioned above the vehicle-mounted fixed platform, a first rotary adjusting piece is arranged between the middle adjusting platform and the vehicle-mounted fixed platform, the first rotary adjusting piece drives the middle adjusting platform to rotate in a vertical plane, the unmanned aerial vehicle taking-off and landing platform is positioned above the middle adjusting platform, and a second rotary adjusting piece is arranged between the unmanned aerial vehicle taking-off and landing platform and the middle adjusting platform, the second rotary adjusting part drives the unmanned aerial vehicle take-off and landing platform to rotate in a vertical plane, a rotating plane where the middle adjusting platform is located is perpendicular to a rotating plane where the unmanned aerial vehicle take-off and landing platform is located, the second rotary adjusting part further comprises an industrial personal computer and a gyroscope installed on the unmanned aerial vehicle take-off and landing platform, and the industrial personal computer is in signal connection with the gyroscope, the first rotary adjusting piece and the second rotary adjusting piece.
As a further improvement of the above technical solution:
the first rotary adjusting piece comprises a first motor, a first mounting table and a first rotating table, the first motor is mounted on the vehicle-mounted fixing table through the first mounting table, the first rotating table is connected with the output end of the first motor, the middle adjusting table is fixedly mounted on the first rotating table, and the first motor is in signal connection with the industrial personal computer.
The first rotating platform is a semi-circular platform, and the middle adjusting platform is fixedly arranged on the flat surface of the semi-circular platform.
The second rotary adjusting part comprises a second motor, a second mounting table and a second rotating table, the second motor is mounted on the middle adjusting table through the second mounting table, the second rotating table is connected with the output end of the second motor, the unmanned aerial vehicle taking-off and landing table is fixedly mounted on the second rotating table, and the second motor is in signal connection with the industrial personal computer.
The second revolving stage sets up to half round platform, unmanned aerial vehicle take off and land the platform and adorn admittedly on the straight face of half round platform.
The first rotating adjusting piece and the second rotating adjusting piece correspondingly start rotating adjustment according to levelness in different directions measured by the gyroscope.
Compared with the prior art, the utility model has the advantages of:
the utility model discloses a platform of taking off and land suitable for mooring unmanned aerial vehicle, including on-vehicle fixed station, middle regulation platform and unmanned aerial vehicle platform of taking off and land, middle regulation platform is located on-vehicle fixed station top, and install first rotation regulation piece between middle regulation platform and the on-vehicle fixed station, regulation platform is at vertical plane internal rotation in the middle of first rotation regulation piece drives, unmanned aerial vehicle takes off and land the platform and is located middle regulation platform top, and install the second rotation regulation piece between unmanned aerial vehicle platform of taking off and land and the middle regulation platform, the second rotation regulation piece drives unmanned aerial vehicle platform of taking off and land at vertical plane internal rotation, the rotation plane at middle regulation platform place and the rotation plane mutually perpendicular at unmanned aerial vehicle platform of taking off and land place, still include the industrial computer and install the gyroscope on unmanned aerial vehicle platform of taking off and land, industrial computer and gyroscope, first rotation regulation piece and the rotatory regulation piece signal coupling of. In the structure, the middle adjusting platform is arranged on the vehicle-mounted fixed platform through a first rotary adjusting piece, the rotary action of the first rotary adjusting piece controls the angle of the middle adjusting platform in the X-axis direction, the unmanned aerial vehicle landing platform is arranged on the middle adjusting platform through a second rotary adjusting piece, the rotary action of the second rotary adjusting piece controls the angle of the unmanned aerial vehicle landing platform in the Y-axis direction, the horizontal plane degree of the unmanned aerial vehicle landing platform is measured by a gyroscope, the horizontal plane degree signal is fed back to the industrial personal computer for data processing, the industrial personal computer outputs signals through the processing result to control the rotation angle output of the first rotation adjusting piece and the second rotation adjusting piece, therefore, the angle between the take-off and landing platform of the unmanned aerial vehicle and the horizontal plane is adjusted, a new horizontal plane degree is obtained through the gyroscope measurement, the new horizontal plane degree is continuously fed back to the industrial personal computer, and the steps are repeated in such a circulating mode until the horizontal degree between the take-off and landing platform of the unmanned aerial vehicle and the horizontal plane is 0. Thereby make on-vehicle unmanned aerial vehicle that moors unmanned aerial vehicle take off and land platform be in the horizontality all the time. The whole structure of the take-off and landing platform is simple and reliable, so that the level of the take-off and landing platform of the unmanned aerial vehicle is self-stabilized, and the unmanned aerial vehicle can normally take off and land safely and nondestructively.
Drawings
Fig. 1 is the utility model is suitable for a main structure schematic diagram of looking at of unmanned aerial vehicle's take off and land platform is moored.
Fig. 2 is a side view schematic diagram (the industrial control machine is not shown in the figure) of the take-off and landing platform for mooring unmanned aerial vehicle.
Fig. 3 is a perspective view (not shown in the figure) of a landing platform for mooring an unmanned aerial vehicle.
The reference numerals in the figures denote:
1. a vehicle-mounted fixed table; 2. a middle adjusting table; 3. an unmanned aerial vehicle landing platform; 4. a first rotary adjustment member; 41. a first motor; 42. a first mounting table; 43. a first rotating table; 5. a second rotation adjustment member; 51. a second motor; 52. a second mounting table; 53. a second rotating table; 6. an industrial personal computer; 7. a gyroscope.
Detailed Description
The invention will be described in further detail with reference to the drawings and specific examples.
As shown in fig. 1 to 3, an embodiment of the landing platform for mooring an unmanned aerial vehicle of the present invention comprises a vehicle-mounted fixing platform 1, an intermediate adjusting platform 2 and an unmanned aerial vehicle landing platform 3, wherein the intermediate adjusting platform 2 is located above the vehicle-mounted fixing platform 1, and a first rotary adjusting member 4 is installed between the intermediate adjusting platform 2 and the vehicle-mounted fixing platform 1, the first rotary adjusting member 4 drives the intermediate adjusting platform 2 to rotate in a vertical plane, the unmanned aerial vehicle landing platform 3 is located above the intermediate adjusting platform 2, and a second rotary adjusting member 5 is installed between the unmanned aerial vehicle landing platform 3 and the intermediate adjusting platform 2, the second rotary adjusting member 5 drives the unmanned aerial vehicle landing platform 3 to rotate in the vertical plane, the rotary plane of the intermediate adjusting platform 2 is perpendicular to the rotary plane of the unmanned aerial vehicle landing platform 3, and further comprises an industrial personal computer 6 and a gyroscope 7 installed on the unmanned aerial vehicle landing platform 3, the industrial personal computer 6 is in signal connection with the gyroscope 7, the first rotation adjusting part 4 and the second rotation adjusting part 5. In the structure, an intermediate adjusting platform 2 is installed on a vehicle-mounted fixed platform 1 through a first rotary adjusting piece 4, the rotary action of the first rotary adjusting piece 4 controls the angle of the intermediate adjusting platform 2 in the X-axis direction, an unmanned aerial vehicle take-off and landing platform 3 is installed on the intermediate adjusting platform 2 through a second rotary adjusting piece 5, the rotary action of the second rotary adjusting piece 5 controls the angle of the unmanned aerial vehicle take-off and landing platform 3 in the Y-axis direction, the horizontal plane degree of the unmanned aerial vehicle take-off and landing platform 3 is measured by a gyroscope 7, a horizontal plane degree signal is fed back to an industrial personal computer 6 for data processing, the industrial personal computer 6 outputs a signal through a processing result to control the rotation angle output of the first rotary adjusting piece 4 and the second rotary adjusting piece 5, so as to adjust the angle between the unmanned aerial vehicle take-off and landing platform 3 and the horizontal plane, a new horizontal plane degree is measured by the gyroscope 7 and is fed, until the levelness of the unmanned aerial vehicle lifting platform 3 and the horizontal plane is 0. Thereby make on-vehicle unmanned aerial vehicle that moors platform 3 all the time be in the horizontality. This platform of taking off and landing's overall structure is simple reliable to realize that unmanned aerial vehicle takes off and land platform 3's level is from steady, let unmanned aerial vehicle can normally take off, land safely and harmlessly.
In this embodiment, the first rotation adjusting member 4 includes a first motor 41, a first mounting table 42 and a first rotating table 43, the first motor 41 is mounted on the vehicle-mounted fixing table 1 through the first mounting table 42, the first rotating table 43 is connected with an output end of the first motor 41, the intermediate adjusting table 2 is fixedly mounted on the first rotating table 43, and the first motor 41 is in signal connection with the industrial personal computer 6. In this structure, first motor 41 is installed on-vehicle fixed station 1 through first mount table 42, and first revolving stage 43 is connected with first motor 41's output, and first motor 41 starts in order to drive first revolving stage 43 rotatory when obtaining industrial computer 6's angle output signal to the angle leveling of regulation platform 2 in the X axle direction in the middle of realizing, the angle leveling of unmanned aerial vehicle platform 3 in the X axle direction has indirectly been realized.
In this embodiment, the first rotating table 43 is a half-round table, and the intermediate adjusting table 2 is fixedly mounted on the flat surface of the half-round table. The first rotating platform 43 is a semi-circular platform, on one hand, a straight surface can be formed to horizontally install the middle adjusting platform 2 so as to ensure the initial levelness of installation, and the semi-circular platform can also ensure the center to be wound during rotation, so that the phenomenon of unbalanced rotation can not occur.
In this embodiment, the second rotation adjusting member 5 includes a second motor 51, a second mounting table 52 and a second rotating table 53, the second motor 51 is mounted on the middle adjusting table 2 through the second mounting table 52, the second rotating table 53 is connected to an output end of the second motor 51, the unmanned aerial vehicle taking-off and landing table 3 is fixedly mounted on the second rotating table 53, and the second motor 51 is in signal connection with the industrial personal computer 6. In this structure, second motor 51 is installed on middle regulation platform 2 through second mount table 52, and second revolving stage 53 is connected with second motor 51's output, and second motor 51 starts in order to drive second revolving stage 53 rotatory when obtaining industrial computer 6's angle output signal to unmanned aerial vehicle take off and land platform 3 has been realized at the angle leveling of Y axle direction.
In this embodiment, the second rotating platform 53 is a semi-circular platform, and the unmanned aerial vehicle take-off and landing platform 3 is fixedly arranged on the flat surface of the semi-circular platform. Set up second revolving stage 53 to the semicircular table and can form a straight face on the one hand and supply 3 horizontal installation of unmanned aerial vehicle take-off and landing platform in order to guarantee to install initial levelness, the semicircular table can also guarantee can be rich the center when rotatory, the phenomenon of rotation unbalance can not appear.
In this embodiment, the first rotation adjusting member 4 and the second rotation adjusting member 5 respectively start rotation adjustment according to levelness in different directions measured by the gyroscope 7. In this configuration, the rotation control logic for the first motor 41 and the second motor 51 is as follows:
the gyroscope 7 detects the angle between the X-axis direction of the point where the gyroscope is located and the horizontal plane in real time, the angle is fed back to the industrial personal computer 6 to be compared, the industrial personal computer 6 sends an angle signal to be adjusted to the first motor 41, the first motor 41 is started according to the angle signal to drive the first rotating table 43 to rotate to achieve angle leveling in the X-axis direction, and angle leveling of the unmanned aerial vehicle take-off and landing table 3 in the X-axis direction is indirectly achieved;
the gyroscope 7 detects the angle between the Y-axis direction of the point where the gyroscope is located and the horizontal plane in real time, the angle is fed back to the industrial personal computer 6 to be compared, the industrial personal computer 6 sends an angle signal to be adjusted to the second motor 51, the second motor 51 is started according to the angle signal to drive the second rotating platform 53 to rotate so as to achieve angle leveling in the Y-axis direction, and the angle leveling of the unmanned aerial vehicle taking-off and landing platform 3 in the Y-axis direction is indirectly achieved.
Although the present invention has been described with reference to the preferred embodiments, it is not intended to limit the present invention. The technical solution of the present invention can be used by anyone skilled in the art to make many possible variations and modifications, or to modify equivalent embodiments, without departing from the scope of the technical solution of the present invention, using the technical content disclosed above. Therefore, any simple modification, equivalent change and modification made to the above embodiments by the technical entity of the present invention should fall within the protection scope of the technical solution of the present invention.
Claims (6)
1. The utility model provides a take off and land platform suitable for mooring unmanned aerial vehicle which characterized in that: the unmanned aerial vehicle take-off and landing system comprises a vehicle-mounted fixed platform (1), a middle adjusting platform (2) and an unmanned aerial vehicle take-off and landing platform (3), wherein the middle adjusting platform (2) is positioned above the vehicle-mounted fixed platform (1), a first rotary adjusting piece (4) is arranged between the middle adjusting platform (2) and the vehicle-mounted fixed platform (1), the first rotary adjusting piece (4) drives the middle adjusting platform (2) to rotate in a vertical plane, the unmanned aerial vehicle take-off and landing platform (3) is positioned above the middle adjusting platform (2), a second rotary adjusting piece (5) is arranged between the unmanned aerial vehicle take-off and landing platform (3) and the middle adjusting platform (2), the second rotary adjusting piece (5) drives the unmanned aerial vehicle take-off and landing platform (3) to rotate in the vertical plane, a rotating plane where the middle adjusting platform (2) is positioned is perpendicular to a rotating plane where the unmanned aerial vehicle take-off and landing platform (3) is positioned, and the unmanned aerial vehicle take-off and landing platform (, the industrial personal computer (6) is in signal connection with the gyroscope (7), the first rotary adjusting piece (4) and the second rotary adjusting piece (5).
2. The take-off and landing platform suitable for mooring a drone of claim 1, wherein: first rotation regulation piece (4) include first motor (41), first mount table (42) and first revolving stage (43), install on-vehicle fixed station (1) through first mount table (42) first motor (41), first revolving stage (43) are connected with the output of first motor (41), middle regulation platform (2) are adorned admittedly on first revolving stage (43), first motor (41) and industrial computer (6) signal coupling.
3. The take-off and landing platform suitable for mooring a drone of claim 2, wherein: the first rotating platform (43) is a semi-circular platform, and the middle adjusting platform (2) is fixedly arranged on the straight surface of the semi-circular platform.
4. The take-off and landing platform suitable for mooring a drone of claim 3, wherein: the second rotating adjusting piece (5) comprises a second motor (51), a second mounting table (52) and a second rotating table (53), the second motor (51) is mounted on the middle adjusting table (2) through the second mounting table (52), the second rotating table (53) is connected with the output end of the second motor (51), the unmanned aerial vehicle lifting table (3) is fixedly mounted on the second rotating table (53), and the second motor (51) is in signal connection with the industrial personal computer (6).
5. The take-off and landing platform suitable for mooring a drone of claim 4, wherein: the second rotating platform (53) is a semi-circular platform, and the unmanned aerial vehicle take-off and landing platform (3) is fixedly arranged on the straight surface of the semi-circular platform.
6. The take-off and landing platform for tethered drones of any of claims 1 to 5, wherein: the first rotary adjusting piece (4) and the second rotary adjusting piece (5) correspondingly start rotary adjustment according to levelness in different directions measured by the gyroscope (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920405631.XU CN209814320U (en) | 2019-03-27 | 2019-03-27 | Take-off and landing platform suitable for mooring unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920405631.XU CN209814320U (en) | 2019-03-27 | 2019-03-27 | Take-off and landing platform suitable for mooring unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN209814320U true CN209814320U (en) | 2019-12-20 |
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| CN201920405631.XU Expired - Fee Related CN209814320U (en) | 2019-03-27 | 2019-03-27 | Take-off and landing platform suitable for mooring unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023206864A1 (en) * | 2022-04-24 | 2023-11-02 | 天津航天中为数据系统科技有限公司 | Dynamic take-off and landing device and method for unmanned aerial vehicle |
-
2019
- 2019-03-27 CN CN201920405631.XU patent/CN209814320U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023206864A1 (en) * | 2022-04-24 | 2023-11-02 | 天津航天中为数据系统科技有限公司 | Dynamic take-off and landing device and method for unmanned aerial vehicle |
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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: 20191220 |