CN105915899B - A kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus - Google Patents
A kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus Download PDFInfo
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- CN105915899B CN105915899B CN201610519358.4A CN201610519358A CN105915899B CN 105915899 B CN105915899 B CN 105915899B CN 201610519358 A CN201610519358 A CN 201610519358A CN 105915899 B CN105915899 B CN 105915899B
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- head
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- motor
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N17/00—Diagnosis, testing or measuring for television systems or their details
-
- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B43/00—Testing correct operation of photographic apparatus or parts thereof
Abstract
The invention discloses a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus, it is related to head detection technique field, including platform, three parts of debugging system and power supply module, the functions such as present invention set " test ", " debugging " and " demonstration " are integrated, the posture and other data of tested head can be gathered comprehensively, be easy to staff to carry out overall merit and debugging to it.
Description
Technical field
The present invention relates to head detection technique field, and in particular to a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus.
Background technology
Current clouds terrace system measures collection data using all kinds of instrument and meters of separation mostly in test surfaces, without pin
The scheme and case study on implementation of digitization are integrally carried out to load.It is inconvenient for use in terms of thereby resulting in clouds terrace system test of today,
There is no remote collection control function, measurement data is not inaccurate comprehensive, it is difficult to bring substantial data reference for test job.
Chinese Application No. CN 201410650930.1 discloses a kind of camera pan-tilt posture testing system, including master
Tank module, camera pan-tilt system module, sensor assembly and work station are controlled, sensor assembly is arranged on camera pan-tilt system
In module, master control tank module is connected with sensor assembly, controls sensor assembly acquisition camera head attitude information, Main Control Tank
Module is connected with work station, the synchronizing signal that parsing work station is sent, to workstation synchronization transmission objectives head attitude information.Should
Invention is integrated come the attitude information of test mechanical arm type head using Multi-orientation multi-angle sensor.But it can be seen that on
State and invent and unresolved existing unmanned aerial vehicle onboard head, multi-faceted, many data collection tasks of photoelectric nacelle, the data of collection compared with
It is few, it is difficult to comprehensive detection and the function of evaluation head.
Chinese Application No. CN 201320411226.1 also discloses a kind of spherical pan head shooting apparatus test device, including
Hold-down support, spherical pan head and the fish eye camera in spherical pan head, including a support component, the one of the support component
End is connected with hold-down support, and the other end of the support component is connected with spherical pan head.This test device by by rotating stand with
The cantilever end hinged connection of support, the rotating stand is connected with spherical pan head video camera, by adjust the angle of rotating stand from
And realize the axis of adjustment fish eye camera and the angle of test card；And effectively entered the angle of rotating stand by caging bolt
Row limitation, by the way of dual fixation, prevents from producing the phenomenon of landing due to the gravity of spherical pan head video camera.But should
Device is planted also without remote collection control function, measurement data is not inaccurate comprehensive.
The content of the invention
It is an object of the invention to provide a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus, to solve to lead in the prior art
The above-mentioned multinomial defect caused.
A kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus, including
Platform：Including desktop, table leg and motor, the motor includes the X-axis motor and y-axis motor on desktop, X-axis
The axle center of motor and y-axis motor is mutually perpendicular to, and the table leg is installed on four corners of desktop, and the center of the desktop is set
Have and X platforms and Y stage are provided with the opening for installing tested head, the opening, X platforms, which are provided with, to be used to accommodate Y stage
Through hole, X platforms are connected with the side of opening by axis of rotation in the X direction, the side of Y stage in the Y direction with through hole
Connected by axis of rotation, X-axis motor and y-axis motor are connected with the rotating shaft axle positioned at X platforms and Y stage side respectively；
Debugging system：Including main control module, motor, voltage and current detection circuit, wireless image passback module, wireless data
Transceiver module, motor is connected by motor-drive circuit with main control module, main control module respectively with voltage and current detection circuit, nothing
Line image returns module and wireless data transceiver module connection, and voltage and current detection circuit also passes through communication/power supply interface and quilt
Survey head connection；
Power supply module：Including power supply circuit, the power supply circuit is electrically connected with tested head and debugging system respectively.
It is preferred that, video-frequency monitor is additionally provided with the desktop, video-frequency monitor is by being tested the remote control carried in head
Receive and figure passes transmitter module and tested head wireless connection.
It is preferred that, the main control module returns module by wireless image and wireless data transceiver module wireless connection is useful
In the host computer of analyze data.
It is preferred that, the main control module is specially main control MCU chip.
It is preferred that, wireless image passback module and wireless data transceiver module be respectively adopted 5.8G figures pass chip and
2.4G wireless chip.
It is preferred that, the motor is brshless DC motor.
The advantage of the invention is that：
(1) function such as set " test ", " debugging " and " demonstration "；
(2) simple in construction, tested head is connected by quick-disassembly structure with platform, dismounting and simple operation；
(3) this plateform system can reflect the response speed of tested head, control accuracy, damping effect grade, electricity in real time
The data such as stream and power consumption, comprehensively, accurately, for overall merit being tested head provides a good platform for data acquisition；
(4) this plateform system can also be used to the centre of gravity adjustment of load camera, the algorithm verification of head exploitation and simulate fly
Influence of the row device posture to task device, comprehensive gathered data, to support the soft hardware performance of head to develop；
(5) manner of execution of motor can be adjusted according to mission requirements；
(6) data acquisition of this plateform system and the control of relevant device can be optional by wired and wireless two ways
Selecting property is good；
(7) setting of video-frequency monitor can intuitively find out the view effect of load camera.
Brief description of the drawings
Fig. 1 is a kind of structural representation of unmanned aerial vehicle onboard multiaxis head debugging apparatus of the present invention.
Fig. 2 is a kind of theory diagram of unmanned aerial vehicle onboard multiaxis head debugging apparatus of the present invention.
Fig. 3 be in a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus of the present invention power supply module and debugging system and
The connection diagram of tested head.
Wherein：1-desktop, 2-table leg, 3-opening, 4-step, 5-quick-disassembly structure, 6-connecting pole, 7-it is tested cloud
Platform, 8-communication/power supply interface, 9-remote control reception and figure pass transmitter module, 10-main control module, 11-motor, 111-X-axis
Motor, 112-y-axis motor, 12-voltage and current detection circuit, 13-wireless image passback module, 14-wireless data transceiving
Module, 15-motor-drive circuit, 16-power supply circuit, 17-video-frequency monitor, 18-host computer, 19-cable data connects
Mouthful, 20-X platforms, 21-Y stage, 22-through hole.
Embodiment
To be easy to understand the technical means, the inventive features, the objects and the advantages of the present invention, with reference to
Embodiment, is expanded on further the present invention.
As shown in Figure 1, Figure 2 and Figure 3, a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus, including
Platform：Including desktop 1, table leg 2 and motor 11, the motor 11 includes the X-axis motor 111 and Y on desktop
The axle center of spindle motor 112, X-axis motor 111 and y-axis motor 112 is mutually perpendicular to, and the table leg 2 is installed on four turnings of desktop 1
Place, the center of the desktop 1 is provided with the opening 3 for being used for installing tested head, the opening 3 and is provided with X platforms 20 and Y stage
21, X platforms 20 are provided with the through hole 22 for being used for accommodating Y stage 21, and side of the X platforms 20 in the X direction with opening 3 passes through rotating shaft
Connection is rotated, side of the Y stage 21 in the Y direction with through hole 22 is connected by axis of rotation, X-axis motor 111 and y-axis motor
112 are connected with the rotating shaft axle positioned at X platforms 20 and the side of Y stage 21 respectively；
Debugging system：Debugging system is arranged on platform, including main control module 10, motor 11, voltage and current detection circuit
12nd, wireless image passback module 13, wireless data transceiver module 14, motor 11 pass through motor-drive circuit 15 and main control module 10
Connection, main control module 10 returns module 13 and wireless data transceiver module with voltage and current detection circuit 12, wireless image respectively
14 connections, voltage and current detection circuit 12 is also connected with tested head 7 by communication/power supply interface 8, wherein also set up on desktop
There is wired data interface 19, as needed can be attached it to related component or circuit；
Power supply module：Including power supply circuit 16, the power supply circuit 16 is electrically connected with tested head 7 and debugging system respectively
Connect.
In the present embodiment, the motor 11 includes the X-axis motor 111 and y-axis motor 112 on step, X-axis motor
111 are located at the left side of step, and y-axis motor 112 is located at the front side of step.
In the present embodiment, video-frequency monitor 17 is additionally provided with the desktop 1, video-frequency monitor 17 is by being tested head 7
The remote control reception and figure inside carried passes transmitter module 9 and the tested wireless connection of head 7.
In the present embodiment, the main control module 10 returns module 13 and wireless data transceiver module 14 by wireless image
It is wirelessly connected with the host computer 18 for analyze data.
In the present embodiment, the main control module 10 is specially main control MCU chip.
In the present embodiment, 5.8G figures are respectively adopted in the wireless image passback module 13 and wireless data transceiver module 14
Pass chip and 2.4G wireless chips.
In addition, the motor 11 is brshless DC motor 11.
Tested head 7 is tested in the present invention, wherein, it is tested the top of head 7 and passes through quick-disassembly structure 5 and X-axis electricity
Machine 111 and y-axis motor 112 are connected, and tested head 7 is connected by the connecting pole 6 located at the bottom of quick-disassembly structure 5 with quick-disassembly structure 5,
The top of quick-disassembly structure 5 is connected provided with communication/power supply interface 8 and with the control module in tested head 7, is tested in head 7 certainly
Band remote control reception and figure pass transmitter module 9, are tested head 7 provided with load camera and pass transmitter module 9 with remote control reception and figure
And communication/power supply interface 8 is connected；
The operating procedure of the present invention is as follows：
(1) tested head 7 is loaded on platform by quick-disassembly structure 5；
(2) load camera is installed on tested head 7, and connects signal wire；
(3) signal wire and supply lines of tested head 7 are connected, starts power supply module；
(4) the attitude data A that tested head 7 is returned from belt sensor is checked；
(5) control device transverse direction/longitudinal motor 11 produces shake, can now obtain the sensor positioned at device center IMU
Attitude data B, upper computer software two groups of attitude datas of automatic real-time matching calculate the sensitivity of tested head 7, reflection indirectly
The tracking accuracy of head, from steady effect；
(6) entirety of the measurable tested head 7 of voltage and current detection circuit 12 when dynamic is with static state in debugging system
Electric current and power consumption；
(7) user can also change " shake " mode (shock conditions in simulated flight device flight course) of motor 11,
The video that load camera is shot can be seen on a video monitor, and video, root also can be remotely seen by radio receiver
The deficiency and problem of head 7 are tested according to video effect inspection.
Based on above-mentioned, advantages of the present invention includes：(1) function such as set " test ", " debugging " and " demonstration "；(2) structure
Simply, it is tested head to be connected with platform by quick-disassembly structure, dismounting and simple operation；(3) this plateform system can reflect in real time
The data such as response speed, control accuracy, damping effect grade, electric current and the power consumption of tested head, data acquisition is comprehensive, accurate,
Head, which is tested, for overall merit provides a good platform；(4) this plateform system can be additionally used in the center of gravity tune of load camera
The influence of whole, head exploitation algorithm verification and simulated flight device posture to task device, comprehensive gathered data, to support cloud
The soft hardware performance exploitation of platform；(5) manner of execution of motor can be adjusted according to mission requirements；(6) number of this plateform system
Can be alternative good by wired and wireless two ways according to collection and the control of relevant device；(7) setting of video-frequency monitor
The view effect of load camera can intuitively be found out.
As known by the technical knowledge, the present invention can be by the embodiment party of other essence or essential feature without departing from its spirit
Case is realized.Therefore, embodiment disclosed above, for each side, is all merely illustrative, and is not only.Institute
Have within the scope of the present invention or be included in the invention in the change being equal in the scope of the present invention.
Claims (6)
1. a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus, it is characterised in that including
Platform：Including desktop, table leg and motor, the motor includes the X-axis motor and y-axis motor on desktop, X-axis motor
It is mutually perpendicular to the axle center of y-axis motor, the table leg is installed on four corners of desktop, and the center of the desktop is provided with use
In being provided with X platforms and Y stage in the opening for installing tested head, the opening, X platforms, which are provided with, to be used to accommodate the logical of Y stage
Hole, X platforms are connected with the side of opening by axis of rotation in the X direction, and Y stage passes through with the side of through hole in the Y direction
Axis of rotation is connected, and X-axis motor and y-axis motor are connected with the rotating shaft axle positioned at X platforms and Y stage side respectively；
Debugging system：Including main control module, voltage and current detection circuit, wireless image passback module, wireless data transceiver module,
Motor is connected by motor-drive circuit with main control module, and main control module is returned with voltage and current detection circuit, wireless image respectively
Transmission module and wireless data transceiver module connection, voltage and current detection circuit are also connected by communication/power supply interface and tested head
Connect；
Power supply module：Including power supply circuit, the power supply circuit is electrically connected with tested head and debugging system respectively.
2. a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus according to claim 1, it is characterised in that：On the desktop
Video-frequency monitor is additionally provided with, the remote control reception and figure that video-frequency monitor is carried by being tested in head pass transmitter module and tested cloud
Platform wireless connection.
3. a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus according to claim 2, it is characterised in that：The master control mould
Block is wirelessly connected with the host computer for analyze data by wireless image passback module and wireless data transceiver module.
4. a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus according to claim 1, it is characterised in that：The master control mould
Block is specially main control MCU chip.
5. a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus according to claim 1, it is characterised in that：It is described without line chart
Chip and 2.4G wireless chips are passed as 5.8G figures are respectively adopted in passback module and wireless data transceiver module.
6. a kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus according to claim 1, it is characterised in that：The motor is
Brshless DC motor.
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| CN201610519358.4A CN105915899B (en) | 2016-07-04 | 2016-07-04 | A kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus |
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| CN201610519358.4A CN105915899B (en) | 2016-07-04 | 2016-07-04 | A kind of unmanned aerial vehicle onboard multiaxis head debugging apparatus |
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| CN105915899B true CN105915899B (en) | 2017-09-12 |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN106494640B (en) * | 2016-11-22 | 2018-11-20 | 珠海市双捷科技有限公司 | A kind of multi-rotor unmanned aerial vehicle test and trained unified platform |
| CN106644487B (en) * | 2016-12-26 | 2019-04-02 | 广东容祺智能科技有限公司 | A kind of dynamic test system of unmanned plane brushless motor |
| CN107036795B (en) * | 2017-04-27 | 2023-08-25 | 上海交通大学 | Multifunctional debugging platform |
| CN109313439A (en) * | 2017-07-28 | 2019-02-05 | 深圳市大疆创新科技有限公司 | Holder method for testing reliability and device |
| CN111566577A (en) * | 2018-11-29 | 2020-08-21 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle instruction processing method, terminal equipment and unmanned aerial vehicle center board |
| CN113365919A (en) * | 2020-06-23 | 2021-09-07 | 深圳市大疆创新科技有限公司 | Test equipment, test method and flight test system |
| CN113795798A (en) * | 2020-07-20 | 2021-12-14 | 深圳市大疆创新科技有限公司 | Holder, holder performance evaluation method and device and movable platform |
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| CN101420593A (en) * | 2007-10-26 | 2009-04-29 | 罗军 | Image comparison method detects the method for operating state of cloud platform video camera |
| CN103776369B (en) * | 2012-10-23 | 2016-08-31 | 国家电网公司 | Test monitor system and method |
| US9317147B2 (en) * | 2012-10-24 | 2016-04-19 | Microsoft Technology Licensing, Llc. | Input testing tool |
| CN104144340A (en) * | 2014-07-14 | 2014-11-12 | 重庆卓美华视光电有限公司 | 3D effect testing system and method |
| CN104394316B (en) * | 2014-11-16 | 2018-05-01 | 南京理工大学 | Camera pan-tilt posture testing system |
| CN104601986B (en) * | 2015-01-15 | 2017-01-25 | 江苏凯尔生物识别科技有限公司 | Double station semi-automatic focusing test device and test method thereof |
| CN204707214U (en) * | 2015-06-18 | 2015-10-14 | 佳立数码(深圳)有限公司 | A kind of camera testing device |
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Effective date of registration: 20221214 Address after: 323000 Block A, Building 1, No. 268, Shiniu Road, Nanmingshan Street, Liandu District, Lishui City, Zhejiang Province (Lishui Yonglian Intelligent Manufacturing Industrial Park) Patentee after: Zhejiang Rongqi Intelligent Equipment Co.,Ltd. Address before: 518109 South Floor 2, Building 9, Dongwu Industrial Park, Donghuan 1st Road, Longhua New District, Shenzhen, Guangdong Patentee before: GUANGDONG RONGQE INTELLIGENT TECHNOLOGY Co.,Ltd. |
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