CN210244152U - Unmanned aerial vehicle flight controller check out test set - Google Patents
Unmanned aerial vehicle flight controller check out test set Download PDFInfo
- Publication number
- CN210244152U CN210244152U CN201920907462.XU CN201920907462U CN210244152U CN 210244152 U CN210244152 U CN 210244152U CN 201920907462 U CN201920907462 U CN 201920907462U CN 210244152 U CN210244152 U CN 210244152U
- Authority
- CN
- China
- Prior art keywords
- flight controller
- aerial vehicle
- unmanned aerial
- unit
- vehicle flight
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Traffic Control Systems (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle flight controller detection device, which comprises a test unit, a control unit and a control unit, wherein the test unit is connected with an unmanned aerial vehicle flight controller and is used for detecting the voltage of the unmanned aerial vehicle flight controller; the communication unit is used for communicating with the unmanned aerial vehicle flight controller to acquire hardware operation information and program software operation information of the unmanned aerial vehicle flight controller; the MCU processing unit is used for processing the voltage data detected by the test unit, processing the operation information of the unmanned aircraft flight controller obtained by the communication unit and obtaining test result information according to the processed voltage data and the operation information; the display unit is used for directly displaying the test result; the storage unit is used for storing the unmanned aerial vehicle flight controller operation data obtained through testing; the test unit, the storage unit, the communication unit and the display unit are all connected with the MCU processing unit. The purpose of rapidly detecting the flight controller in the production process is achieved, and the production detection efficiency of the unmanned aerial vehicle flight controller is improved.
Description
Technical Field
The utility model belongs to the technical field of a remote detection unmanned aerial vehicle flight controller's technique and specifically relates to an unmanned aerial vehicle flight controller check out test set.
Background
At present, unmanned aerial vehicle has been widely used in a great deal of fields, including movie & TV industry, scientific research, accident rescue etc. as long as formulate corresponding rule and service conditions, unmanned aerial vehicle can bring a lot of convenience for our life in fact, and in fact, unmanned aerial vehicle is more and more extensive in civilian field.
Due to the economy, safety and easy operability of the unmanned aerial vehicle, the unmanned aerial vehicle has vigorous demands in many civil fields, and the small unmanned aerial vehicle can be widely applied to the fields of disaster prevention and reduction, search and rescue, traffic supervision, resource exploration, homeland resource monitoring, frontier defense patrol, forest fire prevention, meteorological detection, crop estimation, pipeline patrol and the like. Due to the characteristics of aviation characteristics and large-area patrol of the small unmanned aerial vehicle, the unmanned aerial vehicle has the advantages in real-time monitoring and evaluation of natural disasters such as flood, drought, earthquake, forest fire and the like.
However, in the prior art, generally, the detection of the flight control of the unmanned aerial vehicle which is just produced and assembled is that the unmanned aerial vehicle flight controller is manually and directly powered on, then the universal meter is used for testing the voltage of the flight controller, then the flight control board card is manually installed on the tested unmanned aerial vehicle for being powered on, running and starting, and whether the unmanned aerial vehicle can automatically keep the normal flight attitude of the aircraft is checked; the detection mode can only realize preliminary detection, but when the unmanned aircraft fails after being tested and used, hardware operation information (a gyroscope, an accelerometer, a geomagnetic induction device, an air pressure sensor for roughly controlling the hovering height, an ultrasonic sensor for accurately controlling the low altitude height or avoiding obstacles, an optical flow sensor for accurately determining the hovering horizontal position, operation information such as roughly positioning the horizontal position height, a GPS module, a control circuit and the like) and program software operation information of the flight controller cannot be known, and at the moment, professional technicians are required to check on site, problems are judged according to experience of the professional technicians, and then the problems are solved, so that the detection efficiency of the flight controller of the unmanned aircraft is quite low, and the detection effect cannot meet the requirements of current high-efficiency production.
Disclosure of Invention
The utility model aims at solving the not enough of above-mentioned technique and the unmanned aerial vehicle flight controller check out test set that a can be comparatively quick detects unmanned aerial vehicle flight controller each item operational information in process of production.
The utility model discloses an unmanned aerial vehicle flight controller check out test set, include:
the test unit is connected with the unmanned aerial vehicle flight controller and used for detecting the voltage of the unmanned aerial vehicle flight controller;
the communication unit is used for communicating with the unmanned aerial vehicle flight controller to acquire hardware operation information and program software operation information of the unmanned aerial vehicle flight controller;
the MCU processing unit is used for processing the voltage data detected by the test unit and the operation information of the unmanned aircraft flight controller obtained by the communication unit and obtaining test result information according to the processed voltage data and the operation information;
and the display unit is used for directly displaying the test result.
The storage unit is used for storing the unmanned aerial vehicle flight controller operation data obtained through testing;
the test unit, the storage unit, the communication unit and the display unit are all connected with the MCU processing unit.
Further preferably, the system also comprises a wireless communication unit, and the MCU processing unit is connected with the wireless communication unit.
Further preferably, the wireless communication unit is a 4G wireless communication module.
Further preferably, the system also comprises a USB interface, and the USB interface is connected with the MCU processing unit.
Further preferably, the device further comprises a protection unit, and the protection unit is connected with the MCU processing unit.
Further preferably, the test unit consists of an ADC sampling chip and a test interface connected with the unmanned aircraft flight controller.
Further preferably, the protection unit comprises an optocoupler U4, a comparator U5A, a resistor R4, a resistor R5, a resistor R6, a resistor R7 and a capacitor C9, wherein the anode of a photodiode of the optocoupler U4 is connected with one end of the resistor R6, and the cathode of the photodiode is connected with ground; the collector of the triode in the optical coupler U4 is respectively connected with one end of a resistor R7, a capacitor C9 and the negative input end of a comparator U5A, and the emitter of the triode is connected with the ground; the positive input end of the comparator U5A is connected with the resistor R4, and the output end of the comparator U5A is respectively connected with the resistor R5 and the MCU processing unit; the resistor R6, the resistor R7 and the resistor R4 are all connected with a positive electrode 5V power supply; the comparators U5A and R5 are both connected to a VCC power supply.
Further preferably, the communication unit is composed of a communication chip, a communication chip connection peripheral circuit and a docking interface.
The utility model discloses an unmanned aerial vehicle flight controller check out test set, its structure passes through the communication unit, links to each other with the flight controller with the test unit and can demonstrate on the display screen fast the information and the test result of each hardware, program software on the flight controller to the realization carries out the purpose of short-term test flight controller in process of production, promotes unmanned aerial vehicle flight controller production detection efficiency.
Drawings
FIG. 1 is a schematic view of the overall structure of embodiment 1;
FIG. 2 is a schematic diagram showing the structure of an MCU processing unit according to embodiment 1;
FIG. 3 is a schematic view of the test cell structure of example 1;
FIG. 4 is a schematic structural view of a communication unit according to embodiment 1;
FIG. 5 is a schematic view of the structure of a display unit of embodiment 1;
FIG. 6 is a schematic view of the structure of a memory cell of embodiment 1;
fig. 7 is a schematic structural diagram of a 4G wireless communication unit according to embodiment 1;
fig. 8 is a schematic view of the structure of the protection unit of embodiment 1.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art all belong to the protection scope of the present invention.
Example 1:
as shown in fig. 1 to 8, the unmanned aerial vehicle flight controller detection device described in this embodiment includes a test unit 2, a communication unit 3, an MCU processing unit 1, a display unit 4, and a storage unit 5; the test unit 2, the storage unit 5, the communication unit 3 and the display unit 4 are all connected with the MCU processing unit 1. The MCU processing unit adopts a 32-bit microcontroller series, has a wide voltage working range from 2.5V to 5.5V, has the highest working frequency of 50MHz, and has various communication interfaces (shown in figure 2) such as UART, SP I, I2C and the like; the storage unit adopts a W25Q128FV storage module, the capacity reaches 16M-Bytes, the erasing/programming is carried out for more than 10 ten thousand times, and the service life reaches 20 years (as shown in figure 6); the display unit is an LCD display unit, adopts an LCD12864 model, supports a Chinese character library, and is used for visually displaying the detection, upgrading and parameter adjustment results of the flight control board card (as shown in FIG. 4).
The design principle of the structure is as follows: the power supply 9 is connected with the flight controller and the detection equipment respectively and then is electrified to operate, and a test interface on the test unit is connected with the flight controller to detect the voltage of the unmanned aerial vehicle flight controller during operation; an interface on the communication unit is also connected with a communication interface of the flight controller, so that the hardware operation information and the program software operation information of the unmanned aerial vehicle flight controller are further acquired; and then, inputting the voltage data detected by the test unit and the operation information of the unmanned aerial vehicle flight controller obtained by the communication unit into the MCU processing unit for data rapid processing to obtain a test result, and transmitting the obtained test result data and information to the display unit for direct display and the storage unit for storage respectively.
In this embodiment, the wireless communication device further includes a wireless communication unit (4G wireless communication unit 6), and the MCU processing unit is connected to the wireless communication unit. The wireless connection can be realized through an upper computer of a PC end or a mobile phone APP at any time, the remote connection can be realized only in a place covered by a mobile phone network signal, the communication distance is not limited at all, the setting of a test standard can be realized at any time, and a test result stored in a storage unit can be read; further realize functions such as remote test of flight control, remote upgrade of software, remote parameter adjustment. The 4G wireless communication unit 6 can improve the efficiency and speed of data transmission. Furthermore, this equipment control panel volume is less, easily carries to can work in multiple outdoor environment, operating personnel only need through host computer alright remote operation equipment, in order being in normal use state.
In this embodiment, the device further includes a USB interface 8, and the USB interface is connected to the MCU processing unit. Under the condition that a wireless signal is weak, the USB interface of the detection equipment is connected with an upper computer or a PC (personal computer), so that the functions of setting the test standard, reading the test result stored in the storage unit, performing flight control test, upgrading software, adjusting parameters and the like are realized.
In this embodiment, the device further includes a protection unit 7, and the protection unit is connected to the MCU processing unit. The protection unit comprises an optical coupler U4, a comparator U5A, a resistor R4, a resistor R5, a resistor R6, a resistor R7 and a capacitor C9, wherein the anode of a photosensitive diode of the optical coupler U4 is connected with one end of the resistor R6, and the cathode of the photosensitive diode is connected with the ground; the collector of the triode in the optical coupler U4 is respectively connected with one end of a resistor R7, a capacitor C9 and the negative input end of a comparator U5A, and the emitter of the triode is connected with the ground; the positive input end of the comparator U5A is connected with the resistor R4, and the output end of the comparator U5A is respectively connected with the resistor R5 and the MCU processing unit; the resistor R6, the resistor R7 and the resistor R4 are all connected with a positive electrode 5V power supply; the comparators U5A and R5 are both connected to a VCC power supply. (as shown in fig. 8), in the detection process, whether the detection device is disassembled is judged by the photodiode of the optical coupler, and when the photodiode of the optical coupler U4 senses that the detection device is disassembled, the power supply of the detection device is turned off by the comparator U5A, so that the personal safety of an operator can be effectively protected, that is, the anti-disassembly protection effect is realized.
In this embodiment, the test unit 2 is composed of an ADC sampling chip and a test interface connected to the drone flight controller. The test unit adopts an ADC sampling chip of ADS1118 type, the chip is a high-precision low-power consumption 16-bit analog-to-digital converter, the highest data conversion rate can reach 860 sampling per second, and the wide voltage working range of 2.0V to 5.5V is shown in figure 3.
In this embodiment, the communication unit 3 is composed of a communication chip, a communication chip connection peripheral circuit, and a docking interface (as shown in fig. 4). The structure of the unmanned aerial vehicle flight controller enables the communication effect with the unmanned aerial vehicle flight controller to be better, and hardware operation information and program software operation information of the unmanned aerial vehicle flight controller are completely and reliably acquired; the use performance is improved.
The present invention is not limited to the above-mentioned preferred embodiments, and any other products in various forms can be obtained by the teaching of the present invention, but any changes in the shape or structure thereof, which have the same or similar technical solutions as the present invention, fall within the protection scope of the present invention.
Claims (7)
1. The utility model provides an unmanned aerial vehicle flight controller check out test set which characterized in that includes:
the test unit is connected with the unmanned aerial vehicle flight controller and used for detecting the voltage of the unmanned aerial vehicle flight controller, and the test unit consists of an ADC (analog to digital converter) sampling chip and a test interface connected with the unmanned aerial vehicle flight controller;
the communication unit is used for communicating with the unmanned aerial vehicle flight controller to acquire hardware operation information and program software operation information of the unmanned aerial vehicle flight controller;
the MCU processing unit is used for processing the voltage data detected by the test unit, processing the operation information of the unmanned aircraft flight controller obtained by the communication unit and obtaining test result information according to the processed voltage data and the operation information;
the display unit is used for directly displaying the test result;
the storage unit is used for storing the unmanned aerial vehicle flight controller operation data obtained through testing;
the test unit, the storage unit, the communication unit and the display unit are all connected with the MCU processing unit.
2. The unmanned aerial vehicle flight controller detection device of claim 1, further comprising a wireless communication unit, wherein the MCU processing unit is connected with the wireless communication unit.
3. The unmanned aerial vehicle flight controller detection apparatus of claim 2, wherein the wireless communication unit is a 4G wireless communication module.
4. The unmanned aerial vehicle flight controller detection device of claim 3, further comprising a USB interface, wherein the USB interface is connected to the MCU processing unit.
5. The unmanned aerial vehicle flight controller detection apparatus of claim 3, further comprising a protection unit, the protection unit being connected to the MCU processing unit.
6. The unmanned aerial vehicle flight controller detection device of claim 5, wherein the protection unit comprises an optocoupler U4, a comparator U5A, a resistor R4, a resistor R5, a resistor R6, a resistor R7 and a capacitor C9, wherein the positive electrode of a photodiode of the optocoupler U4 is connected with one end of the resistor R6, and the negative electrode of the optocoupler U4 is connected with the ground; the collector of the triode in the optical coupler U4 is respectively connected with one end of a resistor R7, a capacitor C9 and the negative input end of a comparator U5A, and the emitter of the triode is connected with the ground; the positive input end of the comparator U5A is connected with the resistor R4, and the output end of the comparator U5A is respectively connected with the resistor R5 and the MCU processing unit; the resistor R6, the resistor R7 and the resistor R4 are all connected with a positive electrode 5V power supply; the comparators U5A and R5 are both connected to a VCC power supply.
7. The unmanned aerial vehicle flight controller detection device of claim 1, wherein the communication unit is composed of a communication chip, a communication chip connection peripheral circuit and a docking interface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920907462.XU CN210244152U (en) | 2019-06-17 | 2019-06-17 | Unmanned aerial vehicle flight controller check out test set |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920907462.XU CN210244152U (en) | 2019-06-17 | 2019-06-17 | Unmanned aerial vehicle flight controller check out test set |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210244152U true CN210244152U (en) | 2020-04-03 |
Family
ID=69986003
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920907462.XU Active CN210244152U (en) | 2019-06-17 | 2019-06-17 | Unmanned aerial vehicle flight controller check out test set |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210244152U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111948572A (en) * | 2020-08-20 | 2020-11-17 | 珠海云洲智能科技有限公司 | Automatic detection circuit and automatic detection device of unmanned ship |
| CN117193258A (en) * | 2023-10-10 | 2023-12-08 | 朗戈智能系统(上海)有限公司 | Automatic detection method, equipment and computer readable medium for light-operated controller |
-
2019
- 2019-06-17 CN CN201920907462.XU patent/CN210244152U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111948572A (en) * | 2020-08-20 | 2020-11-17 | 珠海云洲智能科技有限公司 | Automatic detection circuit and automatic detection device of unmanned ship |
| CN117193258A (en) * | 2023-10-10 | 2023-12-08 | 朗戈智能系统(上海)有限公司 | Automatic detection method, equipment and computer readable medium for light-operated controller |
| CN117193258B (en) * | 2023-10-10 | 2024-05-07 | 朗戈智能系统(上海)有限公司 | Automatic detection method, equipment and computer readable medium for light-operated controller |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105588923B (en) | Method of environmental monitoring based on environment monitor and environment monitoring device | |
| CN105179013B (en) | Coal illegal mining monitoring method based on vibration monitoring and positioning | |
| CN210244152U (en) | Unmanned aerial vehicle flight controller check out test set | |
| CN203930095U (en) | A kind of integrated meteorology monitoring instrument | |
| CN204178533U (en) | Remote intelligent monitoring instrument | |
| CN103822667A (en) | Temperature-humidity acquisition system based on Bluetooth technology | |
| CN103472377A (en) | Partial discharging point locating device for GIS type test based on vibration detection | |
| CN111736503A (en) | Environment monitoring system for cultural relic collection display place | |
| CN208314500U (en) | Environmental monitoring system | |
| CN208752423U (en) | A kind of security detection equipment, safety features and safety detecting system | |
| CN104597947A (en) | Gesture interaction type environmental monitoring method and device | |
| CN203958626U (en) | A kind of machine-carried type remote wireless data collection device | |
| CN207301719U (en) | Remote controllers and automatic weather station | |
| CN206827845U (en) | A kind of elevator real-time monitoring device | |
| CN203069733U (en) | A vibration-detection-based partial discharging point positioning device used for GIS tests | |
| CN107357225A (en) | Remote controllers and automatic weather station | |
| CN104111637A (en) | Outdoor data acquisition and control equipment | |
| CN209656656U (en) | A kind of wireless gas detecting instrument | |
| CN206740738U (en) | Multi-parameter gas detection means based on unmanned plane | |
| CN106092201A (en) | A kind of wheeled gas well crusing robot | |
| CN205988012U (en) | A kind of wearable petrochemical industry safety monitoring helmet | |
| CN106954621B (en) | Ultrasonic bird repeller detector and detection method | |
| CN108731793A (en) | A kind of hand-held noise level monitor | |
| CN210462803U (en) | Multifunctional lighting device | |
| CN203908590U (en) | Distributed underground tunnel environment information integrated monitoring system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |