CN212047886U

CN212047886U - A microminiature unmanned aerial vehicle for low latitude remote sensing survey and drawing task

Info

Publication number: CN212047886U
Application number: CN202020370832.3U
Authority: CN
Inventors: 朱航; 张鹤涵; 陈景曦
Original assignee: Jilin University
Current assignee: Jilin University
Priority date: 2020-03-23
Filing date: 2020-03-23
Publication date: 2020-12-01
Anticipated expiration: 2030-03-23

Abstract

A microminiature unmanned aerial vehicle for low-altitude remote sensing mapping task belongs to the technical field of unmanned aerial vehicle mapping remote sensing, and the utility model comprises an automatic undercarriage retracting mechanism group, a foldable arm group, a central plate platform and a tripod head assembly, wherein two automatic undercarriage retracting mechanisms of the automatic undercarriage retracting mechanism group are fixedly connected below the central plate platform, and the two automatic undercarriage retracting mechanisms are bilaterally symmetrical; the eight foldable arms are positioned on the same horizontal plane and are respectively and fixedly connected to eight corners of the central plate platform through respective central plate connecting plates; the cradle head assembly is fixedly connected to the cradle head supporting rod right below the central plate platform through the cradle head connecting plate upper hanging rod fastening piece by the cradle head hanging rod; the utility model discloses not enough to current survey and drawing unmanned aerial vehicle, it is higher to adopt many rotor unmanned aerial vehicle to make flexibility and commonality, and the remote sensing platform of adoption makes the speed that obtains the image become fast, control cost, and the security performance is showing and is improving.

Description

A microminiature unmanned aerial vehicle for low latitude remote sensing survey and drawing task

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle survey and drawing remote sensing, concretely relates to microminiature unmanned aerial vehicle for low latitude remote sensing survey and drawing task.

Background

Compare in traditional aviation remote sensing survey and drawing platform, this small unmanned aerial vehicle obtains improving on image quality, and unmanned aerial vehicle has very high flight flexibility at the flight in-process, and the acquisition data cycle obtains shortening a large amount, obtains showing in the aspect of the working cost reducing. Therefore, in the field of surveying and mapping remote sensing of the unmanned aerial vehicle, the micro unmanned aerial vehicle has a better development prospect.

The traditional unmanned helicopter system adopts a fuel generator as a power source, has a large size and is inconvenient to work; multi-rotor drone systems are limited in their range of endurance. Compared with the traditional aerospace craft, the microminiature unmanned aerial vehicle for low-altitude remote sensing surveying and mapping has higher universality and flexibility, the speed for the unmanned aerial vehicle remote sensing platform to acquire images is higher, and the microminiature unmanned aerial vehicle has higher resolution, and in addition, the microminiature unmanned aerial vehicle also has the advantages of low cost, flexible operation and short task period, and can be widely applied to various fields of the remote sensing surveying and mapping platform.

Disclosure of Invention

An object of the utility model is to current survey and drawing remote sensing unmanned aerial vehicle not enough, provide a microminiature unmanned aerial vehicle for low latitude remote sensing survey and drawing, make it obtain higher flexibility and commonality through adopting many rotor unmanned aerial vehicle, the remote sensing platform of adoption makes the speed that obtains the image faster more, possess higher resolution ratio, and control cost and equipment loss are less, and the security performance is higher.

The utility model comprises an automatic undercarriage retracting mechanism group A, a foldable arm group B, a central panel platform C and a tripod head assembly D, wherein two automatic undercarriage retracting mechanisms of the automatic undercarriage retracting mechanism group A are fixedly connected below the central panel platform C by screws through hole groups arranged above respective retracting mechanism supports, and the two automatic undercarriage retracting mechanisms are bilaterally symmetrical; eight foldable arms of the foldable arm group B are positioned on the same horizontal plane and are respectively and fixedly connected to eight corners of a central plate platform C through respective central plate connecting plates 32; and the holder assembly D is fixedly connected to the holder support rod right below the central plate platform C through the holder hanging rod fastening piece on the upper part of the holder connecting plate.

Undercarriage automatic retraction jack group A constitute by two undercarriage automatic retraction jacks that the structure is the same completely, wherein single undercarriage automatic retraction jack comprises connecting piece 1, sleeve pipe 2, rocker 3, connecting rod 4, crank 5, steering wheel 6, carry frame 7, undercarriage seat 8, bracing piece 9, damping ball I10, connecting plate 11, supporting seat pair 12, base sleeve pipe 13, cloud platform bracing piece 14, auxiliary crank 15, carry frame connecting rod 16, base sleeve pipe damping ring 17, steering wheel mount I18, steering wheel rotating connecting piece 19, wherein: the steering engine 6 is fixedly connected with a steering engine fixing frame I18; the steering engine fixing frame I18 is fixedly connected to the left lower part of the lifting frame seat 8; the main shaft of the steering engine 6 is connected with a steering engine rotating connecting piece 19; the upper ends of the crank 5 and the auxiliary crank 15 are hinged with a steering engine rotating connecting piece 19; the lower end of the crank 5 is hinged with the upper end of the connecting rod 4 through a pin shaft; the lower end of the connecting rod 4 is hinged with the rocker 3 through a pin shaft; the upper end of the sleeve 2 is in interference connection with the inner wall of the rocker 3, and the lower end of the sleeve 2 is in interference connection with the inner wall of the connecting piece 1; the lower end of the connecting piece 1 is connected with the center of the base sleeve 13 in an interference manner; the base sleeve damping rings 17 are nested at two ends of the base sleeve 13; the hanging frame 7 is fixedly connected with a connecting plate 11 through a damping ball I10; two ends of the cradle head support rod 14 are in interference connection through a support seat pair 12 below the connecting plate 11; two landing gear automatic retraction mechanisms with the same structure are connected through a support rod 8; the hanging carrier connecting rod 16 is connected with the inner wall of the hole of the landing gear seat 8 which is symmetrical left and right in an interference way.

The foldable arm group B consists of eight foldable arms with completely identical mechanisms, wherein: a single collapsible horn comprises buckle 20, buckle connecting piece 21, carbon fiber pipe 22, collapsible wing pair 23, steering wheel mount II 24, wing clamp plate 25, motor casing 26, motor I27, motor fixed plate I28, electricity accent mounting panel 29, motor cabinet 30, screw 31, well core connection board 32, wherein: the buckle 20, the buckle connecting piece 21, the carbon fiber pipe 22, the motor base 30 and the electric regulation mounting plate 29 are sequentially arranged from inside to outside and fixedly connected, and the central plate connecting plate 32 is fixedly connected below the buckle connecting piece 21 through a screw 31; the electric regulation mounting plate 29, the motor fixing plate I28, the motor I27, the motor shell 26 and the wing pressing plate 25 are sequentially arranged and fixedly connected from bottom to top; the center of the wing pressing plate 25 is fixedly connected with the output end of the motor I27, and the left end and the right end of the wing pressing plate 25 are movably connected with the inner ends of the two foldable wings of the foldable wing pair 23 through pin shafts.

The central plate platform C consists of an upper plate 33, a support column group 34, a plate cover 35 and a lower plate 36, wherein the upper plate 33, the support column group 34 and the lower plate 36 are arranged from top to bottom, and the upper plate 33 and the lower plate 36 are fixedly connected through eight support columns of the support column group 34; the plate cover 35 is attached to the centers of eight support columns of the support column group 34 via screws.

The tripod head assembly D consists of a camera connecting plate 37, a motor pair 38, a motor gland pair 39, a pitch shaft support arm pair 40, a rolling shaft support arm 41, a motor III 42, a yaw shaft support arm 43, a damping ball II 44, a mounting rod fixing seat 45, a mounting rod fastening piece 46, a motor IV 47, a central plate 48, a tripod head connecting plate pair 49, an upper pressure plate 50, a lower pressure plate 51, a high-resolution camera shell 52, a rolling shaft connecting frame 53, a support arm connecting sleeve 54, a yaw shaft bearing inner shaft sleeve 55, a yaw motor shell 56, a rolling shaft sleeve 57 and a motor fixing plate II 58, wherein the motor IV 47 is positioned in the center of the central plate 48 and fixed in the yaw motor shell 56, and a main shaft of the motor IV 47 is in interference connection with the yaw shaft bearing inner shaft sleeve 55; the yaw motor shell 56 is connected with the upper surface of the motor IV 47 through three supporting arms arranged above the central plate; the lower end of the yaw axis bearing inner shaft sleeve 55 is fixedly connected with the supporting arm connecting sleeve 54; the yaw shaft bearing inner shaft sleeve 55 is in interference connection with a main shaft of the motor III 42; two cradle head connecting plates of the cradle head connecting plate pair 49 are respectively and fixedly connected with the left end and the right end of the central plate 48; four mounting rods of the mounting rod group E are fixedly connected to four corners of the outer ends of the two tripod head connecting plates; the hanging rod consists of a damping ball II 44, a hanging rod fixing seat 45, a hanging rod fastening piece 46, an upper pressure plate 50 and a lower pressure plate 51, the damping ball II 44 and the upper pressure plate 50 are sequentially arranged from bottom to top and fixedly connected, the hanging rod fastening piece 46 is fixedly connected to the upper end of the hanging rod fixing seat 45, and the hanging rod fixing seat 45 is fixedly connected to the outer side of the lower pressure plate 51; the upper end of the yaw axis supporting arm 43 is fixedly connected with the supporting arm connecting sleeve 54, and the lower end of the yaw axis supporting arm 43 is fixedly connected with the middle part of the rolling axis connecting frame 53; the rolling shaft supporting arm 41 is in interference connection with the inner wall of the rolling shaft connecting frame 53; the motor III 42 is fixedly connected to the motor fixing plate II 58, the main shaft of the motor III 42 is positioned at the rear side of the yaw axis supporting arm 43, and the main shaft of the motor III 42 is movably connected with the lower end hole of the yaw axis supporting arm 43 and the upper end hole of the rolling shaft connecting frame 53; the rolling shaft supporting arm 41 is in interference connection with the inner wall of the rolling shaft connecting frame 53; the left and right pitch shaft supporting arms of the pitch shaft supporting arm pair 40 are fixedly connected with the left and right pitch shaft motors of the motor pair 38 through the left and right motor glands of the motor gland pair 39 respectively; the left end of the camera connecting plate 37 is fixedly connected with the high-resolution camera shell 52, and the right end of the camera connecting plate 37 is fixedly connected with the left side of the right pitch shaft motor; the right side of the right pitching shaft motor is connected with the right motor gland; the rear ends of the left and right pitch axis support arms of the pitch axis support arm pair 40 are respectively fixed to the two ends of the roll axis support arm 41.

The utility model discloses confirm unmanned aerial vehicle's overall structure scheme, designed including foldable horn, receive and release mechanical structure such as undercarriage, made unmanned aerial vehicle's flight stability obtain showing and improve, in unmanned aerial vehicle survey and drawing remote sensing field, can combine together with techniques such as machine vision, image processing, make the acquisition process of image simpler to obtain higher-quality image data.

Drawings

FIG. 1 is a schematic structural diagram of a microminiature unmanned aerial vehicle for a low-altitude remote sensing surveying and mapping task

FIG. 2 is a front view of an automatic retraction gear set A

FIG. 3 is a side view of an automatic retraction gear set A

FIG. 4 is an enlarged view of a in FIG. 3

FIG. 5 is a schematic structural diagram of foldable arm set B

FIG. 6 is a schematic view of the structure of the center plate platform C

FIG. 7 is an isometric view of pan and tilt head assembly D

FIG. 8 is a side view of pan and tilt head assembly D

FIG. 9 is an enlarged view of b in FIG. 8

Wherein: A. automatic undercarriage retraction/extension mechanism set B, foldable jib set C, center plate platform D, pan/tilt assembly E, mounting rod set 1, connecting piece 2, sleeve 3, rocker 4, connecting rod 5, crank 6, steering engine 7, mounting frame 8, jib mount 9, supporting rod 10, damping ball I11, connecting plate 12, supporting seat 13, base sleeve 14, pan/tilt supporting rod 15, auxiliary crank 16, mounting frame connecting rod 17, base sleeve damping ring 18, steering engine mount I19, steering engine rotation connecting piece 20, buckle 21, buckle connecting piece 22, carbon fiber pipe 23, foldable wing pair 24, steering engine mount II 25, wing pressing plate 26, motor shell 27, motor I28, motor fixing plate I29, electric adjustment mounting plate 30, motor mount 31, screw 32, center plate 33, upper plate 34, supporting column set 35, plate cover 36, lower plate 37, camera connecting plate cover 36, lower plate 37 Plate 38, motor pair 39, motor gland pair 40, pitch shaft support arm pair 41, roll shaft support arm 42, motor III 43, yaw shaft support arm 44, damping ball II 45, mounting rod mount 46, mounting rod tightening piece 47, motor IV 48, center plate 49, pan head link plate pair 50, upper pressure plate 51, lower pressure plate 52, high resolution camera housing 53, roll shaft link 54, support arm link 55, yaw shaft bearing inner shaft sleeve 56, yaw motor housing 57, roll shaft sleeve 58, motor mount II shaft sleeve 58

Detailed Description

The following describes embodiments of the present invention with reference to the accompanying drawings.

As shown in fig. 1, the present invention comprises an automatic retraction jack group a of landing gear, a foldable arm group B, a central platform C, and a head assembly D, wherein two automatic retraction jacks of the automatic retraction jack group a of landing gear are fixed below the central platform C by screws through hole groups arranged above respective retraction jack supports, and the two automatic retraction jacks are bilaterally symmetrical; eight foldable arms of the foldable arm group B are positioned on the same horizontal plane and are respectively and fixedly connected to eight corners of a central plate platform C through respective central plate connecting plates 32; and the holder assembly D is fixedly connected to the holder support rod right below the central plate platform C through the holder hanging rod fastening piece on the upper part of the holder connecting plate.

The integrated spare part of unmanned aerial vehicle uses carbon fiber material, and it is big to compare in other materials and have intensity, the light advantage of quality, and this eight rotor unmanned aerial vehicle need carry on a visible light camera and two image acquisition equipment of a multispectral imager, and the volume and the quality of cloud platform are all great. Consequently, for guaranteeing unmanned aerial vehicle steady operation under great load, the structure size of unmanned aerial vehicle organism is great. The structure scheme of adopting eight rotors is under the condition of improving lift, increases the fault-tolerant rate of aircraft. The unmanned aerial vehicle horn is designed to be a foldable horn, so that the occupied time in the conveying process is reduced, and convenient conditions are provided for the unmanned aerial vehicle to carry out tasks in the field.

As shown in fig. 2 to 4, the automatic retraction jack group a of the undercarriage is composed of two automatic retraction jacks with the same structure, wherein a single automatic retraction jack of the undercarriage is composed of a connecting piece 1, a sleeve 2, a rocker 3, a connecting rod 4, a crank 5, a steering engine 6, a mounting rack 7, a landing rack seat 8, a supporting rod 9, a damping ball i 10, a connecting plate 11, a supporting seat pair 12, a base sleeve 13, a tripod head supporting rod 14, an auxiliary crank 15, a mounting rack connecting rod 16, a base sleeve damping ring 17, a steering engine fixing rack i 18 and a steering engine rotating connecting piece 19, wherein: the steering engine 6 is fixedly connected with a steering engine fixing frame I18; the steering engine fixing frame I18 is fixedly connected to the left lower part of the lifting frame seat 8; the main shaft of the steering engine 6 is connected with a steering engine rotating connecting piece 19; the upper ends of the crank 5 and the auxiliary crank 15 are hinged with a steering engine rotating connecting piece 19; the lower end of the crank 5 is hinged with the upper end of the connecting rod 4 through a pin shaft; the lower end of the connecting rod 4 is hinged with the rocker 3 through a pin shaft; the upper end of the sleeve 2 is in interference connection with the inner wall of the rocker 3, and the lower end of the sleeve 2 is in interference connection with the inner wall of the connecting piece 1; the lower end of the connecting piece 1 is connected with the center of the base sleeve 13 in an interference manner; the base sleeve damping rings 17 are nested at two ends of the base sleeve 13; the hanging frame 7 is fixedly connected with a connecting plate 11 through a damping ball I10; two ends of the cradle head support rod 14 are in interference connection through a support seat pair 12 below the connecting plate 11; two landing gear automatic retraction mechanisms with the same structure are connected through a support rod 8; the hanging carrier connecting rod 16 is connected with the inner wall of the hole of the landing gear seat 8 which is symmetrical left and right in an interference way.

The undercarriage is unmanned aerial vehicle's support part, keeps the fuselage level when unmanned aerial vehicle takes off and descends, avoids horn or screw and ground to bump, can absorb and consume partial impact energy when landing simultaneously, guarantees the safety of unmanned aerial vehicle organism and platform. When the unmanned aerial vehicle takes off, the unmanned aerial vehicle carrying out the remote sensing mapping task needs to carry out image acquisition through the camera on the cloud platform, so the undercarriage if fixed can influence the image acquisition scope of camera. Therefore, by adopting the automatic retraction jack of the undercarriage, the yaw angle of the hovering unmanned aerial vehicle is not required to be adjusted, so that all image acquisition can be realized, and the control of the unmanned aerial vehicle platform in the remote sensing surveying and mapping task is simplified. The landing gear device can be simplified into a crank and rocker mechanism, a crank is a driving part, a steering engine provides power for the crank, and a rocker is a driven part and does reciprocating swing, namely the retraction and release movement of the landing gear. When unmanned aerial vehicle descends, the undercarriage is transferred, and the landing moment can receive the impact on ground, can apply a moment opposite with the motion to the follower rocker, causes the impact to the steering wheel, produces the harm. At the moment, the rocker can be regarded as a driving piece, when the rocker in the crank rocker mechanism is taken as the driving piece, a dead point position exists, the dead point position can generate a phenomenon of 'top dead', and the rotating moment of the crank is zero. The event can utilize this position to reduce the harm to the steering wheel to can guarantee that the undercarriage can not pack up because of the impact, thereby guaranteed carry cloud platform and unmanned aerial vehicle's security.

As shown in fig. 5, the foldable horn group B is composed of eight foldable horns with identical mechanisms, wherein: a single collapsible horn comprises buckle 20, buckle connecting piece 21, carbon fiber pipe 22, collapsible wing pair 23, steering wheel mount II 24, wing clamp plate 25, motor casing 26, motor I27, motor fixed plate I28, electricity accent mounting panel 29, motor cabinet 30, screw 31, well core connection board 32, wherein: the buckle 20, the buckle connecting piece 21, the carbon fiber pipe 22, the motor base 30 and the electric regulation mounting plate 29 are sequentially arranged from inside to outside and fixedly connected, and the central plate connecting plate 32 is fixedly connected below the buckle connecting piece 21 through a screw 31; the electric regulation mounting plate 29, the motor fixing plate I28, the motor I27, the motor shell 26 and the wing pressing plate 25 are sequentially arranged and fixedly connected from bottom to top; the center of the wing pressing plate 25 is fixedly connected with the output end of the motor I27, and the left end and the right end of the wing pressing plate 25 are movably connected with the inner ends of the two foldable wings of the foldable wing pair 23 through pin shafts.

This eight rotor unmanned aerial vehicle total eight horn, all have a brushless DC motor, one electricity on every horn to transfer, a pair of screw, the electricity is transferred and is installed in the chip inslot of brushless DC motor below, and the motor passes through the fixed plate and is connected with the motor cabinet. The folding mechanism of the horn realizes folding and stretching through a central platform and a buckle device fixed on a carbon fiber tube of the horn. The machine arm is lifted to be in contact with the central platform, the buckling device is rotated, the machine arm is locked, and the machine arm is stretched to enter a working state. When the horn is folded, the buckle that will lock is unscrewed, and the horn relies on self weight whereabouts, gets into fold condition.

As shown in fig. 6, the central plate platform C is composed of an upper plate 33, a support column group 34, a plate cover 35 and a lower plate 36, the upper plate 33, the support column group 34 and the lower plate 36 are arranged from top to bottom, and the upper plate 33 and the lower plate 36 are fixedly connected through eight support columns of the support column group 34; the plate cover 35 is attached to the centers of eight support columns of the support column group 34 via screws.

The central board platform is connected with each part of the unmanned aerial vehicle, and meanwhile, the central board platform can also carry part of sensors, and a power supply board is arranged on the platform to provide electric power for each flight motor. The size of the central board platform meets the requirement that a proper mounting space is arranged below the machine body, and the central board platform cannot interfere with a three-axis pan-tilt head below after the machine arm is folded.

As shown in fig. 7 to 9, the pan-tilt assembly D is composed of a camera connecting plate 37, a motor pair 38, a motor gland pair 39, a pitch shaft supporting arm pair 40, a roll shaft supporting arm 41, a motor iii 42, a yaw shaft supporting arm 43, a damping ball ii 44, a mounting rod fixing seat 45, a mounting rod fastening piece 46, a motor iv 47, a central plate 48, a pan-tilt connecting plate pair 49, an upper pressing plate 50, a lower pressing plate 51, a high resolution camera shell 52, a roll shaft connecting frame 53, a supporting arm connecting sleeve 54, a yaw shaft bearing inner sleeve 55, a yaw motor shell 56, a roll shaft sleeve 57 and a motor fixing plate ii 58, wherein the motor iv 47 is located at the center of the central plate 48 and fixed in the yaw motor shell 56, and a main shaft of the motor iv 47 is in interference connection with the yaw shaft bearing inner sleeve 55; the yaw motor shell 56 is connected with the upper surface of the motor IV 47 through three supporting arms arranged above the central plate; the lower end of the yaw axis bearing inner shaft sleeve 55 is fixedly connected with the supporting arm connecting sleeve 54; the yaw shaft bearing inner shaft sleeve 55 is in interference connection with a main shaft of the motor III 42; two cradle head connecting plates of the cradle head connecting plate pair 49 are respectively and fixedly connected with the left end and the right end of the central plate 48; four mounting rods of the mounting rod group E are fixedly connected to four corners of the outer ends of the two tripod head connecting plates; the hanging rod consists of a damping ball II 44, a hanging rod fixing seat 45, a hanging rod fastening piece 46, an upper pressure plate 50 and a lower pressure plate 51, the damping ball II 44 and the upper pressure plate 50 are sequentially arranged from bottom to top and fixedly connected, the hanging rod fastening piece 46 is fixedly connected to the upper end of the hanging rod fixing seat 45, and the hanging rod fixing seat 45 is fixedly connected to the outer side of the lower pressure plate 51; the upper end of the yaw axis supporting arm 43 is fixedly connected with the supporting arm connecting sleeve 54, and the lower end of the yaw axis supporting arm 43 is fixedly connected with the middle part of the rolling axis connecting frame 53; the rolling shaft supporting arm 41 is in interference connection with the inner wall of the rolling shaft connecting frame 53; the motor III 42 is fixedly connected to the motor fixing plate II 58, the main shaft of the motor III 42 is positioned at the rear side of the yaw axis supporting arm 43, and the main shaft of the motor III 42 is movably connected with the lower end hole of the yaw axis supporting arm 43 and the upper end hole of the rolling shaft connecting frame 53; the rolling shaft supporting arm 41 is in interference connection with the inner wall of the rolling shaft connecting frame 53; the left and right pitch shaft supporting arms of the pitch shaft supporting arm pair 40 are fixedly connected with the left and right pitch shaft motors of the motor pair 38 through the left and right motor glands of the motor gland pair 39 respectively; the left end of the camera connecting plate 37 is fixedly connected with the high-resolution camera shell 52, and the right end of the camera connecting plate 37 is fixedly connected with the left side of the right pitch shaft motor; the right side of the right pitching shaft motor is connected with the right motor gland; the rear ends of the left and right pitch axis support arms of the pitch axis support arm pair 40 are respectively fixed to the two ends of the roll axis support arm 41.

The remote sensing survey and drawing unmanned aerial vehicle cloud platform needs to carry on image acquisition equipment to need to keep the stability of cloud platform in the image acquisition in-process. This unmanned aerial vehicle adopts the triaxial to stabilize the cloud platform certainly, through the position gesture of control motor real-time adjustment cloud platform, reaches the purpose that obtains high quality image information, compares in the angle modulation that the diaxon cloud platform has increased the driftage axle. The image acquisition work under the unmanned aerial vehicle state of hovering can be realized.

The overall structure of the holder adopts a three-axis-three-frame structure, and comprises a yaw axis control motor, a yaw axis frame, a transverse roller frame, a pitch axis motor for finally independently controlling two cameras and a camera mounting frame. The control motor selects an outer rotor type brushless DC motor, and transmits power to each frame through a motor shaft. And stable control of the holder is realized.

Claims

1. A microminiature unmanned aerial vehicle for low-altitude remote sensing surveying and mapping tasks comprises an automatic undercarriage retracting and releasing mechanism group (A), a foldable arm group (B), a central plate platform (C) and a tripod head assembly (D), wherein two automatic undercarriage retracting and releasing mechanisms of the automatic undercarriage retracting and releasing mechanism group (A) are fixedly connected below the central plate platform (C) through hole groups arranged above respective retracting and releasing mechanism supports by screws, and the two automatic undercarriage retracting and releasing mechanisms are bilaterally symmetrical; eight foldable arms of the foldable arm group (B) are positioned on the same horizontal plane and are respectively and fixedly connected to eight corners of the central plate platform (C) through respective central plate connecting plates (32); the holder assembly (D) is fixedly connected to a holder support rod right below the central plate platform (C) through a holder mounting rod fastening piece at the upper part of the holder connecting plate; the central plate platform (C) consists of an upper plate (33), a support column group (34), a plate cover (35) and a lower plate (36), wherein the upper plate (33), the support column group (34) and the lower plate (36) are arranged from top to bottom, and the upper plate (33) is fixedly connected with the lower plate (36) through eight support columns of the support column group (34); the board lid (35) is connected in eight support column centers of support column group (34) through the screw, its characterized in that: undercarriage automatic retraction jack group (A) constitute by two undercarriage automatic retraction jack that the structure is the same completely, wherein single undercarriage automatic retraction jack comprises connecting piece (1), sleeve pipe (2), rocker (3), connecting rod (4), crank (5), steering wheel (6), string carrier (7), landing gear seat (8), bracing piece (9), damping ball I (10), connecting plate (11), the supporting seat is to (12), base sleeve pipe (13), cloud platform bracing piece (14), auxiliary crank (15), string carrier connecting rod (16), base sleeve pipe damping ring (17), steering wheel mount I (18), steering wheel rotation connecting piece (19) are constituteed, wherein: the steering engine (6) is fixedly connected with a steering engine fixing frame I (18); the steering engine fixing frame I (18) is fixedly connected to the left lower part of the lifting frame seat (8); the main shaft of the steering engine (6) is connected with a steering engine rotating connecting piece (19); the upper ends of the crank (5) and the auxiliary crank (15) are hinged with a steering engine rotating connecting piece (19); the lower end of the crank (5) is hinged with the upper end of the connecting rod (4) through a pin shaft; the lower end of the connecting rod (4) is hinged with the rocker (3) through a pin shaft; the upper end of the sleeve (2) is in interference connection with the inner wall of the rocker (3), and the lower end of the sleeve (2) is in interference connection with the inner wall of the connecting piece (1); the lower end of the connecting piece (1) is in interference connection with the center of the base sleeve (13); the base sleeve damping rings (17) are nested at two ends of the base sleeve (13); the hanging frame (7) is fixedly connected with a connecting plate (11) through a damping ball I (10); two ends of the cradle head support rod (14) are in interference connection with the support seat pair (12) below the connecting plate (11); two landing gear automatic retraction mechanisms with the same structure are connected through a support rod (9); the hanging rack connecting rod (16) is connected with the inner wall of the hole of the landing gear seat (8) which is symmetrical left and right in an interference way.

2. A micro unmanned aerial vehicle for low altitude remote sensing mapping mission as claimed in claim 1, wherein: the foldable arm group (B) consists of eight foldable arms with completely identical mechanisms, wherein: a single collapsible horn comprises buckle (20), buckle connecting piece (21), carbon fiber pipe (22), collapsible wing pair (23), steering wheel mount II (24), wing clamp plate (25), motor casing (26), motor I (27), motor fixed plate I (28), electricity accent mounting panel (29), motor cabinet (30), screw (31), well core connection board (32), wherein: the clamp buckle (20), the clamp buckle connecting piece (21), the carbon fiber pipe (22), the motor base (30) and the electric regulation mounting plate (29) are sequentially arranged from inside to outside and fixedly connected, and the central plate connecting plate (32) is fixedly connected below the clamp buckle connecting piece (21) through a screw (31); the electric regulation mounting plate (29), the motor fixing plate I (28), the motor I (27), the motor shell (26) and the wing pressing plate (25) are sequentially arranged from bottom to top and fixedly connected; the center of the wing pressing plate (25) is fixedly connected with the output end of the motor I (27), and the left end and the right end of the wing pressing plate (25) are movably connected with the inner ends of two foldable wings of the foldable wing pair (23) through pin shafts.

3. A micro unmanned aerial vehicle for low altitude remote sensing mapping mission as claimed in claim 1, wherein: the cradle head assembly (D) consists of a camera connecting plate (37), a motor pair (38), a motor gland pair (39), a pitching shaft supporting arm pair (40), a rolling shaft supporting arm (41), a motor III (42), a yawing shaft supporting arm (43), a damping ball II (44), a mounting rod fixing seat (45), a mounting rod fastening piece (46), a motor IV (47), a central plate (48), a cradle head connecting plate pair (49), an upper pressing plate (50), a lower pressing plate (51), a high-resolution camera shell (52), a rolling shaft connecting frame (53), a supporting arm connecting sleeve (54), a yawing shaft bearing inner shaft sleeve (55), a yawing motor shell (56), a rolling shaft sleeve (57) and a motor fixing plate II (58), the motor IV (47) is positioned in the center of the center plate (48) and is fixed in the yaw motor shell (56), and a main shaft of the motor IV (47) is in interference connection with an inner shaft sleeve (55) of a yaw shaft bearing; the yaw motor shell (56) is connected with the upper surface of a motor IV (47) through three supporting arms arranged above the central plate; the lower end of the yaw axis bearing inner shaft sleeve (55) is fixedly connected with a supporting arm connecting sleeve (54); the yaw shaft bearing inner shaft sleeve (55) is in interference connection with a main shaft of the motor III (42); two cradle head connecting plates of the cradle head connecting plate pair (49) are respectively and fixedly connected with the left end and the right end of the central plate (48); four mounting rods of the mounting rod group (E) are fixedly connected to four corners of the outer ends of the two holder connecting plates; the hanging rod consists of a damping ball II (44), a hanging rod fixing seat (45), a hanging rod fastening piece (46), an upper pressure plate (50) and a lower pressure plate (51), wherein the lower pressure plate (51), the damping ball II (44) and the upper pressure plate (50) are sequentially arranged and fixedly connected from bottom to top, the hanging rod fastening piece (46) is fixedly connected to the upper end of the hanging rod fixing seat (45), and the hanging rod fixing seat (45) is fixedly connected to the outer side of the lower pressure plate (51); the upper end of the yaw axis supporting arm (43) is fixedly connected with the supporting arm connecting sleeve (54), and the lower end of the yaw axis supporting arm (43) is fixedly connected with the middle part of the roll axis connecting frame (53); the rolling shaft supporting arm (41) is in interference connection with the inner wall of the rolling shaft connecting frame (53); the motor III (42) is fixedly connected to the motor fixing plate II (58), the main shaft of the motor III (42) is positioned at the rear side of the yaw axis supporting arm (43), and the main shaft of the motor III (42) is movably connected with the lower end hole of the yaw axis supporting arm (43) and the upper end hole of the rolling axis connecting frame (53); the rolling shaft supporting arm (41) is in interference connection with the inner wall of the rolling shaft connecting frame (53); the left and right pitching shaft supporting arms of the pitching shaft supporting arm pair (40) are respectively fixedly connected with the left and right pitching shaft motors of the motor pair (38) through the left and right motor glands of the motor gland pair (39); the left end of the camera connecting plate (37) is fixedly connected with the high-resolution camera shell (52), and the right end of the camera connecting plate (37) is fixedly connected with the left side of the right pitching shaft motor; the right side of the right pitching shaft motor is connected with the right motor gland; the rear ends of the left and right pitch axis supporting arms of the pitch axis supporting arm pair (40) are respectively and fixedly connected with the two ends of the rolling axis supporting arm (41).