WO2019128421A1 - Unmanned aerial vehicle tracking antenna, remote control kit and unmanned aerial vehicle kit - Google Patents
Unmanned aerial vehicle tracking antenna, remote control kit and unmanned aerial vehicle kit Download PDFInfo
- Publication number
- WO2019128421A1 WO2019128421A1 PCT/CN2018/111724 CN2018111724W WO2019128421A1 WO 2019128421 A1 WO2019128421 A1 WO 2019128421A1 CN 2018111724 W CN2018111724 W CN 2018111724W WO 2019128421 A1 WO2019128421 A1 WO 2019128421A1
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- Prior art keywords
- antenna
- unmanned aerial
- aerial vehicle
- housing
- tracking antenna
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D3/00—Control of position or direction
- G05D3/12—Control of position or direction using feedback
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- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/285—Aircraft wire antennas
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
- H01Q3/08—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
- H01Q3/10—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation to produce a conical or spiral scan
Definitions
- the present invention relates to the field of unmanned aerial vehicles, and more particularly to an unmanned aerial vehicle tracking antenna, a remote control kit, and an unmanned aerial vehicle kit.
- UAV remote control usually uses an omnidirectional antenna. Due to the low radiation gain of the omnidirectional antenna, the communication distance is limited (generally less than 10 km), when the UAV flight distance reaches tens of kilometers or even hundreds of kilometers. The omnidirectional antenna can not fully meet the requirements, greatly reducing the user experience of using the UAV remote control to control the unmanned aerial vehicle. Therefore, it is necessary to provide a remote control antenna having a long communication distance.
- the purpose of embodiments of the present invention is to provide an unmanned aerial vehicle tracking antenna, a remote control kit, and an unmanned aerial vehicle kit to solve the technical problem that the remote control antenna of the existing unmanned aerial vehicle has a short communication distance.
- An unmanned aerial vehicle tracking antenna comprising:
- An antenna assembly configured to receive position information of the unmanned aerial vehicle, including an antenna module and a support connected to the antenna module;
- the antenna assembly is mounted to the main body portion through the support, and is configured to drive the antenna assembly to rotate according to the position information of the unmanned aerial vehicle received by the antenna assembly, so that the The maximum radiation direction of the antenna assembly is directed to the unmanned aerial vehicle.
- the main body portion includes:
- a second drive assembly disposed in the housing and coupled to the mount, the second drive assembly for driving the antenna assembly to rotate about a second axis of rotation;
- a first driving component at least partially disposed in the housing, the first driving component for driving the housing, the antenna assembly and the second driving component to rotate about a first rotation axis;
- the first axis of rotation is perpendicular to the second axis of rotation.
- the first driving component comprises:
- a turntable mounted on the connecting shaft, rotatable relative to the base about the first axis of rotation;
- the gear mechanism includes a first gear sleeved on the rotating shaft and a second gear sleeved on the connecting shaft, and the first gear meshes with the second gear.
- the base is located outside of the housing.
- the turntable is disposed in the housing.
- the first gear and the second gear are both spur gears;
- the first gear and the second gear are both helical gears.
- the first driving assembly further includes a bearing, the bearing is sleeved on the connecting shaft, and the turntable is fixedly mounted between the two bearings.
- the first motor is a brushless DC gear motor.
- the second driving component comprises:
- a motor mount coupled to the axle arm
- a central axis of the rotating shaft of the second motor coincides with the second axis of rotation, and a rotating shaft of the second motor is coupled to the holder for driving the antenna assembly to rotate about the second axis of rotation.
- the support comprises a first support and a second support spaced apart from the first support;
- the second driving assembly further includes an angle sensor mounted on the second branch, the angle sensor is configured to sense a rotating shaft of the second motor The angle of rotation.
- the second drive assembly further includes a mounting rod extending from the second mount to the second motor, the angle sensor being mounted to one end of the mounting rod.
- the second motor is a brushless DC gear motor.
- the UAV tracking antenna further includes a main board disposed in the housing, a battery assembly for supplying power to the main board, and a graphic transmission module electrically connected to the main board;
- the antenna assembly, the first driving component, and the second driving component are all electrically connected to the motherboard.
- the UAV tracking antenna further includes a slip ring disposed in the housing, the slip ring includes:
- stator portion mounted to the turntable
- a rotor portion sleeved in the connecting shaft and housed in the stator portion, the rotor portion being rotatable relative to the stator portion;
- the housing includes a first housing portion, a second housing portion and a third housing portion, the first housing portion, the second housing portion, and the The third housing portions are fastened to each other.
- the housing is an integrally formed housing.
- the first housing portion includes a first side wall and a second side wall, and the two second side walls are connected to each other in parallel with each other on opposite sides of the first side wall ;
- the second housing portion includes a bottom wall and a third side wall, the bottom wall is connected to the third side wall, and the first side wall and the two second side walls are respectively mounted on the bottom wall
- the two sides of the third side wall are respectively connected to the two second side walls, the third side wall is provided with a notch, and opposite sides of the third side wall extend out of the mounting frame;
- the third housing includes a top wall, an insertion wall and a connecting wall, the top wall is mounted to the mounting frame, the embedded wall is embedded in the notch, the connecting wall is connected to the top wall and the embedded Between the walls.
- the mounting frame includes three mounting strips, and the three mounting strips are respectively mounted on the first sidewall and the two sidewalls;
- the top wall is mounted to three mounting strips of the mounting frame.
- the connecting wall includes a cylindrical cavity that receives the second drive assembly.
- the antenna module is a vertically polarized planar antenna module.
- the present invention also provides a remote controller kit including a remote controller and an unmanned aerial vehicle tracking antenna as described above, the remote controller and the unmanned aerial vehicle tracking antenna communication connection.
- the present invention also provides an unmanned aerial vehicle kit comprising an unmanned aerial vehicle and a remote control kit as described above, the remote controller being capable of tracking an antenna and the unmanned aerial vehicle through the unmanned aerial vehicle Communication connection.
- the main body portion can drive the antenna assembly to rotate such that a maximum radiation direction of the antenna assembly is directed to an unmanned aerial vehicle, so that the The unmanned aerial vehicle can obtain a better remote control signal from the antenna assembly, thereby achieving the purpose of remotely controlling the unmanned aerial vehicle.
- FIG. 1 is a perspective view of an unmanned aerial vehicle tracking antenna according to an embodiment of the present invention
- Figure 2 is a perspective view of another angle of the UAV tracking antenna shown in Figure 1;
- Figure 3 is an exploded view of the UAV tracking antenna shown in Figure 1;
- FIG. 4 is an exploded view of another angle of the UAV tracking antenna shown in FIG. 1;
- Figure 5 is an assembled view of the first drive assembly and the second drive assembly of the UAV tracking antenna of Figure 1;
- FIG. 6 is an assembled view of another angle of the first drive component and the second drive component in the UAV tracking antenna shown in FIG. 1;
- Figure 7 is an assembled view of the first drive assembly, the base and the slip ring in the assembled view shown in Figure 6;
- FIG. 8 is a perspective view of a slip ring in the UAV tracking antenna shown in FIG. 1.
- an unmanned aerial vehicle tracking antenna 100 includes a main body portion 10 and an antenna assembly 20 .
- the antenna assembly 20 is mounted on the main body portion 10 for receiving unmanned aerial vehicle position information, and the main body portion 10 is configured to acquire the unmanned aerial vehicle position information received by the antenna assembly 20, and according to the The human aircraft position information adjusts the antenna assembly 20 such that the maximum radiation direction of the antenna assembly 20 is directed toward the UAV to enable the UAV to obtain a preferred remote control signal from the antenna assembly 20.
- the antenna assembly 20 includes an antenna module 202 and a support disposed on the back of the antenna module 202 and connected to the antenna module 202 .
- the antenna module 202 is a vertically polarized planar antenna module for communicating with the unmanned aerial vehicle, including receiving the unmanned aerial vehicle position information, transmitting a remote control signal sent by the remote controller, and the like.
- the antenna module 202 uses a planar antenna to achieve directional transmission and reception signals, and the signal is stronger than the omnidirectional antenna.
- the support includes a first abutment 204 and a second abutment 206 disposed opposite the first abutment 204.
- the first support 204 and the second support 206 are respectively fixedly mounted on the antenna module 202, and the first support 204 and the second support 206 respectively hinge the main body 10.
- the antenna module 202 can also be other types of antenna modules, such as a horizontally polarized planar antenna module, as long as it can better cooperate with the antenna on the unmanned aerial vehicle. Yes, there are no strict restrictions here.
- the main body portion 10 includes a housing, a first driving component 12 disposed at least partially in the housing, and a second driving component 13 disposed in the housing.
- the antenna assembly 20, the first drive assembly 12, the second drive assembly 13, and the slip ring 18 are all electrically connected to the main board 15.
- the housing is generally rectangular parallelepiped and may be fabricated from a plastic material, the housing including a first housing portion 190, a second housing portion 192 and a third housing portion 194.
- the first case portion 190, the second case portion 192, and the third case portion 194 are engaged with each other to form a housing space.
- the housing may also be an integrally formed housing.
- the first housing portion 190 includes a first sidewall 1902 and a second sidewall 1904.
- the two second sidewalls 1904 are connected to opposite sides of the first sidewall 1902 in parallel with each other.
- the first sidewall 1902 is provided with a wire through hole 1906.
- the second housing portion 192 includes a bottom wall 1922 and a third side wall 1924.
- the bottom wall 1922 is connected to the third side wall 1924.
- the first side wall 1902 and the two second side walls 1904 are respectively mounted on the bottom wall 1922.
- the bottom wall 1922 is provided with a base through hole. 1926.
- Two opposite sidewalls 1904 are respectively connected to opposite sides of the third sidewall 1924, the third sidewall 1924 faces the first sidewall 1902, and the third sidewall 1924 and the The first side walls 1902 are parallel to each other.
- the third side wall 1924 is provided with a notch 1928, and the opposite sides of the third side wall 1924 extend out of the mounting frame 1927.
- the mounting frame 1927 includes three mounting strips, and the three mounting strips are connected to each other. Installed on the first sidewall 1902 and the two second sidewalls 1904, respectively.
- the third housing 194 includes a top wall 1942 that is embedded in the wall 1944 and the connecting wall 1946.
- the top wall 1942 is mounted to the three mounting strips of the mounting frame 1927.
- the embedded wall 1944 is embedded in the notch 1928.
- the connecting wall 1946 is coupled between the top wall 1942 and the embedded wall 1944, and the connecting wall 1946 includes a cylindrical cavity for receiving the second drive assembly 13.
- Two mounting holes 1948 are respectively disposed on opposite sides of the connecting wall 1946.
- the first housing portion 190, the second housing portion 192 and the third housing portion 194 are fastened to each other to form the housing, and the turntable 11 and the first driving assembly 12 can be conveniently arranged.
- the second drive assembly 13, the base 14, the main board 15, the battery assembly 16, the image transfer module 17 and the slip ring 18 are mounted in the housing.
- the first drive unit 12 includes a base 14 having a connecting shaft 123, a turntable 11 mounted to the connecting shaft 123, a first motor 120 mounted to the turntable 11, and a gear mechanism.
- the base 14 is located outside the housing, and the turntable 11 is disposed inside the housing. In other possible embodiments, the base 14 can also be disposed inside the housing.
- the turntable 11 is fixedly mounted in the casing, and the turntable 11 supports the first driving component 12, the second driving component 13, the image transmitting module 17, the slip ring 18, the main board 15 and the Battery assembly 16.
- the turntable 11 can be made of a material that is light in weight and suitable in strength, such as an aluminum alloy, a magnesium alloy or a plastic material.
- the first motor 120 is configured to drive the turntable 11, the first driving component 12, the second driving component 13, the circuit board 15, the battery component 16.
- the image transmission module 17 and the outer casing are rotated about the base 14 to rotate the antenna assembly 20 about the first axis of rotation O1.
- the first motor 120 is fixedly mounted on the turntable 12, and the rotating shaft 121 extends through the turntable 11.
- the first motor 120 can be a brushless DC geared motor and is a large reduction ratio motor, thereby providing a large torque.
- the rotating shaft 121 passes through the turntable 12, and the rotating shaft 121 is coupled to the rotating shaft of the first motor 120 through a coupling.
- the central axis of the rotating shaft 121 coincides with the central axis of the rotating shaft of the first motor 120.
- the gear mechanism includes a first gear 122 sleeved on the rotating shaft 121 and a second gear 125 sleeved on the connecting shaft 123.
- the second gear 125 meshes with the first gear 122.
- the first gear 122 and the second gear 125 are both spur gears.
- the first gear 122 and the second gear 125 may also be helical gears.
- One end of the connecting shaft 123 is fixedly connected to the base 14 , and the other end is connected to the slip ring 18 .
- the rotating shaft 121 is disposed in parallel with the connecting shaft 123.
- the central axis of the connecting shaft 123 coincides with the first rotational axis O1.
- the first driving assembly 12 may further include a bearing 124.
- the bearing 124 is sleeved on the connecting shaft 123.
- the turntable 11 is sleeved on the connecting shaft 123 and fixedly mounted between the two bearings 124.
- the turntable 11 and the bearing 124 are rotatable together with respect to the connecting shaft 123 about the first rotation axis O1.
- the first motor 120 When the first motor 120 is in operation, the first motor 120 provides rotational power to the rotating shaft 121 and the first gear 122.
- the connecting shaft 123 and the second gear 125 Holding the first motor 120, the first motor 120 drives the turntable 11, the bearing 124, the rotating shaft 121 and the first gear 122 together around the first rotation axis O1 and the second The gear 125 rotates.
- the rotating shaft 121 and the connecting shaft 123 can also be driven by a belt, or other suitable transmission manner or the like.
- the second driving component 13 is coupled to the support of the antenna assembly 20 for driving the antenna assembly 20 to rotate about a second axis of rotation O2, the second axis of rotation O2 being perpendicular to the first axis of rotation O1 .
- the second drive assembly 13 includes a second motor 130, a motor mount 131, an angle sensor 133, and a shaft arm 134.
- the second motor 130 may be a brushless DC gear motor, which is a large reduction ratio motor, thereby providing a large torque.
- the motor base 131 is a rectangular parallelepiped frame structure, which is advantageous for reducing weight.
- the second motor 130 is mounted to the motor base 131 via a bearing, and the rotating shaft of the second motor 130 sequentially passes through the bearing and the mounting hole 1948 of the third housing 194 to connect the first bearing 204.
- the angle sensor 133 is fixedly mounted to the second holder 206 by a mounting rod 1330 for sensing the rotation angle of the rotating shaft of the second motor 130. In other possible embodiments, the angle sensor 133 can also be mounted directly on the second mount 206.
- the shaft arm 134 is substantially in the shape of a rod, and one end thereof extends perpendicularly from the turntable 11 in a direction away from the turntable 11 and is fixedly connected to the turntable 11 and the other end is mounted to the motor base 131.
- the turntable 11 rotates relative to the connecting shaft 123 about the first rotation axis O1
- the turntable 11 drives the second driving component 13 to rotate about the first rotation axis O1 through the shaft arm 134.
- the antenna assembly 20 is also rotated about the first axis of rotation O1.
- the rotating shaft of the second motor 130 drives the first pedestal 204 to rotate, thereby rotating the antenna assembly 20 about the second rotation axis O2.
- the base 14 is fixedly mounted on one end of the connecting shaft 123 and received in the base through hole 1926.
- the base 14 is rotatable relative to the outer casing.
- the base 14 is provided with a threaded interface 140 (see FIG. 4) for attaching a tripod, such as a camera tripod, such that the UAV tracking antenna 100 can be mounted to a tripod.
- the threaded interface 140 can be a 1/4 inch camera tripod universal threaded interface.
- the main board 15 is electrically connected to the antenna assembly 20, the first driving unit 12 and the second driving unit 13.
- the main board 15 is mounted with electronic components such as a main controller and a memory, and the main board 15 is configured to receive the unmanned aerial vehicle position information from the antenna assembly 20, and analyze the unmanned aerial vehicle position information to obtain the The position of the unmanned aerial vehicle, including longitude, latitude and altitude, combined with the flight direction command issued by the remote controller, calculates the exact position of the unmanned aerial vehicle, and controls the accurate position of the unmanned aerial vehicle according to the calculation
- a drive assembly 12 and the second drive assembly 13 operate to adjust the maximum radiation direction of the antenna assembly 20 toward the UAV.
- the main board 15 is mounted to the battery assembly 16.
- the main board 15 can be installed at any position within the housing according to actual needs.
- the battery pack 16 includes a battery compartment 160 and a battery 162, and the battery compartment 160 is fixedly mounted to the turntable 11 by a bracket, and the main board 15 is mounted to the battery compartment 160.
- the battery 160 is mounted in the battery compartment 160 for supplying power to the main board 15, the first motor 120, the second motor 130, and the antenna module 202.
- the image transmission module 17 and the radio frequency module are mounted on a mounting plate, and the mounting plate is screwed to the axle arm 134, and the image transmission module 17 is configured to receive an image transmitted by the UAV.
- the slip ring 18 includes a stator portion 180, a rotor portion 182 and a wire 184.
- the stator portion 180 is sleeved outside the rotor portion 182, and the rotor portion 182 is fixedly connected.
- the connecting shaft 123 is fixedly connected to the bearing portion 124 such that the stator portion 180 is fixedly mounted to the turntable 11.
- the wire 184 extends through the rotor portion 182, and the wire 184 includes a radio frequency line and a signal line.
- One end of the wire 184 is electrically connected to the main board 15, and the stator portion 180 can rotate indefinitely with respect to the turntable 11 and the bearing 124 with respect to the rotor portion 182, and the radio frequency line and signal of the wire 184 After the wire runs through the connecting shaft 123, the RF cable interface, the earphone hole and the USB port are connected through the base 14 to realize wired communication with the remote controller.
- the UAV tracking antenna 100 is mounted to a tripod, the first axis of rotation O1 being vertically disposed, and the second axis of rotation O2 being horizontally disposed.
- the UAV acquires coordinates (including longitude and latitude) of the UAV through its positioning module (for example, a Beidou positioning module), and acquires the height of the UAV through its barometer to determine the UAV Adjusting the relative position of the antenna 100 with the UAV tracking antenna, adjusting the horizontal angle of the antenna assembly 20 by controlling the first driving component 12, and adjusting the antenna assembly 20 by controlling the second driving component 13
- the pitch angle causes the maximum radiation direction of the antenna module 202 to track the unmanned aerial vehicle in real time.
- the remote controller connects the UAV tracking antenna 100 through a signal line, and sends a remote command to the UAV through the antenna module 202, thereby achieving the purpose of remotely controlling the UAV.
- the adjustment range of the UAV tracking antenna 100 is: an infinite rotation around the first rotation axis O1, that is, no rotation angle limitation, and a rotation angle around the second rotation axis O2 is -25 to 90 degrees.
- the angle of the antenna assembly 20 can be adjusted in a wide range by the first driving component 12 and the second driving component 13 so that the maximum radiation direction of the antenna component 20 is directed to the unmanned The aircraft, it can be understood that in some other implementations, the antenna assembly 202 can be at an angle to the first axis of rotation O1, such as 45 degrees, the second drive assembly 13 can be omitted, the first drive The assembly 12 is coupled to the antenna assembly 20, and in use, the first axis of rotation O1 is vertically disposed, the antenna assembly 20 is at an angle of 45 degrees to a horizontal plane, and the first drive assembly 12 drives the antenna The assembly 20 is rotated about the first axis of rotation O1 to point to the unmanned aerial vehicle.
- the first driving component 12 is configured to drive the second driving component 13 and the antenna component 20 to rotate about the first rotation axis O1
- the second driving component 13 is used to drive the
- the antenna assembly 20 is rotated about the second axis of rotation O2, the first axis of rotation O1 and the second axis of rotation O2 being perpendicular to each other, such that the maximum radiation direction of the antenna assembly 20 can track the UAV In order to enable the UAV to obtain a better remote control signal from the antenna assembly 20, thereby achieving the purpose of remotely controlling the UAV.
- Another embodiment of the present invention provides a remote control kit including a remote controller and the UAV tracking antenna 100 provided by the above embodiment, the remote controller being coupled to the UAV tracking antenna 100 via the wire 184. It will be appreciated that in some other embodiments, the remote control can be coupled to the UAV tracking antenna 100 by wireless communication, such as Bluetooth, WiFi, and the like.
- Yet another embodiment of the present invention provides an unmanned aerial vehicle kit including an unmanned aerial vehicle and a remote control kit provided by the above embodiment, the remote controller being communicable with the unmanned aerial vehicle through the UAV tracking antenna 100 .
- the UAV may be a fixed wing unmanned aerial vehicle, a multi-rotor unmanned aerial vehicle, or the like.
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Abstract
Description
【相关申请的交叉引用】[Cross-reference to related applications]
本申请要求申请号为201711483798.X,申请日为2017年12月29日申请的中国专利申请的优先权,其全部内容通过引用结合于本文。The present application claims priority to the Japanese Patent Application No. JP-A------
本发明涉及无人飞行器技术领域,尤其涉及一种无人飞行器跟踪天线,遥控器套件以及无人飞行器套件。The present invention relates to the field of unmanned aerial vehicles, and more particularly to an unmanned aerial vehicle tracking antenna, a remote control kit, and an unmanned aerial vehicle kit.
固定翼无人飞行器是无人飞行器领域的重要一员,其飞行距离相对多旋翼无人飞行器要远很多,飞行时间也要更长。传统的无人飞行器的遥控器通常采用全向天线,由于全向天线的辐射增益低,通信距离受限(一般低于10公里),当无人飞行器飞行距离达到数十公里甚至上百公里时,全向天线就不能完全满足要求了,大大降低用户使用无人飞行器遥控器控制无人飞行器的体验。因此,有必要提供一种通信距离长的遥控器天线。Fixed-wing unmanned aerial vehicles are an important part of the field of unmanned aerial vehicles. Their flight distance is much longer than that of multi-rotor unmanned aerial vehicles, and the flight time is longer. The traditional UAV remote control usually uses an omnidirectional antenna. Due to the low radiation gain of the omnidirectional antenna, the communication distance is limited (generally less than 10 km), when the UAV flight distance reaches tens of kilometers or even hundreds of kilometers. The omnidirectional antenna can not fully meet the requirements, greatly reducing the user experience of using the UAV remote control to control the unmanned aerial vehicle. Therefore, it is necessary to provide a remote control antenna having a long communication distance.
【发明内容】[Summary of the Invention]
本发明实施例的目的旨在提供一种无人飞行器跟踪天线,遥控器套件以及无人飞行器套件,以解决现有的无人飞行器的遥控器天线通信距离短的技术问题。The purpose of embodiments of the present invention is to provide an unmanned aerial vehicle tracking antenna, a remote control kit, and an unmanned aerial vehicle kit to solve the technical problem that the remote control antenna of the existing unmanned aerial vehicle has a short communication distance.
本发明实施例解决其技术问题采用以下技术方案:The embodiments of the present invention solve the technical problems and adopt the following technical solutions:
一种无人飞行器跟踪天线,包括:An unmanned aerial vehicle tracking antenna comprising:
天线组件,用于接收所述无人飞行器的位置信息,包括天线模组和与所述天线模组相连的支座;以及An antenna assembly, configured to receive position information of the unmanned aerial vehicle, including an antenna module and a support connected to the antenna module;
主体部,所述天线组件通过所述支座安装于所述主体部,用于根据所述天线组件接收的所述无人飞行器的所述位置信息,驱动所述天线组件转动, 以使得所述天线组件的最大辐射方向指向所述无人飞行器。a main body portion, the antenna assembly is mounted to the main body portion through the support, and is configured to drive the antenna assembly to rotate according to the position information of the unmanned aerial vehicle received by the antenna assembly, so that the The maximum radiation direction of the antenna assembly is directed to the unmanned aerial vehicle.
在本发明的一实施例中,所述主体部包括:In an embodiment of the invention, the main body portion includes:
壳体;case;
第二驱动组件,设于所述壳体内并与所述支座相连,所述第二驱动组件用于驱动所述天线组件绕第二旋转轴线转动;以及a second drive assembly disposed in the housing and coupled to the mount, the second drive assembly for driving the antenna assembly to rotate about a second axis of rotation;
第一驱动组件,至少有部分设于所述壳体内,所述第一驱动组件用于驱动所述壳体、所述天线组件和所述第二驱动组件绕第一旋转轴线转动;a first driving component, at least partially disposed in the housing, the first driving component for driving the housing, the antenna assembly and the second driving component to rotate about a first rotation axis;
所述第一旋转轴线与所述第二旋转轴线垂直。The first axis of rotation is perpendicular to the second axis of rotation.
在本发明的一实施例中,所述第一驱动组件包括:In an embodiment of the invention, the first driving component comprises:
底座,具有连接轴;a base having a connecting shaft;
转盘,安装于所述连接轴,可相对于所述底座绕所述第一旋转轴线转动;a turntable mounted on the connecting shaft, rotatable relative to the base about the first axis of rotation;
第一电机,安装于所述转盘,所述第一电机的转动轴贯穿所述转盘;以及a first motor mounted to the turntable, the rotating shaft of the first motor penetrating the turntable;
齿轮机构,包括套设于所述转动轴的第一齿轮和套设于所述连接轴的第二齿轮,所述第一齿轮与所述第二齿轮啮合。The gear mechanism includes a first gear sleeved on the rotating shaft and a second gear sleeved on the connecting shaft, and the first gear meshes with the second gear.
在本发明的一实施例中,所述底座位于所述壳体外部。In an embodiment of the invention, the base is located outside of the housing.
在本发明的一实施例中,所述转盘设于所述壳体内。In an embodiment of the invention, the turntable is disposed in the housing.
在本发明的一实施例中,所述第一齿轮和所述第二齿轮皆为直齿轮;或者,In an embodiment of the invention, the first gear and the second gear are both spur gears; or
所述第一齿轮和所述第二齿轮皆为斜齿轮。The first gear and the second gear are both helical gears.
在本发明的一实施例中,所述第一驱动组件还包括轴承,所述轴承套设于所述连接轴,所述转盘固定安装于两个所述轴承之间。In an embodiment of the invention, the first driving assembly further includes a bearing, the bearing is sleeved on the connecting shaft, and the turntable is fixedly mounted between the two bearings.
在本发明的一实施例中,所述第一电机为无刷直流减速电机。In an embodiment of the invention, the first motor is a brushless DC gear motor.
在本发明的一实施例中,所述第二驱动组件包括:In an embodiment of the invention, the second driving component comprises:
轴臂,自所述转盘向远离所述转盘的方向垂直延伸;a shaft arm extending perpendicularly from the turntable in a direction away from the turntable;
电机座,与所述轴臂相连;以及a motor mount coupled to the axle arm;
第二电机,安装于所述电机座;a second motor mounted to the motor base;
所述第二电机的转轴的中轴线与所述第二旋转轴线重合,所述第二电机的转轴与所述支座连接,用于驱动所述天线组件绕所述第二旋转轴线转动。A central axis of the rotating shaft of the second motor coincides with the second axis of rotation, and a rotating shaft of the second motor is coupled to the holder for driving the antenna assembly to rotate about the second axis of rotation.
在本发明的一实施例中,所述支座包括第一支座和与所述第一支座相对 间隔设置的第二支座;In an embodiment of the invention, the support comprises a first support and a second support spaced apart from the first support;
所述第二电机的转轴与所述第一支座相连,所述第二驱动组件还包括安装于所述第二支的角度传感器,所述角度传感器用于感测所述第二电机的转轴的旋转角度。a rotating shaft of the second motor is coupled to the first support, the second driving assembly further includes an angle sensor mounted on the second branch, the angle sensor is configured to sense a rotating shaft of the second motor The angle of rotation.
在本发明的一实施例中,所述第二驱动组件还包括自所述第二支座向所述第二电机延伸的安装杆,所述角度传感器安装于所述安装杆的一端。In an embodiment of the invention, the second drive assembly further includes a mounting rod extending from the second mount to the second motor, the angle sensor being mounted to one end of the mounting rod.
在本发明的一实施例中,所述第二电机为无刷直流减速电机。In an embodiment of the invention, the second motor is a brushless DC gear motor.
在本发明的一实施例中,所述无人飞行器跟踪天线还包括设于所述壳体内的主板、用于给所述主板供电的电池组件以及与所述主板电连接的图传模组;In an embodiment of the present invention, the UAV tracking antenna further includes a main board disposed in the housing, a battery assembly for supplying power to the main board, and a graphic transmission module electrically connected to the main board;
所述天线组件、所述第一驱动组件和所述第二驱动组件均与所述主板电连接。The antenna assembly, the first driving component, and the second driving component are all electrically connected to the motherboard.
在本发明的一实施例中,所述无人飞行器跟踪天线还包括设于所述壳体内的滑环,所述滑环包括:In an embodiment of the invention, the UAV tracking antenna further includes a slip ring disposed in the housing, the slip ring includes:
定子部,安装于所述转盘;a stator portion mounted to the turntable;
转子部,套设于所述连接轴且收容于所述定子部内,所述转子部可相对于所述定子部转动;以及a rotor portion sleeved in the connecting shaft and housed in the stator portion, the rotor portion being rotatable relative to the stator portion;
导线,所述导线贯穿所述转子部和所述连接轴,且所述导线的一端与所述主板电连接。a wire penetrating the rotor portion and the connecting shaft, and one end of the wire is electrically connected to the main board.
在本发明的一实施例中,所述壳体包括第一壳体部,第二壳体部和第三壳体部,所述第一壳体部,所述第二壳体部和所述第三壳体部相互扣合。In an embodiment of the invention, the housing includes a first housing portion, a second housing portion and a third housing portion, the first housing portion, the second housing portion, and the The third housing portions are fastened to each other.
在本发明的一实施例中,所述壳体为一体成型的壳体。In an embodiment of the invention, the housing is an integrally formed housing.
在本发明的一实施例中,所述第一壳体部包括第一侧壁和第二侧壁,两个所述第二侧壁相互平行地连接于所述第一侧壁的相对两侧;In an embodiment of the invention, the first housing portion includes a first side wall and a second side wall, and the two second side walls are connected to each other in parallel with each other on opposite sides of the first side wall ;
所述第二壳体部包括底壁和第三侧壁,所述底壁连接所述第三侧壁,所述第一侧壁和两个所述第二侧壁分别安装于所述底壁,所述第三侧壁的相对两侧分别连接两个所述第二侧壁,所述第三侧壁设有缺口,并且所述第三侧壁的相对两侧延伸出安装框架;The second housing portion includes a bottom wall and a third side wall, the bottom wall is connected to the third side wall, and the first side wall and the two second side walls are respectively mounted on the bottom wall The two sides of the third side wall are respectively connected to the two second side walls, the third side wall is provided with a notch, and opposite sides of the third side wall extend out of the mounting frame;
所述第三壳体包括顶壁,嵌入壁和连接壁,所述顶壁安装于所述安装框架,所述嵌入壁嵌入所述缺口,所述连接壁连接于所述顶壁和所述嵌入壁之 间。The third housing includes a top wall, an insertion wall and a connecting wall, the top wall is mounted to the mounting frame, the embedded wall is embedded in the notch, the connecting wall is connected to the top wall and the embedded Between the walls.
在本发明的一实施例中,所述安装框架包括三条安装边条,所述三条安装边条分别安装于所述第一侧壁和两个所述第二侧壁;In an embodiment of the invention, the mounting frame includes three mounting strips, and the three mounting strips are respectively mounted on the first sidewall and the two sidewalls;
所述顶壁安装于所述安装框架的三条安装边条。The top wall is mounted to three mounting strips of the mounting frame.
在本发明的一实施例中,所述连接壁为包括圆柱形空腔,所述圆柱形空腔收容所述第二驱动组件。In an embodiment of the invention, the connecting wall includes a cylindrical cavity that receives the second drive assembly.
在本发明的一实施例中,所述天线模组为垂直极化平板天线模组。In an embodiment of the invention, the antenna module is a vertically polarized planar antenna module.
为解决其技术问题,本发明还提供一种遥控器套件,包括遥控器和如上述所述的无人飞行器跟踪天线,所述遥控器和所述无人飞行器跟踪天线通信连接。In order to solve the technical problem thereof, the present invention also provides a remote controller kit including a remote controller and an unmanned aerial vehicle tracking antenna as described above, the remote controller and the unmanned aerial vehicle tracking antenna communication connection.
为解决其技术问题,本发明还提供一种无人飞行器套件,包括无人飞行器和如上述所述的遥控器套件,所述遥控器可通过所述无人飞行器跟踪天线与所述无人飞行器通信连接。In order to solve the technical problem thereof, the present invention also provides an unmanned aerial vehicle kit comprising an unmanned aerial vehicle and a remote control kit as described above, the remote controller being capable of tracking an antenna and the unmanned aerial vehicle through the unmanned aerial vehicle Communication connection.
与现有技术相比较,在本发明实施例的无人飞行器跟踪天线中,所述主体部可驱动所述天线组件转动,使得所述天线组件的最大辐射方向指向无人飞行器,以使所述无人飞行器能从所述天线组件获得较佳的遥控信号,从而实现远距离控制无人飞行器的目的。In an unmanned aerial vehicle tracking antenna according to an embodiment of the present invention, the main body portion can drive the antenna assembly to rotate such that a maximum radiation direction of the antenna assembly is directed to an unmanned aerial vehicle, so that the The unmanned aerial vehicle can obtain a better remote control signal from the antenna assembly, thereby achieving the purpose of remotely controlling the unmanned aerial vehicle.
一个或多个实施例通过与之对应的附图进行示例性说明,这些示例性说明并不构成对实施例的限定,附图中具有相同参考数字标号的元件表示为类似的元件,除非有特别申明,附图中的图不构成比例限制。The one or more embodiments are exemplified by the accompanying drawings, which are not to be construed as limiting. It is stated that the figures in the drawings do not constitute a proportional limitation.
图1为本发明其中一实施例提供的一种无人飞行器跟踪天线的立体图;1 is a perspective view of an unmanned aerial vehicle tracking antenna according to an embodiment of the present invention;
图2为图1所示的无人飞行器跟踪天线的另一角度的立体图;Figure 2 is a perspective view of another angle of the UAV tracking antenna shown in Figure 1;
图3为图1所示的无人飞行器跟踪天线的分解图;Figure 3 is an exploded view of the UAV tracking antenna shown in Figure 1;
图4为图1所示的无人飞行器跟踪天线的另一角度的分解图;4 is an exploded view of another angle of the UAV tracking antenna shown in FIG. 1;
图5为图1所示的无人飞行器跟踪天线中第一驱动组件和第二驱动组件 的装配图;Figure 5 is an assembled view of the first drive assembly and the second drive assembly of the UAV tracking antenna of Figure 1;
图6为图1所示的无人飞行器跟踪天线中第一驱动组件和第二驱动组件另一角度的装配图;6 is an assembled view of another angle of the first drive component and the second drive component in the UAV tracking antenna shown in FIG. 1;
图7为图6所示的装配图中第一驱动组件,底座以及滑环的装配图;Figure 7 is an assembled view of the first drive assembly, the base and the slip ring in the assembled view shown in Figure 6;
图8为图1所示的无人飞行器跟踪天线中滑环的立体图。8 is a perspective view of a slip ring in the UAV tracking antenna shown in FIG. 1.
为了便于理解本发明,下面结合附图和具体实施例,对本发明进行更详细的说明。需要说明的是,当元件被表述“固定于”另一个元件,它可以直接在另一个元件上、或者其间可以存在一个或多个居中的元件。当一个元件被表述“连接”另一个元件,它可以是直接连接到另一个元件、或者其间可以存在一个或多个居中的元件。本说明书所使用的术语“垂直的”、“水平的”、“左”、“右”、“内”、“外”以及类似的表述只是为了说明的目的。In order to facilitate the understanding of the present invention, the present invention will be described in more detail below with reference to the accompanying drawings and specific embodiments. It is to be noted that when an element is described as being "fixed" to another element, it can be directly on the other element, or one or more central elements can be present. When an element is referred to as "connected" to another element, it can be a <RTI ID=0.0> </ RTI> </ RTI> <RTIgt; The terms "vertical," "horizontal," "left," "right," "inside," "outside," and the like, as used in this specification, are for the purpose of illustration.
除非另有定义,本说明书所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。在本发明的说明书中所使用的术语只是为了描述具体的实施例的目的,不是用于限制本发明。本说明书所使用的术语“和/或”包括一个或多个相关的所列项目的任意的和所有的组合。Unless otherwise defined, all technical and scientific terms used in the specification are the same meaning The terms used in the description of the present invention are for the purpose of describing the specific embodiments and are not intended to limit the invention. The term "and/or" used in this specification includes any and all combinations of one or more of the associated listed items.
此外,下面所描述的本发明不同实施例中所涉及的技术特征只要彼此之间未构成冲突就可以相互结合。Further, the technical features involved in the different embodiments of the present invention described below may be combined with each other as long as they do not constitute a conflict with each other.
请一并参阅图1和图2,本发明其中一实施例提供的一种无人飞行器跟踪天线100包括主体部10和天线组件20。所述天线组件20安装于所述主体部10,用于接收无人飞行器位置信息,所述主体部10用于获取所述天线组件20接收的所述无人飞行器位置信息,并根据所述无人飞行器位置信息调节所述天线组件20,使得所述天线组件20的最大辐射方向指向所述无人飞行器,以使所述无人飞行器能从所述天线组件20获得较佳的遥控信号。Referring to FIG. 1 and FIG. 2 , an unmanned aerial
请参阅图3,所述天线组件20包括天线模组202和设于所述天线模组202背面并与所述天线模组202相连的支座。所述天线模组202为垂直极化平板天线模组,用于与所述无人飞行器通信,包括接收所述无人飞行器位置信息,发送遥控器发出的遥控信号等。在本实施例中,所述天线模组202采用平板 天线,实现定向发射和接收信号,相比于全方向天线,信号更强。在本发明的一实施例中,所述支座包括第一支座204和与所述第一支座204相对间隔设置的第二支座206。所述第一支座204和所述第二支座206分别固定安装于所述天线模组202,所述第一支座204和所述第二支座206分别铰接所述主体部10。Referring to FIG. 3 , the
可以理解的是,在一些其他实施例中,所述天线模组202还可以为其他类型的天线模组,如水平极化平板天线模组,只要能和无人飞行器上的天线更好配合使用即可,这里不作严格限制。It can be understood that in some other embodiments, the
请一并参阅图3和图4,所述主体部10包括壳体、至少有部分设于所述壳体内的第一驱动组件12、设于所述壳体内的第二驱动组件13、设于所述壳体内的主板15、用于给主板15供电的电池组件16、与主板15电连接的图传模组17和设于所述壳体内的滑环18。天线组件20、第一驱动组件12、第二驱动组件13以及滑环18均与主板15电连接。Referring to FIG. 3 and FIG. 4 together, the
所述壳体大致为长方体,可由塑胶材料制得,所述壳体包括第一壳体部190,第二壳体部192和第三壳体部194。第一壳体部190、第二壳体部192和第三壳体部194相互扣合形成收容空间。在其他可能的实施例中,所述壳体也可以是一体成型的壳体。The housing is generally rectangular parallelepiped and may be fabricated from a plastic material, the housing including a
所述第一壳体部190包括第一侧壁1902和第二侧壁1904,两个所述第二侧壁1904相互平行地连接于所述第一侧壁1902的相对两侧。所述第一侧壁1902设有导线通孔1906。The
所述第二壳体部192包括底壁1922和第三侧壁1924。所述底壁1922连接所述第三侧壁1924,所述第一侧壁1902和两个所述第二侧壁1904分别安装于所述底壁1922,所述底壁1922设有底座通孔1926。所述第三侧壁1924的相对两侧分别连接两个所述第二侧壁1904,所述第三侧壁1924朝向所述第一侧壁1902,且所述第三侧壁1924和所述第一侧壁1902相互平行。所述第三侧壁1924设有缺口1928,并且所述第三侧壁1924的相对两侧延伸出安装框架1927,所述安装框架1927包括三条安装边条,所述三条安装边条相互连接且分别安装于所述第一侧壁1902和两个所述第二侧壁1904。The
所述第三壳体194包括顶壁1942,嵌入壁1944和连接壁1946。所述顶壁1942安装于所述安装框架1927的三条安装边条。所述嵌入壁1944嵌入所 述缺口1928。所述连接壁1946连接于所述顶壁1942和所述嵌入壁1944之间,所述连接壁1946包括圆柱形空腔,用于收容所述第二驱动组件13。所述连接壁1946的相对两侧分别设有两个安装孔1948。The
所述第一壳体部190,所述第二壳体部192和所述第三壳体部194相互扣合组成所述壳体,可方便将所述转盘11,第一驱动组件12,第二驱动组件13,底座14,主板15,电池组件16,图传模组17以及滑环18安装于所述壳体内。The
第一驱动组件12包括具有连接轴123的底座14、安装于所述连接轴123的转盘11、安装于所述转盘11的第一电机120和齿轮机构。The
在本发明的一实施例中,底座14位于壳体外部,转盘11设于所述壳体内部。在其他可能的实施例中,底座14也可以设于壳体内部。所述转盘11固定安装于所述壳体内,所述转盘11支承所述第一驱动组件12,所述第二驱动组件13,图传模组17,滑环18,所述主板15和所述电池组件16。所述转盘11可由重量轻且强度合适的材料制得,例如,铝合金,镁合金或者塑胶材料等。In an embodiment of the invention, the
请一并参阅图5至图7,所述第一电机120用于驱动所述转盘11,所述第一驱动组件12,所述第二驱动组件13,所述电路板15,所述电池组件16,所述图传模组17以及所述外壳绕所述底座14转动,以使所述天线组件20绕第一旋转轴线O1转动。Referring to FIG. 5 to FIG. 7 together, the
所述第一电机120固定安装于所述转盘12,其转动轴121贯穿所述转盘11,所述第一电机120可为无刷直流减速电机,为大减速比电机,从而提供大扭矩。The
所述转动轴121穿过所述转盘12,所述转动轴121通过联轴器连接所述第一电机120的转轴。所述转动轴121的中轴线与所述第一电机120的转轴的中轴线重合。The
齿轮机构包括套设于所述转动轴121的第一齿轮122和套设于所述连接轴123的第二齿轮125,第二齿轮125与第一齿轮122啮合。在本发明的一实施例中,所述第一齿轮122与所述第二齿轮125均为直齿轮。在其他可能的实施例中,所述第一齿轮122与所述第二齿轮125也可以是斜齿轮。The gear mechanism includes a
所述连接轴123的一端固定连接所述底座14,另一端连接所述滑环18。所述转动轴121与所述连接轴123平行设置。所述连接轴123的中轴线与所 述第一旋转轴线O1重合。One end of the connecting
第一驱动组件12还可以包括轴承124,所述轴承124套设于所述连接轴123,所述转盘11套设于所述连接轴123,并固定安装于两个所述轴承124之间,所述转盘11和所述轴承124可一同绕所述第一旋转轴线O1相对于所述连接轴123转动。The
所述第一电机120工作时,所述第一电机120为所述转动轴121和所述第一齿轮122提供旋转动力,在所述底座14,所述连接轴123和所述第二齿轮125保持不动的情况下,所述第一电机120带动所述转盘11,所述轴承124,所述转动轴121以及所述第一齿轮122一同绕所述第一旋转轴线O1和所述第二齿轮125转动。When the
可以理解的是,在一些其它实施例中,,所述转动轴121和所述连接轴123之间还可以通过皮带传动,或者其它合适的传动方式等。It can be understood that in some other embodiments, the
所述第二驱动组件13与所述天线组件20的支座连接,用于驱动所述天线组件20绕第二旋转轴线O2转动,所述第二旋转轴线O2垂直于所述第一旋转轴线O1。所述第二驱动组件13包括第二电机130,电机座131,角度传感器133以及轴臂134。The
所述第二电机130的转轴的中轴线与所述第二旋转轴线O2重合。所述第二电机130可为无刷直流减速电机,为大减速比电机,从而提供大扭矩。A central axis of the rotating shaft of the
所述电机座131为长方体框架结构,有利于减轻重量。所述第二电机130通过轴承安装于所述电机座131,所述第二电机130的转轴依次穿过所述轴承和所述第三壳体194的安装孔1948,连接所述第一支座204。The
所述角度传感器133通过一安装杆1330固定安装于所述第二支座206,用于感测所述第二电机130的转轴的旋转角度。在其他可能的实施例中,角度传感器133也可以直接安装在第二支座206上。The
所述轴臂134大致为杆状,其一端自所述转盘11向远离所述转盘11的方向垂直延伸,并与所述转盘11固定连接,另一端用于安装于所述电机座131。所述转盘11绕所述第一旋转轴线O1相对于所述连接轴123转动时,所述转盘11通过所述轴臂134带动所述第二驱动组件13绕所述第一旋转轴线O1转动,从而也带动所述天线组件20绕所述第一旋转轴线O1转动。The
所述第二电机130工作时,所述第二电机130的转轴驱动所述第一支座 204转动,从而带动所述天线组件20绕所述第二旋转轴线O2转动。When the
所述底座14固定安装于所述连接轴123的一端,并收容于所述底座通孔1926,所述底座14可相对于所述外壳转动。所述底座14设有螺纹接口140(见图4),用于连接三脚架,例如,相机三脚架,从而可将所述无人飞行器跟踪天线100安装于三脚架。所述螺纹接口140可为1/4英寸的相机三脚架通用螺纹接口。The
请复参阅图3,所述主板15与所述天线组件20,所述第一驱动组件12和所述第二驱动组件13电连接。所述主板15上安装有主控制器和存储器等电子元器件,所述主板15用于从所述天线组件20接收所述无人飞行器位置信息,解析所述无人飞行器位置信息后获得所述无人飞行器的位置,包括经度,纬度以及高度,并结合遥控器发出的飞行方向指令,计算得到所述无人飞行器的准确位置,根据计算得到的所述无人飞行器的准确位置控制所述第一驱动组件12和所述第二驱动组件13工作,以调节所述天线组件20的最大辐射方向指向所述无人飞行器。所述主板15安装于所述电池组件16。Referring to FIG. 3, the
可以理解的是,在一些其它实施例中,所述主板15可根据实际需要安装于所述壳体内的任何位置。It can be understood that in some other embodiments, the
所述电池组件16包括电池仓160和电池162,所述电池仓160通过支架固定安装于所述转盘11,所述主板15安装于所述电池仓160。所述电池160安装于所述电池仓160内,用于为所述主板15,所述第一电机120,所述第二电机130以及所述天线模组202供电。The battery pack 16 includes a battery compartment 160 and a
所述图传模组17和射频模块安装在安装板上,所述安装板用螺钉安装在所述轴臂134,所述图传模组17用于接收所述无人飞行器发送的图像。The
请一并参阅图7和图8,所述滑环18包括定子部180,转子部182以及导线184,所述定子部180套设于所述转子部182外,所述转子部182固定连接所述连接轴123,所述定子部180固定连接所述轴承124,以使得所述定子部180固定安装于所述转盘11。所述导线184贯穿所述转子部182,所述导线184包括射频线和信号线。所述导线184的一端与所述主板15电连接,所述定子部180可以随所述转盘11和所述轴承124相对于所述转子部182无限次旋转,所述导线184的射频线和信号线贯穿所述连接轴123后,穿过所述底座14向外引出连接射频线接口、耳机孔和USB口,从而实现与遥控器有 线通信。Referring to FIG. 7 and FIG. 8 together, the
使用时,将所述无人飞行器跟踪天线100安装于三脚架,所述第一旋转轴线O1竖直设置,所述第二旋转轴线O2水平设置。所述无人飞行器通过其定位模块(例如北斗定位模块)获取所述无人飞行器的坐标(包括经度和纬度),通过其气压计获取所述无人飞行器的高度,从而确定所述无人飞行器与所述无人飞行器跟踪天线100的相对位置,通过控制所述第一驱动组件12来调节所述天线组件20的水平角度,通过控制所述第二驱动组件13来调节所述天线组件20的俯仰角度,使得所述天线模组202的最大辐射方向实时跟踪所述无人飞行器。遥控器通过信号线连接所述无人飞行器跟踪天线100,通过所述天线模组202向所述无人飞行器发送遥控指令,从而实现远距离控制无人飞行器的目的。In use, the
在本实施例中,所述无人飞行器跟踪天线100的调节范围是:绕所述第一旋转轴线O1为无限转,也就是没有旋转角度限制,绕所述第二旋转轴线O2的旋转角度为-25至90度。In this embodiment, the adjustment range of the
在本实施例中,借助所述第一驱动组件12和所述第二驱动组件13可以大范围调节所述天线组件20的角度,以使所述天线组件20的最大辐射方向指向所述无人飞行器,可以理解的是,在一些其它实施中,所述天线组件202可与所述第一旋转轴线O1呈夹角,例如45度,所述第二驱动组件13可以省略,所述第一驱动组件12与所述天线组件20连接,在使用时,所述第一旋转轴线O1竖直设置,所述天线组件20与水平面的夹角为45度,所述第一驱动组件12驱动所述天线组件20绕所述第一旋转轴线O1转动,以指向无人飞行器。In this embodiment, the angle of the
在本实施例中,所述第一驱动组件12用于驱动所述第二驱动组件13和所述天线组件20绕所述第一旋转轴线O1转动,所述第二驱动组件13用于驱动所述天线组件20绕所述第二旋转轴线O2转动,所述第一旋转轴线O1与所述第二旋转轴线O2相互垂直,可使得所述天线组件20的最大辐射方向能跟踪所述无人飞行器,以使所述无人飞行器能从所述天线组件20获得较佳的遥控信号,从而实现远距离控制无人飞行器的目的。In this embodiment, the
本发明另一实施例提供一种遥控器套件,包括遥控器和以上实施例所提供的无人飞行器跟踪天线100,所述遥控器通过所述导线184与所述无人飞行 器跟踪天线100连接。可以理解的是,在一些其它实施例中,所述遥控器可通过无线通信方式与所述无人飞行器跟踪天线100连接,例如,蓝牙,WiFi等。Another embodiment of the present invention provides a remote control kit including a remote controller and the
本发明又一实施例提供一种无人飞行器套件,包括无人飞行器和以上实施例所提供的遥控器套件,所述遥控器可通过所述无人飞行器跟踪天线100与所述无人飞行器通信。所述无人飞行器可以是固定翼无人飞行器,多旋翼无人飞行器等。Yet another embodiment of the present invention provides an unmanned aerial vehicle kit including an unmanned aerial vehicle and a remote control kit provided by the above embodiment, the remote controller being communicable with the unmanned aerial vehicle through the
最后应说明的是:以上实施例仅用以说明本发明的技术方案,而非对其限制;在本发明的思路下,以上实施例或者不同实施例中的技术特征之间也可以进行组合,步骤可以以任意顺序实现,并存在如上所述的本发明的不同方面的许多其它变化,为了简明,它们没有在细节中提供;尽管参照前述实施例对本发明进行了详细的说明,本领域的普通技术人员应当理解:其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本发明各实施例技术方案的范围。Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, and are not limited thereto; in the idea of the present invention, the technical features in the above embodiments or different embodiments may also be combined. The steps may be carried out in any order, and there are many other variations of the various aspects of the invention as described above, which are not provided in the details for the sake of brevity; although the invention has been described in detail with reference to the foregoing embodiments, It should be understood by those skilled in the art that the technical solutions described in the foregoing embodiments may be modified or equivalently substituted for some of the technical features; and the modifications or substitutions do not deviate from the embodiments of the present invention. The scope of the technical solution.
Claims (22)
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| CN201711483798.XA CN108008741B (en) | 2017-12-29 | 2017-12-29 | Unmanned vehicles tracking antenna, remote controller external member and unmanned vehicles external member |
| CN201711483798.X | 2017-12-29 |
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| CN112599955A (en) * | 2020-12-18 | 2021-04-02 | 安徽恒诺机电科技有限公司 | Servo turntable for antenna erection |
| CN112635996A (en) * | 2020-11-06 | 2021-04-09 | 广州辰创科技发展有限公司 | Ka-band antenna pointing control execution method |
| CN115189134A (en) * | 2022-08-09 | 2022-10-14 | 北京赛博通科技发展有限公司 | Automatic tracking antenna |
| CN118099703A (en) * | 2024-04-28 | 2024-05-28 | 鱼合熊掌网络科技南通有限公司 | Internet of things monitoring equipment antenna |
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| CN108008741B (en) * | 2017-12-29 | 2022-06-03 | 深圳市道通智能航空技术股份有限公司 | Unmanned vehicles tracking antenna, remote controller external member and unmanned vehicles external member |
| CN110769364B (en) * | 2019-10-16 | 2020-12-18 | 广东美嘉欣创新科技股份有限公司 | A UAV flight data and image transmission system |
| CN114256617A (en) * | 2021-12-24 | 2022-03-29 | 中国电子科技集团公司第五十四研究所 | Series multi-target microwave communication antenna |
| CN217932035U (en) * | 2022-03-16 | 2022-11-29 | 深圳市道通智能航空技术股份有限公司 | Unmanned aerial vehicle tracking means |
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| CN108008741A (en) | 2018-05-08 |
| CN108008741B (en) | 2022-06-03 |
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