CN109866935B - Fixed wing unmanned aerial vehicle device of taking photo by plane - Google Patents
Fixed wing unmanned aerial vehicle device of taking photo by plane Download PDFInfo
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- CN109866935B CN109866935B CN201910082551.XA CN201910082551A CN109866935B CN 109866935 B CN109866935 B CN 109866935B CN 201910082551 A CN201910082551 A CN 201910082551A CN 109866935 B CN109866935 B CN 109866935B
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Abstract
Fixed wing unmanned aerial vehicle device of taking photo by plane. The invention relates to an aerial photographing device for a fixed-wing unmanned aerial vehicle. Move linear electric motor I (2) and linear electric motor II (3) on linear electric motor track (1), fixed connection increases piece I (4) on linear electric motor I (2), it has recess I (5) to increase piece I (4) top surface division, the top surface that increases piece I (4) sets up motor support I (6), motor I (7) are packed into in motor support I (6), motor I (7) bottom is unsettled as to recess I (5), the output shaft of motor I (7) passes through shaft coupling I (8) and connects extension rod I (9), the tail end of extension rod I (9) sets up control box I (10), the head end of extension rod I (9) sets up camera I (11), be connected through the wire between control box I (10) and camera I (11). The invention is convenient to use, can shoot at the height of the machine body and also can shoot at the belly position, and has wide application range.
Description
Technical Field
The invention relates to an aerial photographing device for a fixed-wing unmanned aerial vehicle.
Background
At present unmanned aerial vehicle is more and more the task of taking photo by plane of execution, but current fixed wing unmanned aerial vehicle carries the camera in the air mostly 1 or 2, and fixed position, and the application is inflexible, uses inconveniently.
Disclosure of Invention
The invention aims to provide an aerial photographing device of a fixed-wing unmanned aerial vehicle, which is convenient to use, can photograph at the height of a machine body and the belly position, and has a wide application range.
The above purpose is realized by the following technical scheme:
the utility model provides a device is taken photo by plane to fixed wing unmanned aerial vehicle, its constitution includes: the linear motor track 1, a linear motor I2 and a linear motor II 3 run on the linear motor track 1, a heightening block I4 is fixedly connected to the linear motor I2, a groove I5 is formed in the top surface of the heightening block I4, a motor support I6 is arranged on the top surface of the heightening block I4, a motor I7 is installed in the motor support I6, the bottom end of the motor I7 is suspended in the groove I5, an output shaft of the motor I7 is connected with an extension rod I9 through a coupler I8, a control box I10 is arranged at the tail end of the extension rod I9, a camera I11 is arranged at the head end of the extension rod I9, and the control box I10 is connected with the camera I11 through a wire;
the linear motor II 3 is fixedly connected with a heightening block II 12, the top surface of the heightening block II 12 is provided with a groove II 13, the top surface of the heightening block II 12 is provided with a motor support II 14, a motor II 16 is arranged in the motor support II 14, the bottom end of the motor II 16 is suspended in the groove II 13, an output shaft of the motor II 16 is connected with an extension rod II 18 through a coupling II 17, the tail end of the extension rod II 18 is provided with a control box II 19, the head end of the extension rod II 18 is provided with a camera II 20, and the control box II 19 is connected with the camera II 20 through a wire;
the fixing shaft I21 and the fixing shaft II 22 are arranged on the outer side of the linear motor track 1, the fixing shaft I21 is connected with a hollow cross rod I23, the hollow cross rod I23 is communicated with a hollow vertical rod I24, the hollow vertical rod I24 is communicated with a hollow L-shaped rod I25, and the bottom end of the hollow L-shaped rod I25 is connected with a camera III 26;
the fixing shaft II 22 is connected with a hollow cross rod II 27, the hollow cross rod II 27 is communicated with a hollow vertical rod II 28, the hollow vertical rod II 28 is communicated with a hollow L-shaped rod II 29, and the bottom end of the hollow L-shaped rod II 29 is connected with a camera IV 30.
Furthermore, the motor I7, the motor II 16, the linear motor I2 and the linear motor II 3 are all controlled by a microprocessor MCU (microprogrammed control Unit), the microprocessor MCU receives signals of the wireless transceiver circuit II, the wireless transceiver circuit II receives signals of the wireless transceiver circuit I,
the micro-processor MCU also controls the opening of the camera I11, the camera II 20, the camera III 26 and the camera IV 30, the camera I11, the camera II 20, the camera III 26 and the camera IV 30 transmit data to the memory and the upper computer, and the upper computer displays pictures on a screen through the screen splitting device.
Has the beneficial effects that:
1. the invention can pass through the inside of the case, can control the angle and is convenient to use.
2. The remote control device is controlled remotely, the micro processor MCU is provided with an external interface, and the remote control device can be connected with external equipment such as a keyboard and the like, and is convenient to use.
3. According to the invention, the hollow cross rod I, the hollow vertical rod I, the hollow L-shaped rod I, the hollow cross rod II 27, the hollow vertical rod II and the hollow L-shaped rod II can be connected with a plurality of cameras and stably placed on the fixed-wing unmanned aerial vehicle, and the cameras cannot fall off in any parting action.
Description of the drawings:
FIG. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a partially enlarged schematic view of the present invention.
Fig. 3 is a top view of the present invention in a positional relationship.
Fig. 4 is a logic signal flow diagram of the present invention.
Fig. 5 is a circuit diagram of a wireless transceiver according to the present invention.
FIG. 6 is a circuit diagram of a microprocessor MCU of the present invention.
Fig. 7 is a circuit diagram of a motor i of the present invention.
Fig. 8 is a circuit diagram of the motor ii of the present invention.
Fig. 9 is a circuit diagram of a linear motor i 3 of the present invention.
Fig. 10 is a circuit diagram of a linear motor ii of the present invention.
Fig. 11 is a reset circuit diagram of the present invention.
Fig. 12 is a memory circuit diagram of the present invention.
The specific implementation mode is as follows:
the utility model provides a device is taken photo by plane to fixed wing unmanned aerial vehicle, its constitution includes: the linear motor track 1, a linear motor I2 and a linear motor II 3 run on the linear motor track 1, a heightening block I4 is fixedly connected to the linear motor I2, a groove I5 is formed in the top surface of the heightening block I4, a motor support I6 is arranged on the top surface of the heightening block I4, a motor I7 is installed in the motor support I6, the bottom end of the motor I7 is suspended in the groove I5, an output shaft of the motor I7 is connected with an extension rod I9 through a coupler I8, a control box I10 is arranged at the tail end of the extension rod I9, a camera I11 is arranged at the head end of the extension rod I9, and the control box I10 is connected with the camera I11 through a wire;
the linear motor II 3 is fixedly connected with a heightening block II 12, the top surface of the heightening block II 12 is provided with a groove II 13, the top surface of the heightening block II 12 is provided with a motor support II 14, a motor II 16 is arranged in the motor support II 14, the bottom end of the motor II 16 is suspended in the groove II 13, an output shaft of the motor II 16 is connected with an extension rod II 18 through a coupling II 17, the tail end of the extension rod II 18 is provided with a control box II 19, the head end of the extension rod II 18 is provided with a camera II 20, and the control box II 19 is connected with the camera II 20 through a wire;
the fixing shaft I21 and the fixing shaft II 22 are arranged on the outer side of the linear motor track 1, the fixing shaft I21 is connected with a hollow cross rod I23, the hollow cross rod I23 is communicated with a hollow vertical rod I24, the hollow vertical rod I24 is communicated with a hollow L-shaped rod I25, and the bottom end of the hollow L-shaped rod I25 is connected with a camera III 26;
the fixing shaft II 22 is connected with a hollow cross rod II 27, the hollow cross rod II 27 is communicated with a hollow vertical rod II 28, the hollow vertical rod II 28 is communicated with a hollow L-shaped rod II 29, and the bottom end of the hollow L-shaped rod II 29 is connected with a camera IV 30;
the lengths of the hollow vertical rod I24 and the hollow vertical rod II 28 are determined according to the sum of the thickness of the bottom plate of the fixed wing unmanned aerial vehicle and the height of the linear motor track 1.
The length of hollow horizontal pole I23 and hollow horizontal pole II 27 subtract the distance between fixed axle I21 and the fixed axle II 22 for the width of fixed wing unmanned aerial vehicle.
Furthermore, the motor I7, the motor II 16, the linear motor I2 and the linear motor II 3 are all controlled by a microprocessor MCU (microprogrammed control Unit), the microprocessor MCU receives signals of the wireless transceiver circuit II, the wireless transceiver circuit II receives signals of the wireless transceiver circuit I,
the micro-processor MCU also controls the opening of the camera I11, the camera II 20, the camera III 26 and the camera IV 30, the camera I11, the camera II 20, the camera III 26 and the camera IV 30 transmit data to the memory and the upper computer, and the upper computer displays pictures on a screen through the screen splitting device.
Furthermore, the structure of the wireless transceiver circuit ii is the same as that of the wireless transceiver circuit i, the wireless transceiver circuit ii includes a wireless transmitter module U5, the end 1 of the wireless transmitter module U5 is connected to the end 3 of the interface JI2, the end 2 of the wireless transmitter module U5 is connected to the end 4 of the interface JI2, the end 3 of the wireless transmitter module U5 is connected to the end 5 of the interface JI2, the end 4 of the wireless transmitter module U5 is connected to the end 6 of the interface JI2, the end 5 of the wireless transmitter module U5 is connected to the end 7 of the interface JI2, the end 6 of the wireless transmitter module U5 is connected to the end 8 of the interface JI2,
the No. 7 end of the wireless sending module U5 is connected with the No. 18 end of the wireless sending module U5, the No. 15 end of the wireless sending module U5, one end of a capacitor C16, one end of a capacitor C17 and a working voltage VCC, the other end of the capacitor C16 is grounded, the other end of the capacitor C17 is grounded, the No. 8 end of the wireless sending module U5 is connected with the No. 14 end of the wireless sending module U5 and then grounded, the No. 9 end of the wireless sending module U5 is connected with one end of a crystal oscillator CY4, one end of a resistor R26 and one end of a capacitor C25, the No. 10 end of the wireless sending module U5 is connected with the other end of the crystal oscillator CY4, the other end of the resistor R26 and one end of the capacitor C26, the other end of the capacitor C25 is connected with the other end of the capacitor C26 and then grounded,
the No. 11 end of the wireless transmitting module U5 is connected with one end of a capacitor C22, one end of a capacitor C23 and one end of an inductor L6, the other end of the inductor L6 is connected with one end of an inductor L5 and the No. 12 end of the wireless transmitting module U5, the No. 13 end of the wireless transmitting module U5 is connected with the other end of the inductor L5 and one end of an inductor L4, the other end of the inductor L4 is connected with one end of a capacitor C19, the other end of the capacitor C19 is connected with one end of the capacitor C20 and the No. 1 end of an interface J9, the other end of the capacitor C20 is grounded, and the No. 2 end of the interface J9 is grounded;
the No. 16 end of the wireless transmitting module U5 is connected with the No. 17 end of the wireless transmitting module U5 after being connected with the resistor R17 in series and then is grounded with the No. 20 end of the wireless transmitting module U5, and the No. 19 end of the wireless transmitting module U5 is connected with the capacitor C15 in series and then is grounded.
Furthermore, the No. 3 end of the microprocessor MCU is connected with the No. 1 end of the interface J1,
the No. 4 end of the microprocessor MCU is connected with the No. 2 end of the interface J1,
the No. 5 end of the microprocessor MCU is connected with the No. 3 end of the interface J1,
the No. 6 end of the microprocessor MCU is connected with the No. 4 end of the interface J1,
the No. 20 end of the microprocessor MCU is grounded,
the No. 25 end of the microprocessor MCU is connected with one end of a resistor R1, the other end of the resistor R1 is connected with a base electrode b of a triode Q4, an emitting electrode e of the triode Q4 is grounded, a collector electrode c of the triode Q4 is connected with a linear motor II 3 and then is connected with a working voltage VCC,
the number 26 end of the microprocessor MCU is connected with one end of a resistor R2, the other end of the resistor R2 is connected with a base electrode b of a triode Q3, an emitter electrode e of the triode Q3 is grounded, a collector electrode c of the triode Q3 is connected with a working voltage VCC after being connected with a linear motor I2,
the No. 27 end of the microprocessor MCU is connected with one end of a resistor R4, the other end of the resistor R4 is connected with a base electrode b of a triode Q2, an emitting electrode e of the triode Q2 is grounded, a collector electrode c of the triode Q2 is connected with a working voltage VCC after being connected with a motor II 16,
the 28 th end of the microprocessor MCU is connected with one end of a resistor R3, the other end of the resistor R3 is connected with a base electrode b of a triode Q1, an emitter electrode e of the triode Q1 is grounded, a collector electrode c of the triode Q1 is connected with a working voltage VCC after being connected with a motor I7,
the working voltage VCC end is connected with an emitter e of a triode Q5, a collector C of the triode Q5 is connected with one end of a resistor R12 and the No. 3 end of an interface J2, the other end of the resistor R12 is grounded, a base b of the triode Q5 is connected with one end of a resistor R11, the other end of the resistor R11 is connected with one end of the resistor R10, one end of a capacitor C5 and one end of a switch RSTK, the other end of the resistor R10 is grounded, and the other end of the capacitor C5 is connected with the other end of the switch RSTK and then connected with the working voltage VCC end.
Further, the memory circuit includes chip W1, No. 1 end of chip W1 connect microprocessor MCU's No. 40 end, No. 2 end of chip W1 connect microprocessor MCU's No. 20 end, No. 3 end of chip W1 connect microprocessor MCU's No. 8 end, chip W1's No. 4 termination ground, chip W1's No. 5 end connecting resistance R5's one end, chip W1's No. 5 end connecting resistance R6's one end, chip W1's No. 8 end connecting resistance R5's the other end, resistance R6's the other end and operating voltage VCC.
A0 of the chip W1 is connected with a VCC end or a GND end, A1 of the chip W1 is connected with a GND end or a VCC end, SCL and SDA are connected with a pull-up resistor (the data of the pull-up resistor is 10K), and then the chip is connected with an I/O port end of the microprocessor MCU, so that the chip content can be read and written.
The working process is as follows:
the linear motor track 1 penetrates through the engine room, the linear motor I2 and the linear motor II 3 are started to move towards the two sides of the linear motor track 1, the angle between the extension rod I9 and the extension rod II 18 is adjusted, pictures shot by the camera I11 and the camera II 20 are transmitted to the storage circuit and the upper computer,
according to needs, the I23 hollow cross rod is in threaded connection with the I21 fixing shaft, the I23 hollow cross rod, the I24 hollow vertical rod and the I25 hollow L-shaped rod are clamped on the bottom plate part of the cabin, the II 27 hollow cross rod is clamped on the bottom plate part of the cabin, the III 2626 camera and the IV 30 camera are placed on the belly at the bottom end of the cabin to shoot, and multi-angle shooting is achieved.
It is to be understood that the above description is not intended to limit the present invention, and the present invention is not limited to the above examples, and those skilled in the art may make modifications, alterations, additions or substitutions within the spirit and scope of the present invention.
Claims (5)
1. The utility model provides a device is taken photo by plane to fixed wing unmanned aerial vehicle, its constitution includes: linear electric motor track (1), characterized by: the linear motor track (1) is provided with a linear motor I (2) and a linear motor II (3) in a running mode, the linear motor I (2) is fixedly connected with a height increasing block I (4), the top surface of the height increasing block I (4) is provided with a groove I (5), the top surface of the height increasing block I (4) is provided with a motor support I (6), a motor I (7) is arranged in the motor support I (6), the bottom end of the motor I (7) is suspended in the groove I (5), an output shaft of the motor I (7) is connected with an extension rod I (9) through a shaft coupling I (8), the tail end of the extension rod I (9) is provided with a control box I (10), the head end of the extension rod I (9) is provided with a camera I (11), and the control box I (10) is connected with the camera I (11) through a wire;
the linear motor II (3) is fixedly connected with a heightening block II (12), the top surface of the heightening block II (12) is provided with a groove II (13), the top surface of the heightening block II (12) is provided with a motor support II (14), a motor II (16) is arranged in the motor support II (14), the bottom end of the motor II (16) is suspended in the groove II (13), an output shaft of the motor II (16) is connected with an extension rod II (18) through a coupler II (17), the tail end of the extension rod II (18) is provided with a control box II (19), the head end of the extension rod II (18) is provided with a camera II (20), and the control box II (19) is connected with the camera II (20) through a wire;
a fixing shaft I (21) and a fixing shaft II (22) are arranged on the outer side of the linear motor track (1), the fixing shaft I (21) is connected with a hollow cross rod I (23), the hollow cross rod I (23) is communicated with a hollow vertical rod I (24), the hollow vertical rod I (24) is communicated with a hollow L-shaped rod I (25), and the bottom end of the hollow L-shaped rod I (25) is connected with a camera III (26);
the fixed shaft II (22) on connect hollow horizontal pole II (27), hollow horizontal pole II (27) communicate hollow montant II (28), hollow montant II (28) communicate hollow L shape pole II (29), the bottom of hollow L shape pole II (29) connect camera IV (30).
2. The fixed-wing drone aerial device of claim 1, wherein: the motor I (7), the motor II (16), the linear motor I (2) and the linear motor II (3) are all controlled by a microprocessor MCU, the microprocessor MCU receives signals of the wireless transceiver circuit II, the wireless transceiver circuit II receives signals of the wireless transceiver circuit I,
the microprocessor MCU also controls the opening of the camera I (11), the camera II (20), the camera III (26) and the camera IV (30), the camera I (11), the camera II (20), the camera III (26) and the camera IV (30) transmit data to the memory and the upper computer, and the upper computer displays pictures on a screen through the screen dividing device.
3. The fixed-wing drone aerial device of claim 2, wherein: the structure of the wireless transceiver circuit II is the same as that of the wireless transceiver circuit I, the wireless transceiver circuit II comprises a wireless transmitting module U5, the end 1 of the wireless transmitting module U5 is connected with the end 3 of the interface JI2, the end 2 of the wireless transmitting module U5 is connected with the end 4 of the interface JI2, the end 3 of the wireless transmitting module U5 is connected with the end 5 of the interface JI2, the end 4 of the wireless transmitting module U5 is connected with the end 6 of the interface JI2, the end 5 of the wireless transmitting module U5 is connected with the end 7 of the interface JI2, the end 6 of the wireless transmitting module U5 is connected with the end 8 of the interface JI2,
the No. 7 end of the wireless sending module U5 is connected with the No. 18 end of the wireless sending module U5, the No. 15 end of the wireless sending module U5, one end of a capacitor C16, one end of a capacitor C17 and a working voltage VCC, the other end of the capacitor C16 is grounded, the other end of the capacitor C17 is grounded, the No. 8 end of the wireless sending module U5 is connected with the No. 14 end of the wireless sending module U5 and then grounded, the No. 9 end of the wireless sending module U5 is connected with one end of a crystal oscillator CY4, one end of a resistor R26 and one end of a capacitor C25, the No. 10 end of the wireless sending module U5 is connected with the other end of the crystal oscillator CY4, the other end of the resistor R26 and one end of the capacitor C26, the other end of the capacitor C25 is connected with the other end of the capacitor C26 and then grounded,
the No. 11 end of the wireless transmitting module U5 is connected to one end of a capacitor C22, one end of a capacitor C23 and one end of an inductor L6, the other end of the inductor L6 is connected to one end of an inductor L5 and the No. 12 end of the wireless transmitting module U5, the No. 13 end of the wireless transmitting module U5 is connected to the other end of the inductor L5 and one end of an inductor L4, the other end of the inductor L4 is connected to one end of a capacitor C19, the other end of the capacitor C19 is connected to one end of a capacitor C20 and the No. 1 end of an interface J9, the other end of the capacitor C20 is grounded, and the No. 2 end of the interface J9 is grounded;
the No. 16 end of the wireless sending module U5 is connected with the No. 17 end of the wireless sending module U5 and the No. 20 end of the wireless sending module U5 in series through a resistor R17 and then is grounded, and the No. 19 end of the wireless sending module U5 is connected with a capacitor C15 in series and then is grounded.
4. The fixed-wing drone aerial photography device of claim 2, wherein: the No. 3 end of the microprocessor MCU is connected with the No. 1 end of the interface J1,
the No. 4 end of the microprocessor MCU is connected with the No. 2 end of the interface J1,
the No. 5 end of the microprocessor MCU is connected with the No. 3 end of the interface J1,
the No. 6 end of the microprocessor MCU is connected with the No. 4 end of the interface J1,
the No. 20 end of the microprocessor MCU is grounded,
the No. 25 end of the microprocessor MCU is connected with one end of a resistor R1, the other end of the resistor R1 is connected with a base electrode b of a triode Q4, an emitting electrode e of the triode Q4 is grounded, a collector electrode c of the triode Q4 is connected with a linear motor II (3) and then is connected with a working voltage VCC,
the number 26 end of the microprocessor MCU is connected with one end of a resistor R2, the other end of the resistor R2 is connected with a base electrode b of a triode Q3, an emitter electrode e of the triode Q3 is grounded, a collector electrode c of the triode Q3 is connected with a working voltage VCC after being connected with a linear motor I (2),
the number 27 end of the microprocessor MCU is connected with one end of a resistor R4, the other end of the resistor R4 is connected with a base electrode b of a triode Q2, an emitting electrode e of the triode Q2 is grounded, a collector electrode c of the triode Q2 is connected with a working voltage VCC after being connected with a motor II (16),
the 28 th end of the microprocessor MCU is connected with one end of a resistor R3, the other end of the resistor R3 is connected with a base b of a triode Q1, an emitter e of the triode Q1 is grounded, a collector c of the triode Q1 is connected with a working voltage VCC after being connected with a motor I (7),
the working voltage VCC end is connected with an emitter e of a triode Q5, a collector C of the triode Q5 is connected with one end of a resistor R12 and the No. 3 end of an interface J2, the other end of the resistor R12 is grounded, a base b of the triode Q5 is connected with one end of a resistor R11, the other end of the resistor R11 is connected with one end of the resistor R10, one end of a capacitor C5 and one end of a switch RSTK, the other end of the resistor R10 is grounded, and the other end of the capacitor C5 is connected with the other end of the switch RSTK and then connected with the working voltage VCC end.
5. The fixed-wing drone aerial device of claim 2, wherein: the memory circuit includes chip W1, No. 1 end connection microprocessor MCU's of chip W1 No. 40 end, No. 2 end connection microprocessor MCU's of chip W1 No. 20 end, No. 3 end connection microprocessor MCU's of chip W1 No. 8 end, chip W1 No. 4 termination ground, chip W1's No. 5 end connecting resistance R5's one end, chip W1's No. 5 end connecting resistance R6's one end, chip W1's No. 8 end connecting resistance R5's the other end, resistance R6's the other end and operating voltage VCC.
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| CN201910082551.XA CN109866935B (en) | 2019-01-28 | 2019-01-28 | Fixed wing unmanned aerial vehicle device of taking photo by plane |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002154491A (en) * | 2000-11-17 | 2002-05-28 | Jeikamu:Kk | Mounting device for video camera |
| CN103366622A (en) * | 2013-07-17 | 2013-10-23 | 石家庄学院 | Aerial photogrammetry simulation system |
| CN203512045U (en) * | 2013-04-12 | 2014-04-02 | 西北农林科技大学 | Aerial photography tripod head taking fixed wind model airplane as aerial carrier |
| CN205770195U (en) * | 2016-06-30 | 2016-12-07 | 北京嘉源东方科技发展有限公司 | A kind of special unmanned plane of taking photo by plane of wind-powered electricity generation |
| CN207301805U (en) * | 2017-10-10 | 2018-05-01 | 范斌 | A kind of big visual angle unmanned plane for taking photo by plane |
| CN109131919A (en) * | 2018-09-10 | 2019-01-04 | 济宁群艺广告传媒有限公司 | One kind for VR take photo by plane panorama self-stabilization, double synchronize seamless spliced filming apparatus |
-
2019
- 2019-01-28 CN CN201910082551.XA patent/CN109866935B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002154491A (en) * | 2000-11-17 | 2002-05-28 | Jeikamu:Kk | Mounting device for video camera |
| CN203512045U (en) * | 2013-04-12 | 2014-04-02 | 西北农林科技大学 | Aerial photography tripod head taking fixed wind model airplane as aerial carrier |
| CN103366622A (en) * | 2013-07-17 | 2013-10-23 | 石家庄学院 | Aerial photogrammetry simulation system |
| CN205770195U (en) * | 2016-06-30 | 2016-12-07 | 北京嘉源东方科技发展有限公司 | A kind of special unmanned plane of taking photo by plane of wind-powered electricity generation |
| CN207301805U (en) * | 2017-10-10 | 2018-05-01 | 范斌 | A kind of big visual angle unmanned plane for taking photo by plane |
| CN109131919A (en) * | 2018-09-10 | 2019-01-04 | 济宁群艺广告传媒有限公司 | One kind for VR take photo by plane panorama self-stabilization, double synchronize seamless spliced filming apparatus |
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