CN206734657U - The on-board component equipment and system of a kind of dynamic flying performance test - Google Patents
The on-board component equipment and system of a kind of dynamic flying performance test Download PDFInfo
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- CN206734657U CN206734657U CN201720242078.3U CN201720242078U CN206734657U CN 206734657 U CN206734657 U CN 206734657U CN 201720242078 U CN201720242078 U CN 201720242078U CN 206734657 U CN206734657 U CN 206734657U
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Abstract
The utility model discloses a kind of on-board component equipment of dynamic flying performance test and system, the on-board component equipment includes：Sensing module, decoder module, memory module and respectively sensing module and decoder module provide the power supply module of power supply.On-board component hanging equipment provided by the utility model is loaded onto unmanned plane, carry out real winged test with unmanned plane, in test process, on-board component electrical system is totally independent of tested unmanned electrical-mechanical system, carried out by power itself module and powered, collection includes three axial acceleration to each sensor in sensor assembly in real time, the relevant parameters such as longitude and latitude height, decoded module resolving processing, each parameter is converted into digital quantity form to store to memory module, after unmanned plane completes mission program landing according to flight path, download offline or download online by way of carry out data readback, retaking of a year or grade is played back to ground data and processing equipment, carry out Data Management Analysis, according to the standardization criterion of test reference, provide performance test conclusion.
Description
Technical field
Technical field of performance test is the utility model is related to, is to be related to a kind of dynamic flying performance test in particular
On-board component equipment and system.
Background technology
With the continuous progress of unmanned air vehicle technique, its performance is become better and better, and the function of realization becomes increasingly abundant.For unmanned plane
Security, the reliability of each airborne equipment of system increasingly cause the concern of people, and with the listing of a large amount of civilian unmanned planes, prison
Pipe missing directly embodies.Because present unmanned plane testing standard is not yet unified, test parameter and performance judge index also due to
The actual use scene of unmanned plane is different and has differences, e.g., traffic administration, power-line patrolling, geologic prospect etc., it is therefore desirable to
Third-party testing regulator is established, it is more and more important and anxious to build a set of comprehensive unmanned aerial vehicle comprehensive test platform
Compel.
Utility model content
In view of this, the utility model provides the on-board component equipment and system of a kind of dynamic flying performance test, leads to
Cross and fly the system using actual hang, third-party testing can be carried out, and can obtain independently of corresponding outside unmanned plane
Measured parameter.
To achieve the above object, the utility model provides following technical scheme：
A kind of on-board component equipment of dynamic flying performance test, including：
Gather data message of the unmanned plane in flight course in real time by sensor, and by the data message packing
Reason, the sensing module as the input data of dynamic flying performance test；
It is connected with the sensing module, the decoding mould that the supplemental characteristic of the sensing module is acquired and decoded
Block；
It is connected with the decoder module, the storage stored to the supplemental characteristic decoded in the decoder module
Module；
It is connected respectively with the sensing module and the decoder module, is provided for the sensing module and the decoder module
The power supply module of power supply.
Preferably, in addition to：Structure housing, the structure housing is integrated and Streamline Design.
Wherein, the sensing module is the sensor group based on micro-electromechanical system (MEMS) integrated navigation system.
Wherein, the sensor group includes：MEMS gyro, accelerometer, the Big Dipper/GPS, navigational computer.
Wherein, the memory module is the internal storage or External memory equipment of the on-board component equipment.
Wherein, the power supply module is standard lithium battery group, and its voltage output standard is set according to the on-board component
Standby internal circuit demand setting.
A kind of dynamic flying Performance Test System, including：On-board component equipment described above, in addition to：
It is connected with the on-board component equipment, carries out the host computer of data readback.
Wherein, the host computer is PC, desktop computer or tablet personal computer.
Wherein, the host computer is portable reinforcing data readback equipment.
Wherein, the host computer is the playback of high-performance test data and processing equipment.
Understand that compared with prior art, the utility model discloses a kind of dynamic flying via above-mentioned technical scheme
The on-board component equipment and system that can be tested, the on-board component equipment include：Unmanned plane is gathered in real time by sensor to fly
During data message, and data message packing is handled, the sensing mould as the input data of dynamic flying performance test
Block；It is connected with sensing module, the decoder module that the supplemental characteristic of sensing module is acquired and decoded；With decoder module phase
Connection, the memory module stored to the supplemental characteristic decoded in decoder module；Respectively with sensing module and decoder module phase
Even, the power supply module of power supply is provided for sensing module and decoder module.The utility model provides on-board component hanging equipment and is loaded onto nothing
It is man-machine, carry out with unmanned plane and fly test in fact, in test process, on-board component electrical system is totally independent of tested unmanned electrical-mechanical
System, carried out by power itself module and powered, the collection in real time of each sensor in sensor assembly includes three axial acceleration, warp
The relevant parameters such as latitude height, decoded module resolving processing, are converted into digital quantity form by each parameter and store to memory module, nobody
Machine according to flight path complete mission program landing after, download offline or download online by way of carry out data readback, return
Read to ground data playback and processing equipment, carry out Data Management Analysis, according to the standardization criterion of test reference, provide performance
Test result.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only
It is embodiment of the present utility model, for those of ordinary skill in the art, on the premise of not paying creative work, also
Other accompanying drawings can be obtained according to the accompanying drawing of offer.
Fig. 1 is a kind of on-board component device structure signal for dynamic flying performance test that the utility model embodiment provides
Figure；
Fig. 2 is the structural representation for the sensing module 101 that the utility model embodiment provides；
Fig. 3 is the structural representation for the decoder module 102 that the utility model embodiment provides；
Fig. 4 is a kind of tool of the on-board component device structure for dynamic flying performance test that the utility model embodiment provides
Body schematic diagram；
Fig. 5 is a kind of dynamic flying Performance Test System structural representation that the utility model embodiment provides.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Accompanying drawing 1 is referred to, Fig. 1 is a kind of on-board component for dynamic flying performance test that the utility model embodiment provides
Device structure schematic diagram.As shown in figure 1, the utility model discloses a kind of on-board component equipment of dynamic flying performance test,
The on-board component equipment specifically includes as follows：
On-board component equipment is realized during unmanned plane during flying, to quilts such as unmanned plane during flying height, speed, posture, GPS
Test detection is acquired, stored.After unmanned plane during flying terminates, using ground data playback with processing equipment by flying quality
Online unloading and offline unloading are carried out, then to tested detection data review andanalysis.On-board component is divided by function, and can have
Body is divided into sensing module 101, decoder module 102, memory module 103 and power supply module 104, and structure housing 105.
Sensing module 101 gathers data message of the unmanned plane in flight course by sensor in real time, and data are believed
Cease packing processing, the input data as dynamic flying performance test；Wherein, data message includes：The present speed of unmanned plane,
The current pose information of the current acceleration of unmanned plane, the current location of unmanned plane and unmanned plane.
Specifically, referring to accompanying drawing 2, Fig. 2 is that the concrete structure for the sensing module 101 that the utility model embodiment provides shows
It is intended to.As shown in Fig. 2 core component of the sensing module 101 as test system, it gathers unmanned plane in real time by each sensor
Speed, acceleration in flight course, position, attitude information, and data packing is handled, as dynamic flying performance test
Input data, be unmanned plane test system and test dependable performance whether important technology ensure, wherein, sensor be based on micro-
The sensor group of Mechatronic Systems MEMS integrated navigation systems, the sensor group mainly include：MEMS gyro, three axial acceleration
The high-performance integrated navigation system of the composition such as meter, the Big Dipper/GPS, navigational computer, based on gyro, accelerometer it is used
Property navigation and the navigation of inertia/combinations of satellites calculate, the information such as the course of carrier, pitching, rolling, speed, position can be measured.Adopt
With high-performance algorithm, possesses moving alignment, inertial navigation/combinations of satellites navigation, inertial navigation/odometer reckoning, autonomous zero-speed are repaiied
Just, the function such as self-calibration.
It is connected with sensing module 101, the decoder module that the supplemental characteristic of sensing module 101 is acquired and decoded
102；
Specifically, parameter acquisition of the solid line of decoder module 102 to sensing module 101, by acquired data storage to storing mould
In block 103, accompanying drawing 3 is referred to, Fig. 3 is the concrete structure schematic diagram for the deciphering module 102 that the utility model embodiment provides.Such as
Shown in Fig. 3, decoder module 102 includes：Voltage conversion unit, central processor MCU and Ethernet chip PHY, such as Fig. 3 institutes
Show, three axial accelerometer is connected with MCU SPI interface, gathers the data message of three axial accelerometer, Ethernet chip
PHY is connected with MCU RMII interfaces, realizes the download online of data, and MCU USB interface can realize data it is offline under
Carry, i.e., offline to download, MCU also includes：UART, I/O interface, FSMC interfaces, I2C interface and UART interface.
It is connected with decoder module 102, the memory module stored to the supplemental characteristic decoded in decoder module 102
103；
Specifically, memory module 103 can be the internal storage or External memory equipment of on-board component equipment.
Memory module 103 is deposited for the tested detections such as flying height, speed, posture, GPS during unmanned plane during flying
Storage media；After unmanned plane during flying terminates, memory module is taken out or directly downloaded in on-board component device interior, passes through ground
The tested detection item data during unmanned plane during flying is read in data readback with processing equipment, can be arranged by playing back software
Table, the form of image show tested detection.
It is connected respectively with sensing module 101 and decoder module 102, electricity is provided for sensing module 101 and decoder module 102
The power supply module 104 in source.
Specifically, power supply module 104 is standard lithium battery group, its voltage output standard is according to on-board component equipment
Internal circuit demand is set.
On-board component equipment power supply module uses the form of standard lithium battery group, and voltage output standard is according in reality
Depending on portion's circuit requirements, versatility requirement is to need to meet the practical flight testing time, such as tested unmanned plane nominal cruising time
For Xh, then power supply module battery capacity, which calculates, requires at least above cruising time Xh。
Power supply module 104 is to supply solution after voltage is carried out into voltage conversion by voltage conversion unit with decoder module 102
Code module 102 realizes work.
Preferably, the on-board component equipment also includes：Structure housing 105, structure housing 105 is integrated and streamline is set
Meter.
Structure housing follows integrated design, in the design process, it is necessary to which to take into account loss of weight, protection, electromagnetic compatibility etc. multinomial
Content, need to consider Streamline Design theory in design, reducing flight of the windage on measurand influences.
The utility model discloses a kind of on-board component equipment of dynamic flying performance test, the on-board component equipment bag
Include：Gather data message of the unmanned plane in flight course in real time by sensor, and data message packing is handled, as dynamic
The sensing module of the input data of state flying quality test；It is connected with sensing module, the supplemental characteristic of sensing module is carried out
The decoder module for gathering and decoding；It is connected with decoder module, is deposited to what the supplemental characteristic decoded in decoder module was stored
Store up module；It is connected respectively with sensing module and decoder module, the power supply module of power supply is provided for sensing module and decoder module.This
Utility model provides on-board component hanging equipment and is loaded onto unmanned plane, carries out with unmanned plane and flies test in fact, in test process, on-board component
Electrical system is totally independent of tested unmanned electrical-mechanical system, is carried out by power itself module and powered, each in sensor assembly
Sensor collection in real time includes the relevant parameters such as three axial acceleration, longitude and latitude height, decoded module resolving processing, each parameter is turned
Digital quantity form is turned to store to memory module, unmanned plane is completed after mission program lands according to flight path, by offline or
Online mode carries out data readback, and retaking of a year or grade to ground data plays back and processing equipment, Data Management Analysis is carried out, according to test
The standardization criterion of reference, provides performance test conclusion.
Specifically, referring to accompanying drawing 4, Fig. 4 is a kind of dynamic flying performance test that the utility model embodiment provides
The concrete structure schematic diagram of on-board component equipment.As shown in figure 4, specifically, the unit component of the dynamic flying performance test is set
The annexation between each module in standby is as illustrated, sensing module 101 is connected with MCU UART or I/O interface, and three axially
Accelerometer is connected by SPI interface, and other interfaces are connected by MCU UART interface, the I2C interface phase that GPS passes through MCU
Even, sensing module 101 can directly be connected with power supply module 104, be powered by power supply module 104 directly to sensing module 101.Solution
Code module 102 is connected by its distinctive voltage conversion unit with power supply module 104, and power supply module 104 passes through voltage cell mould
The voltage class that block converts voltages into decoder module 102 and can used is powered.MCU RMII interface and Ethernet interface
PHY is connected, and realizes the download online of related data, and MCU USB interface is directly inserted into from USB mode, realizes related data
Offline download.Memory module 103 is connected by FSMC interfaces with MCU, realizes the storage of related data.
Accompanying drawing 5 is referred to, Fig. 5 is that a kind of dynamic flying Performance Test System structure that the utility model embodiment provides is shown
It is intended to.As shown in figure 5, the invention also discloses a kind of dynamic flying Performance Test System, including：Above-mentioned on-board component
Equipment 301, in addition to：It is connected with on-board component equipment 301, carries out the host computer 302 of data readback.
Wherein, host computer 302 can be PC, desktop computer or tablet personal computer.
Wherein, host computer 302 can be that portable reinforcing data readback equipment or high-performance test data playback is set with processing
It is standby.
As shown in figure 5, the memory module described in Fig. 5 can be External memory equipment, on-board component equipment carries out carry
Data acquisition, real winged test is carried out with unmanned plane, the data gathered in test process can also be stored to external storage simultaneously to be set
In standby and internal storage, it is stored in External memory equipment and can removes External memory equipment directly after flying to terminate in fact and enter
The offline download of row data；Offline or online network can be passed through after flying over journey in fact or terminating by being stored in internal storage
Carry out the download online of data.
Dynamic performance testing software can be run on upper computer equipment with indiscriminate, and the difference for host computer is exactly
The height of performance, the speed of data processing is influenceed, observe the details of data.
Function：Dynamic performance testing software be exactly test data is parsed, judged, is provided test report processing it is soft
Part；Host computer is exactly the different performance of dynamic performance testing running software, the computer platform of different structure form.
To ensure outfield test flight, portable reinforcing data readback and processing equipment, PC or tablet personal computer are configured；Internal field
The playback of high-performance test data and processing equipment or desktop computer are configured, data download and process performance can be ensured.
On-board component carry is to unmanned plane in the technical program, with unmanned plane carry out it is real fly test, it is airborne in test process
Component electrical system is totally independent of tested unmanned electrical-mechanical system, is powered by power itself module, in sensor assembly
Each sensor collection includes the relevant parameters such as three axial acceleration, longitude and latitude height in real time, decoded module resolving is handled, by each ginseng
Number is converted into digital quantity form and stored to memory module, and unmanned plane is completed after mission program lands according to flight path, by from
The form that line is downloaded carries out data readback, and retaking of a year or grade to host computer carries out Data Management Analysis, is sentenced according to the standardization of test reference
According to providing performance test conclusion.
In summary, should the utility model discloses a kind of on-board component equipment of dynamic flying performance test and system
On-board component equipment includes：Gather data message of the unmanned plane in flight course in real time by sensor, and by data message
Packing is handled, the sensing module as the input data for surveying dynamic flying performance test；It is connected with sensing module, to sensing mould
The decoder module that the supplemental characteristic of block is acquired and decoded；It is connected with decoder module, to the parameter decoded in decoder module
The memory module that data are stored；It is connected respectively with sensing module and decoder module, is provided for sensing module and decoder module
The power supply module of power supply.The utility model provides on-board component hanging equipment and is loaded onto unmanned plane, carries out real winged test with unmanned plane, surveys
During examination, on-board component electrical system is totally independent of tested unmanned electrical-mechanical system, is powered by power itself module,
Collection includes the relevant parameters such as three axial acceleration, longitude and latitude height, decoded module solution to each sensor in sensor assembly in real time
Calculation is handled, and each parameter is converted into digital quantity form stores to memory module, and unmanned plane is according to flight path completion mission program
After landing, data readback is carried out by offline or online mode, retaking of a year or grade to ground data plays back and processing equipment, carries out data
Treatment Analysis, according to the standardization criterion of test reference, provide performance test conclusion.
It should be noted that each embodiment in this specification is described by the way of progressive, each embodiment weight
Point explanation is all difference with other embodiment, between each embodiment identical similar part mutually referring to.
The method proposed above in association with accompanying drawing to the utility model is exemplarily described, the explanation of above example
It is only intended to help and understands core concept of the present utility model.For those of ordinary skill in the art, according to the utility model
Thought, there will be changes in specific embodiments and applications, as front-rear axle has motor to participate in the mixed of driving
Close dynamical system etc..In summary, this specification content should not be construed as to limitation of the present utility model.
The foregoing description of the disclosed embodiments, professional and technical personnel in the field are enable to realize or new using this practicality
Type.A variety of modifications to these embodiments will be apparent for those skilled in the art, determine herein
The General Principle of justice can be realized in other embodiments in the case where not departing from spirit or scope of the present utility model.Cause
This, the utility model is not intended to be limited to the embodiments shown herein, and is to fit to and principles disclosed herein
The most wide scope consistent with features of novelty.
Claims (10)
- A kind of 1. on-board component equipment of dynamic flying performance test, it is characterised in that including：Gather data message of the unmanned plane in flight course in real time by sensor, and the data message packing handled, Sensing module as the input data of dynamic flying performance test；It is connected with the sensing module, the decoder module that the supplemental characteristic of the sensing module is acquired and decoded；It is connected with the decoder module, the storage mould stored to the supplemental characteristic decoded in the decoder module Block；It is connected respectively with the sensing module and the decoder module, power supply is provided for the sensing module and the decoder module Power supply module.
- 2. on-board component equipment according to claim 1, it is characterised in that also include：Structure housing, the structure housing Integrated and Streamline Design.
- 3. on-board component equipment according to claim 1, it is characterised in that the sensing module is based on MEMS The sensor group of MEMS integrated navigation systems.
- 4. on-board component equipment according to claim 3, it is characterised in that the sensor group includes：MEMS gyro, add Speedometer, the Big Dipper/GPS, navigational computer.
- 5. on-board component equipment according to claim 1, it is characterised in that the memory module is that the on-board component is set Standby internal storage or External memory equipment.
- 6. on-board component equipment according to claim 1, it is characterised in that the power supply module is standard lithium battery Group, its voltage output standard are set according to the internal circuit demand of the on-board component equipment.
- A kind of 7. dynamic flying Performance Test System, it is characterised in that including：Described in the claims 1-6 any one On-board component equipment, in addition to：It is connected with the on-board component equipment, carries out the host computer of data readback.
- 8. dynamic flying Performance Test System according to claim 7, it is characterised in that the host computer is PC, platform Formula machine or tablet personal computer.
- 9. dynamic flying Performance Test System according to claim 7, it is characterised in that the host computer is portable reinforcing Data readback equipment.
- 10. dynamic flying Performance Test System according to claim 7, it is characterised in that the host computer is high-performance Test data plays back and processing equipment.
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108196578A (en) * | 2018-01-24 | 2018-06-22 | 广东容祺智能科技有限公司 | A kind of digitlization unmanned plane during flying Performance Test System |
| CN109669434A (en) * | 2018-11-13 | 2019-04-23 | 昆山优尼电能运动科技有限公司 | Unmanned plane automated testing method and system |
| CN110928324A (en) * | 2019-12-30 | 2020-03-27 | 北京润科通用技术有限公司 | Unmanned aerial vehicle flight parameter acquisition equipment and calibration method thereof |
| CN111179464A (en) * | 2020-01-03 | 2020-05-19 | 深圳市瑞达飞行科技有限公司 | Flight data processing method, file construction, processing device and electronic equipment |
| CN112198887A (en) * | 2019-12-31 | 2021-01-08 | 北京理工大学 | Multi-rotor unmanned aerial vehicle onboard computer performance evaluation system method |
| CN114229033A (en) * | 2021-12-17 | 2022-03-25 | 广州信邦智能装备股份有限公司 | High-low temperature test system for flight device position marker |
| CN114577264A (en) * | 2022-03-02 | 2022-06-03 | 北京卫星环境工程研究所 | Optical fiber multi-module multi-parameter ground online testing method |
-
2017
- 2017-03-13 CN CN201720242078.3U patent/CN206734657U/en active Active
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108196578A (en) * | 2018-01-24 | 2018-06-22 | 广东容祺智能科技有限公司 | A kind of digitlization unmanned plane during flying Performance Test System |
| CN109669434A (en) * | 2018-11-13 | 2019-04-23 | 昆山优尼电能运动科技有限公司 | Unmanned plane automated testing method and system |
| CN110928324A (en) * | 2019-12-30 | 2020-03-27 | 北京润科通用技术有限公司 | Unmanned aerial vehicle flight parameter acquisition equipment and calibration method thereof |
| CN110928324B (en) * | 2019-12-30 | 2023-07-14 | 北京润科通用技术有限公司 | Unmanned plane flight parameter acquisition equipment and calibration method thereof |
| CN112198887A (en) * | 2019-12-31 | 2021-01-08 | 北京理工大学 | Multi-rotor unmanned aerial vehicle onboard computer performance evaluation system method |
| CN112198887B (en) * | 2019-12-31 | 2022-04-01 | 北京理工大学 | Multi-rotor unmanned aerial vehicle onboard computer performance evaluation system method |
| CN111179464A (en) * | 2020-01-03 | 2020-05-19 | 深圳市瑞达飞行科技有限公司 | Flight data processing method, file construction, processing device and electronic equipment |
| CN114229033A (en) * | 2021-12-17 | 2022-03-25 | 广州信邦智能装备股份有限公司 | High-low temperature test system for flight device position marker |
| CN114577264A (en) * | 2022-03-02 | 2022-06-03 | 北京卫星环境工程研究所 | Optical fiber multi-module multi-parameter ground online testing method |
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