CN112363529A - Unmanned aerial vehicle navigation system terminal with protection function - Google Patents
Unmanned aerial vehicle navigation system terminal with protection function Download PDFInfo
- Publication number
- CN112363529A CN112363529A CN202011143518.2A CN202011143518A CN112363529A CN 112363529 A CN112363529 A CN 112363529A CN 202011143518 A CN202011143518 A CN 202011143518A CN 112363529 A CN112363529 A CN 112363529A
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- China
- Prior art keywords
- side wall
- terminal
- box
- fixedly connected
- terminal box
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Links
- 238000007789 sealing Methods 0.000 claims abstract description 22
- 238000009434 installation Methods 0.000 claims description 21
- 229910000963 austenitic stainless steel Inorganic materials 0.000 claims description 5
- 239000004743 Polypropylene Substances 0.000 claims description 3
- 239000000835 fiber Substances 0.000 claims description 3
- -1 polypropylene Polymers 0.000 claims description 3
- 229920001155 polypropylene Polymers 0.000 claims description 3
- 239000000428 dust Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000004078 waterproofing Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
Abstract
The invention discloses an unmanned aerial vehicle navigation system terminal with a protection function, which comprises a terminal box, a first display screen, a terminal processor, a control box, a second display screen and a WIFI transmitter, wherein the outer side wall of the terminal box is provided with a positioning groove, the control box is fixedly arranged on the inner side wall of the terminal box, the inner bottom of the terminal box is fixedly connected with a plurality of buffer springs, the tail ends of the buffer springs are fixedly connected with a mounting frame, the terminal processor is arranged on the inner bottom of the mounting frame, the first display screen is arranged on the inner side wall of the mounting frame, the mounting frame penetrates through the positioning groove, the outer side wall of the terminal box is rotatably connected with a fixing box, the fixing box drives a sealing plate to move rightwards through a connecting rod when the fixing box rotates downwards, so that the sealing plate is tightly attached to the inner side wall of a filter tank, and moisture is prevented from entering the inside of the terminal box through, causing short circuit of the components inside the sealing plate and protecting the terminal box from being damaged.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle navigation system terminal with a protection function.
Background
The unmanned plane is an unmanned aerial vehicle operated by radio remote control equipment and a self-contained program control device. Unmanned aerial vehicle need carry out the WIFI with the terminal and be connected, appoints the flight route for unmanned aerial vehicle through the terminal to come to carry out real time monitoring to the picture that unmanned aerial vehicle shot through the terminal, unmanned aerial vehicle is unmanned vehicles's general name in fact, can divide into from the technical angle definition: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane, etc. Compared with manned aircraft, it has small, the cost is low, convenient to use, and unmanned aerial vehicle can be applied to disaster area rescue, agriculture and forestry plant protection, meteorological observation and movie & TV drama and shoot.
Traditional unmanned aerial vehicle navigation terminal is owing to be in the open air and can take place to collide with in the use, owing to lack preceding shock mitigation system, the display device that may lead to the terminal of colliding with is impaired to the content that unable real time monitoring unmanned aerial vehicle shot, and when not using, moisture may flow into the terminal through the louvre on the terminal inside and do not lead to the terminal inside short circuit that takes place, consequently need one kind to have protect function unmanned aerial vehicle navigation terminal.
Disclosure of Invention
The invention aims to solve the defects in the prior art, and provides an unmanned aerial vehicle navigation system terminal with a protection function.
In order to achieve the purpose, the invention adopts the following technical scheme:
an unmanned aerial vehicle navigation system terminal with a protection function comprises a terminal box, a first display screen, a terminal processor, a control box, a second display screen and a WIFI transmitter, wherein a positioning groove is formed in the outer side wall of the terminal box, the control box is fixedly arranged on the inner side wall of the terminal box, a plurality of buffer springs are fixedly connected to the inner bottom of the terminal box, the tail ends of the buffer springs are fixedly connected with an installation frame, the terminal processor is arranged on the inner bottom of the installation frame, the first display screen is arranged on the inner side wall of the installation frame, the installation frame penetrates through the positioning groove, a fixing box is rotatably connected to the outer side wall of the terminal box, the second display screen is fixedly arranged on the outer side wall of the fixing box, the WIFI transmitter is fixedly connected to the inner side wall of the fixing box, a filter tank is formed in the bottom of the terminal box, an installation cavity is formed in the terminal box, the terminal box comprises a terminal box and is characterized in that a sliding groove is formed in the inner side wall of the terminal box, the mounting cavity is communicated with the sliding groove, a waterproof mechanism is fixedly connected to the inner side wall of the mounting cavity, the tail end of the waterproof mechanism is tightly abutted to the inner side wall of the filtering groove, a fixing groove is formed in the outer side wall of the terminal box, a positioning cavity is formed in the terminal box, an opening and closing mechanism is fixedly connected to the inner side wall of the positioning cavity, a locking block is fixedly connected to the outer side wall of the fixing box, and the opening and closing mechanism is tightly abutted to the outer side.
Preferably, waterproofing mechanism includes the first pressure spring of fixed connection on the installation cavity inside wall, first pressure spring's terminal fixedly connected with closing plate, the installation cavity is run through to the end of closing plate, the end of closing plate offsets tightly with the inside wall of filter-tank, it is connected with the connecting rod to rotate on the lateral wall of installation cavity, the connecting rod runs through the sliding tray, the end of connecting rod rotates with the lateral wall of stationary box to be connected.
Preferably, the filter screen is fixedly installed on the inner side wall of the filter tank, and the filter screen is made of polypropylene fibers.
Preferably, the mechanism that opens and shuts includes the second pressure spring of fixed connection on the locating cavity inner wall, the terminal fixedly connected with locating piece of second pressure spring, the locating piece runs through the locating cavity, fixedly connected with pull rod on the lateral wall of locating piece, the pulling groove has been seted up on the lateral wall of terminal box, the pull rod runs through the pulling groove, the lateral wall and the locking block counterbalance of locating piece are tight.
Preferably, the pulling groove communicates with the inside of the fixing groove.
Preferably, the sealing plate is closely attached to the inner side wall of the filter tank.
Preferably, the positioning block and the locking block are made of austenitic stainless steel, and the positioning block and the locking block are in barb shapes.
Preferably, the outer side wall of the terminal box is symmetrically and fixedly connected with a rocker and a button.
Compared with the prior art, the invention has the beneficial effects that:
1. when the terminal box needs to be used, the pull rod is pushed leftwards, the pull rod drives the positioning block to move leftwards, the positioning block moves leftwards, so that the positioning block loses the limiting function of the locking block, then the fixed box rotates upwards, the fixed box is opened, in the process of upward rotation of the fixed box, the fixed box drives the connecting rod to start to move upwards, the connecting rod drives the sealing plate to move leftwards, the sealing plate moves leftwards, so that the filter tank is opened, the filter screen is installed on the inner side wall of the filter tank, the filter screen can filter external dust, the dust is prevented from entering the inside of the terminal box, so that the service life of components inside the terminal box is shortened, after the terminal box is used, the fixed box rotates downwards, the fixed box drives the locking block to rotate downwards until the locking block abuts against the outer side wall of the positioning block, so that the terminal box and the fixed box are locked, and when, the fixing box drives the sealing plate to move rightwards through the connecting rod, so that the sealing plate is tightly attached to the inner side wall of the filter tank, the situation that moisture enters the terminal box through the filter tank is avoided, the short circuit of an internal component of the sealing plate is caused, and the terminal box is protected from being damaged.
2. When terminal box takes place to collide with because gravity can the downstream when colliding with carelessly, buffer spring can play the cushioning effect to the installing frame to reduce the vibration that the installing frame received, guarantee the safety of installing frame, the material of locking piece is austenitic stainless steel, and austenitic stainless steel structure is stable, can use for a long time and need not change.
Drawings
Fig. 1 is a perspective view of an unmanned aerial vehicle navigation system terminal with a protection function according to the present invention;
FIG. 2 is a schematic structural view of the present invention;
FIG. 3 is an enlarged view of a portion A of the present invention;
FIG. 4 is an enlarged view of a portion B of the present invention;
FIG. 5 is an enlarged view of a portion C of the present invention;
fig. 6 is a block diagram of the system of the present invention.
In the figure: 1 terminal box, 2 constant head tank, 3 installing frames, 4 first display screens, 5 terminal treater, 6 buffer spring, 7 control box, 8 second display screens, 9 WIFI transmitter, 10 filter tanks, 11 filter screens, 12 installation cavities, 13 first pressure spring, 14 sealing plates, 15 connecting rods, 16 sliding chutes, 17 fixed slots, 18 locating pieces, 19 locating cavities, 20 second pressure spring, 21 pull rods, 22 pulling grooves, 23 locking blocks, 24 fixed boxes, 25 terminal central processing module, 26 display module, 27 control module, 28 WIFI transmitting module, 29 WIFI receiving module, 30 unmanned aerial vehicle central processing module, 31 navigation positioning module, 32 ultrasonic ranging module, 33 shooting storage module.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
Referring to fig. 1-6, an unmanned aerial vehicle navigation system terminal with protection function comprises a terminal box 1, a first display screen 4, a terminal processor 5, a control box 7, a second display screen 8, a WIFI transmitter 9, a positioning groove 2 is arranged on the outer side wall of the terminal box 1, the control box 7 is fixedly arranged on the inner side wall of the terminal box 1, a plurality of buffer springs 6 are fixedly connected to the inner bottom of the terminal box 1, a mounting frame 3 is fixedly connected to the tail ends of the buffer springs 6, the terminal processor 5 is arranged on the inner bottom of the mounting frame 3, the first display screen 4 is arranged on the inner side wall of the mounting frame 3, the mounting frame 3 penetrates through the positioning groove 2, a fixing box 24 is rotatably connected to the outer side wall of the terminal box 1, the second display screen 8 is fixedly arranged on the outer side wall of the fixing box 24, the WIFI transmitter 9 is fixedly connected to the inner side wall of the fixing box 24, a filter tank, a filter screen 11 is fixedly installed on the inner side wall of the filter tank 10, the filter screen 11 is made of polypropylene fibers, an installation cavity 12 is formed in the terminal box 1, a sliding groove 16 is formed in the inner side wall of the terminal box 1, and the installation cavity 12 is communicated with the sliding groove 16;
a waterproof mechanism is fixedly connected to the inner side wall of the mounting cavity 12, the tail end of the waterproof mechanism is abutted against the inner side wall of the filter tank 10, the waterproof mechanism comprises a first pressure spring 13 fixedly connected to the inner side wall of the mounting cavity 12, a sealing plate 14 is fixedly connected to the tail end of the first pressure spring 13, the tail end of the sealing plate 14 penetrates through the mounting cavity 12, the tail end of the sealing plate 14 is abutted against the inner side wall of the filter tank 10, the sealing plate 14 is tightly attached to the inner side wall of the filter tank 10, a connecting rod 15 is rotatably connected to the outer side wall of the mounting cavity 12, the connecting rod 15 penetrates through a sliding groove 16, the tail end of the connecting rod 15 is rotatably connected with the outer side wall of a fixed box 24, a fixed groove 17 is;
the inside wall fixedly connected with mechanism that opens and shuts of location chamber 19, the mechanism that opens and shuts includes second pressure spring 20 of fixed connection on the inside wall of location chamber 19, the terminal fixedly connected with locating piece 18 of second pressure spring 20, locating piece 18 runs through location chamber 19, fixedly connected with pull rod 21 on the lateral wall of locating piece 18, pulling groove 22 has been seted up on the lateral wall of terminal box 1, pulling groove 22 is linked together with the inside of fixed slot 17, pull rod 21 runs through pulling groove 22, the lateral wall of locating piece 18 offsets tightly with locking block 23, fixedly connected with locking block 23 on the lateral wall of fixed box 24, it offsets tightly with the lateral wall of locking block 23 to open and shut the mechanism, the material of locating piece 18 and locking block 23 is austenitic stainless steel, the shape of locating piece 18 and locking block 23 all is the barb form, barb form is convenient for locking block 23 and locating piece 18 to offset tightly, realize the locking effect, symmetry fixedly connected with rocker and button on the lateral wall of terminal box.
The control module 27 is installed inside the control box 7, the display module 26 is installed inside the first display screen 4 and the second display screen 8, the terminal central processing module 25 is installed inside the terminal processor 5, the WIFI transmitting module 28 is installed inside the WIFI transmitter 9, the terminal processor 5 is electrically connected with the WIFI transmitter 9, a rocker on the outer side wall of the terminal box 1 is electrically connected with the control box 7, the first display screen 4 and the second display screen 8 are both electrically connected with the terminal processor 5, the WIFI receiving module 29, the unmanned aerial vehicle central processing module 30, the navigation positioning module 31, the ultrasonic ranging module 32 and the shooting storage module 33 are all installed inside the unmanned aerial vehicle, the WIFI transmitting module 28 is connected with the WIFI receiving module 29 inside the unmanned aerial vehicle, the shooting storage module 33 stores shot images, and the navigation positioning module 31 transmits the position of the navigation positioning module 31 to the unmanned aerial vehicle central processing module 30, the unmanned aerial vehicle central processing module 30 transmits the signals to the WIFI transmitting module 28 through the WIFI receiving module 29, the signals are transmitted to the terminal central processing module 25 through the WIFI transmitting module 28, the signals are finally transmitted to the display module 26 through the terminal central processing module 25, the self-positioning of the unmanned aerial vehicle is displayed on the surface of the first display screen 4, the image signals of the shooting storage module 33 are transmitted to the unmanned aerial vehicle central processing module 30, the unmanned aerial vehicle central processing module 30 is transmitted to the WIFI transmitting module 28 through the WIFI receiving module 29, the signals are transmitted to the terminal central processing module 25 through the WIFI transmitting module 28, the signals are finally transmitted to the display module 26 through the terminal central processing module 25, the shot images are displayed on the second display screen 8 in real time, the ultrasonic ranging module 32 can identify obstacles in front of the unmanned aerial vehicle, when the front of the unmanned aerial vehicle encounters an obstacle, the ultrasonic ranging module 32 transmits signals to the unmanned aerial vehicle central processing module 30, the unmanned aerial vehicle central processing module 30 transmits the signals to the terminal central processing module 25 through the WIFI receiving module 29 and the WIFI transmitting module 28, the terminal central processing module 25 transmits the signals to the display module 26, the signals are displayed on the first display screen 4, a rocker on the outer side wall of the terminal box 1 is controlled at the moment, the rocker transmits the signals to the control module 27 in the control box 7, the control module 27 transmits the signals to the terminal central processing module 25, the terminal central processing module 25 transmits the signals to the unmanned aerial vehicle central processing module 30 through the WIFI transmitting module 28 and the WIFI receiving module 29, and the unmanned aerial vehicle central processing module 30 controls a power system to avoid obstacles urgently.
In the invention, when in use, the pull rod 21 is pushed leftwards, the pull rod 21 drives the positioning block 18 to move leftwards, the positioning block 18 moves leftwards to compress the second pressure spring 20, the positioning block 18 loses the limiting function on the locking block 23, then the fixed box 24 rotates upwards, the fixed box 24 rotates to drive the connecting rod 15 to rotate upwards, the connecting rod 15 rotates upwards and drives the sealing plate 14 to move leftwards, the sealing plate 14 moves leftwards to open the filter tank 10, heat generated during the operation of components in the terminal box 1 cannot be removed in time is avoided, external dust can be filtered through the terminal box 1, the external dust is prevented from entering the inside of the terminal box 1, after the flight is finished, the fixed box 24 rotates downwards, the sealing plate 14 is driven to move rightwards through the connecting rod 15 until the sealing plate 14 is tightly attached to the inner side wall of the filter tank 10, and moisture is prevented from entering the inside of the terminal box 1 through the filter tank, and then the internal components of the terminal box 1 are short-circuited, and the fixing box 24 drives the locking block 23 to rotate downwards, so that the locking block 23 is abutted against the outer side wall of the positioning block 18, and the locking of the terminal box 1 and the fixing box 24 is realized.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.
Claims (8)
1. An unmanned aerial vehicle navigation system terminal with a protection function comprises a terminal box (1), a first display screen (4), a terminal processor (5), a control box (7), a second display screen (8) and a WIFI transmitter (9), and is characterized in that a positioning groove (2) is formed in the outer side wall of the terminal box (1), the control box (7) is fixedly installed on the inner side wall of the terminal box (1), a plurality of buffer springs (6) are fixedly connected to the inner bottom of the terminal box (1), an installation frame (3) is fixedly connected to the tail ends of the buffer springs (6), the terminal processor (5) is installed on the inner bottom of the installation frame (3), the first display screen (4) is installed on the inner side wall of the installation frame (3), the installation frame (3) penetrates through the positioning groove (2), a fixed box (24) is rotatably connected to the outer side wall of the terminal box (1), the second display screen (8) is fixedly installed on the outer side wall of the fixed box (24), the WIFI transmitter (9) is fixedly connected to the inner side wall of the fixed box (24), the bottom of the terminal box (1) is provided with the filter tank (10), the interior of the terminal box (1) is provided with the installation cavity (12), the inner side wall of the terminal box (1) is provided with the sliding groove (16), the installation cavity (12) is communicated with the sliding groove (16), the inner side wall of the installation cavity (12) is fixedly connected with the waterproof mechanism, the tail end of the waterproof mechanism is tightly abutted to the inner side wall of the filter tank (10), the outer side wall of the terminal box (1) is provided with the fixed groove (17), the interior of the terminal box (1) is provided with the positioning cavity (19), the inner side wall of the positioning cavity (19) is fixedly connected with the opening and closing mechanism, the outer side wall of the fixed box (24) is fixedly connected with the locking block, the opening and closing mechanism is abutted against the outer side wall of the locking block (23).
2. The unmanned aerial vehicle navigation system terminal with the protection function of claim 1, wherein the waterproof mechanism comprises a first pressure spring (13) fixedly connected to the inner side wall of the installation cavity (12), a sealing plate (14) is fixedly connected to the tail end of the first pressure spring (13), the tail end of the sealing plate (14) penetrates through the installation cavity (12), the tail end of the sealing plate (14) abuts against the inner side wall of the filter tank (10), a connecting rod (15) is rotatably connected to the outer side wall of the installation cavity (12), the connecting rod (15) penetrates through the sliding groove (16), and the tail end of the connecting rod (15) is rotatably connected with the outer side wall of the fixing box (24).
3. The unmanned aerial vehicle navigation system terminal with the protection function of claim 1, wherein a filter screen (11) is fixedly installed on an inner side wall of the filter tank (10), and the filter screen (11) is made of polypropylene fibers.
4. The unmanned aerial vehicle navigation system terminal with the protection function of claim 1, wherein the opening and closing mechanism comprises a second pressure spring (20) fixedly connected to the inner side wall of a positioning cavity (19), a positioning block (18) is fixedly connected to the tail end of the second pressure spring (20), the positioning block (18) penetrates through the positioning cavity (19), a pull rod (21) is fixedly connected to the outer side wall of the positioning block (18), a pulling groove (22) is formed in the outer side wall of the terminal box (1), the pull rod (21) penetrates through the pulling groove (22), and the outer side wall of the positioning block (18) abuts against a locking block (23).
5. The unmanned aerial vehicle navigation system terminal with protection function of claim 4, wherein the pulling groove (22) is communicated with the inside of the fixing groove (17).
6. The unmanned aerial vehicle navigation system terminal with protection function of claim 2, wherein the sealing plate (14) is closely attached to the inner side wall of the filter tank (10).
7. The unmanned aerial vehicle navigation system terminal with the protection function of claim 4, wherein the positioning block (18) and the locking block (23) are made of austenitic stainless steel, and the positioning block (18) and the locking block (23) are in the shape of a barb.
8. The unmanned aerial vehicle navigation system terminal with protection function of claim 1, wherein the outer side wall of the terminal box (1) is symmetrically and fixedly connected with rockers and buttons.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011143518.2A CN112363529B (en) | 2020-10-23 | 2020-10-23 | Unmanned aerial vehicle navigation system terminal with protect function |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011143518.2A CN112363529B (en) | 2020-10-23 | 2020-10-23 | Unmanned aerial vehicle navigation system terminal with protect function |
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| Publication Number | Publication Date |
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| CN112363529A true CN112363529A (en) | 2021-02-12 |
| CN112363529B CN112363529B (en) | 2024-02-02 |
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Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104748991A (en) * | 2013-12-26 | 2015-07-01 | 波音公司 | Detection and assessment of damage to composite structure |
| CN207352434U (en) * | 2017-11-13 | 2018-05-11 | 大连海洋大学 | A kind of dedicated computer electronic control unit of Navigation of Pilotless Aircraft |
| WO2018094701A1 (en) * | 2016-11-25 | 2018-05-31 | 深圳市杏桉科技有限公司 | Unmanned aerial vehicle navigation system and navigation method |
| CN109436351A (en) * | 2018-11-19 | 2019-03-08 | 浙江云来集科技有限公司 | A kind of contour autonomous inspection device of earth's surface unmanned plane of long range |
| CN209182715U (en) * | 2019-01-14 | 2019-07-30 | 中国人民解放军空军通信士官学校 | A kind of Navigation of Pilotless Aircraft device |
| CN209215887U (en) * | 2018-12-27 | 2019-08-06 | 航天神舟飞行器有限公司 | A kind of small drone detection and control terminal based on XX6 platform |
| CN110901917A (en) * | 2019-12-17 | 2020-03-24 | 潍坊学院 | But agricultural plant protection unmanned aerial vehicle at remote transmission data to cell-phone terminal |
| KR20200032999A (en) * | 2018-09-19 | 2020-03-27 | 주식회사 티지에스코리아 | Unmanned aerial vehicles adopting protection functions |
| CN111561632A (en) * | 2020-05-21 | 2020-08-21 | 无锡湖山智能科技有限公司 | Automatic agricultural machinery intelligent terminal box based on big dipper location |
-
2020
- 2020-10-23 CN CN202011143518.2A patent/CN112363529B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104748991A (en) * | 2013-12-26 | 2015-07-01 | 波音公司 | Detection and assessment of damage to composite structure |
| WO2018094701A1 (en) * | 2016-11-25 | 2018-05-31 | 深圳市杏桉科技有限公司 | Unmanned aerial vehicle navigation system and navigation method |
| CN207352434U (en) * | 2017-11-13 | 2018-05-11 | 大连海洋大学 | A kind of dedicated computer electronic control unit of Navigation of Pilotless Aircraft |
| KR20200032999A (en) * | 2018-09-19 | 2020-03-27 | 주식회사 티지에스코리아 | Unmanned aerial vehicles adopting protection functions |
| CN109436351A (en) * | 2018-11-19 | 2019-03-08 | 浙江云来集科技有限公司 | A kind of contour autonomous inspection device of earth's surface unmanned plane of long range |
| CN209215887U (en) * | 2018-12-27 | 2019-08-06 | 航天神舟飞行器有限公司 | A kind of small drone detection and control terminal based on XX6 platform |
| CN209182715U (en) * | 2019-01-14 | 2019-07-30 | 中国人民解放军空军通信士官学校 | A kind of Navigation of Pilotless Aircraft device |
| CN110901917A (en) * | 2019-12-17 | 2020-03-24 | 潍坊学院 | But agricultural plant protection unmanned aerial vehicle at remote transmission data to cell-phone terminal |
| CN111561632A (en) * | 2020-05-21 | 2020-08-21 | 无锡湖山智能科技有限公司 | Automatic agricultural machinery intelligent terminal box based on big dipper location |
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| CN112363529B (en) | 2024-02-02 |
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