Light reflecting mechanism and unmanned aerial vehicle system

By installing reflectors and servo motor-driven reflective light mechanisms on the drone, the light beam is reflected to multiple directions, solving the problems of increased load and shortened battery life caused by the drone light source, achieving longer battery life and better Good light effect.

CN222230328UActive Publication Date: 2024-12-24何佳林
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Patent Information

Application Number
CN202421115723.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-05-22
Publication Date
2024-12-24
Estimated Expiration
2034-05-22

AI Technical Summary

Technical Problem

When existing drones are equipped with light sources, high brightness leads to an increase in battery mass, an increase in load capacity, and a shortened battery life, making it difficult to meet the needs of lighting performances while extending the battery life.

Method used

Design a reflective light mechanism to use reflectors to reflect the beam emitted by the lower light source to multiple directions, reduce the burden on the light source and battery on the drone, and adjust the beam angle through the servo motor, combining with GPS-RTK in the drone system Positioning components and remote control enable precise control.

Benefits of technology

Effectively reduce the load on the drone, extend the battery life, and improve the light effect. It is suitable for outdoor light shows and performance scenes.

✦ Generated by Eureka AI based on patent content.

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Patent Text Reader

Abstract

The utility model discloses a reflection light mechanism and unmanned aerial vehicle system relates to unmanned aerial vehicle technical field, wherein the reflection light mechanism mainly includes lower part light source and reflector, lower part light source is used for emitting lower part light beam to unmanned aerial vehicle, the reflector is used for installing on the unmanned aerial vehicle, the reflector is three-dimensional structure, and the reflector is used for installing on the unmanned aerial vehicle. A reflecting lens is laid on the surface of the reflecting body and used for reflecting the lower light beams emitted by the lower light source in multiple directions. The unmanned aerial vehicle system comprises the unmanned aerial vehicle and the light reflecting mechanism, the unmanned aerial vehicle comprises an unmanned aerial vehicle body, the reflector is installed at the bottom of the unmanned aerial vehicle body, a plurality of connecting arms are further arranged on the unmanned aerial vehicle body, and the light reflecting mechanism is arranged on the connecting arms. And a propeller is arranged at the end part of one end, far away from the unmanned aerial vehicle body, of any connecting arm. The unmanned aerial vehicle can effectively reduce the load of the unmanned aerial vehicle, prolong the endurance time of the unmanned aerial vehicle and improve the light effect.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a reflective lighting mechanism and an unmanned aerial vehicle system. Background Art

[0002] Existing drones can carry light sources to work in the air, producing unique light effects for light shows. However, the light sources carried by drones need to be powered by batteries. When the brightness of the light source is very high, a large battery is required, which makes the drone carry a large load and greatly shortens the drone's flight time.

[0003] Therefore, how to extend the flight time of drones while meeting the needs of drone light performances has become a technical problem that needs to be solved urgently. Utility Model Content

[0004] The purpose of the utility model is to provide a reflective lighting mechanism and a UAV system to solve the problems existing in the above-mentioned prior art, which can effectively reduce the load of the UAV, extend the flight time of the UAV, and improve the lighting effect.

[0005] To achieve the above purpose, the utility model provides the following solutions:

[0006] The utility model provides a light reflection mechanism, comprising:

[0007] A lower light source, the lower light source is used to emit a lower light beam to the drone;

[0008] A reflector is used to be installed on the drone, and the reflector is a three-dimensional structure. A reflective lens is laid on the surface of the reflector to reflect the lower light beam emitted by the lower light source in multiple directions.

[0009] Preferably, the reflector is a spherical structure, and the spherical surface of the spherical structure faces downward, and the reflective lens is laid on the spherical surface;

[0010] Wherein, a plurality of circles of the reflective lenses are sequentially arranged on the spherical surface along its radial direction, and a plurality of the reflective lenses in any circle are evenly distributed along the circumference.

[0011] Preferably, the reflector is a spherical structure formed by 3D printing using a resin material.

[0012] Preferably, a silver-plated layer is provided on the reflective surface of the reflective lens.

[0013] Preferably, the lower light source is a beam lamp, and the beam lamp is connected to a driving system, and the driving system can drive the beam lamp to follow the rotation of the drone to adjust the angle at which the beam lamp emits the lower light beam.

[0014] Preferably, the driving system includes a base, a mounting frame, a first servo motor and a second servo motor, wherein the beam lamp is rotatably mounted on the mounting frame via a horizontal rotating shaft, and the first servo motor is used to drive the beam lamp to rotate around the axis of the horizontal rotating shaft; the mounting frame is rotatably mounted on the base via a vertical rotating shaft, and the second servo motor is used to drive the mounting frame and the beam lamp to rotate around the axis of the vertical rotating shaft.

[0015] The utility model also provides an unmanned aerial vehicle system, comprising an unmanned aerial vehicle and the reflective lighting mechanism as described above; wherein, the unmanned aerial vehicle comprises an unmanned aerial vehicle body, the reflector is installed at the bottom of the unmanned aerial vehicle body, and a plurality of connecting arms are also provided on the unmanned aerial vehicle body, and a propeller is provided at one end of any connecting arm away from the unmanned aerial vehicle body.

[0016] Preferably, it further comprises a positioning bracket, wherein a central through hole is provided in the middle of the positioning bracket, and a plurality of positioning holes are further provided on the positioning bracket, and the positioning holes are arranged around the central through hole;

[0017] A driving motor is provided at the top of one end of any of the connecting arms away from the UAV body, and the driving motor is used to drive the corresponding propeller to rotate; and a positioning rod is provided at the bottom of one end of any of the connecting arms away from the UAV body, and the positioning rod is provided in one-to-one correspondence with the positioning hole on the positioning bracket;

[0018] In the initial state, the positioning bracket is located directly above the lower light source, the positioning rod of the drone body is located in the corresponding positioning hole, and the lower light beam emitted by the lower light source can pass through the central through hole and face the drone body.

[0019] Preferably, the connecting arm is a hollow carbon fiber tube, and one end of the connecting arm away from the drone body extends beyond the reflector.

[0020] Preferably, the flight control chip and battery of the drone are both installed in the drone body, and the battery is used to power the drone; a positioning component is also installed on the drone body, and the positioning component is connected to the flight control chip signal to realize the positioning of the drone, and the flight control chip is also connected to the lower light source signal;

[0021] Wherein, the positioning component is a GPS-RTK positioning component, and is installed above the UAV body;

[0022] The drone system also includes a remote controller, which is connected to the flight control chip signal, wherein the remote controller is provided with a switch button, an azimuth adjustment button, a lifting control lever and a rotating control lever.

[0023] Compared with the prior art, the utility model has achieved the following technical effects:

[0024] The utility model is provided with a reflector, which is carried on the drone and can reflect the lower light beam emitted by the lower light source to produce a unique light effect. Compared with the solution in the prior art that the light source and the battery required for the light source are carried on the drone, the utility model can effectively reduce the load of the drone and extend the flight time of the drone.

[0025] Furthermore, the reflector in the utility model is a three-dimensional structure, and a reflective lens is laid on the surface, which can reflect the lower light beam emitted by the lower light source in multiple directions, thereby improving the light effect. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings required for use in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0027] Figure 1 This is a first angle axonometric view of the drone in the embodiment of the utility model;

[0028] Figure 2 A second angle axonometric view of the drone in the embodiment of the utility model;

[0029] Figure 3 A top view of a drone in an embodiment of the utility model;

[0030] Figure 4 A bottom view of the drone in the embodiment of the utility model;

[0031] Figure 5 A side view of a drone in an embodiment of the utility model;

[0032] Figure 6 It is a partial schematic diagram of a reflector in an embodiment of the utility model;

[0033] Figure 7 This is a schematic diagram of the structure of the lower light source in the embodiment of the utility model;

[0034] Figure 8 This is a schematic diagram of the structure of the positioning bracket in the embodiment of the utility model;

[0035] Fig. 9 It is a three-dimensional schematic diagram of the UAV system in the initial state in the embodiment of the utility model;

[0036] Fig.10 This is a front view of the UAV system in the initial state in the embodiment of the utility model;

[0037] Fig.11 It is a top view of the UAV system in the initial state in the embodiment of the utility model;

[0038] Fig.12 This is a schematic diagram of the working state of the UAV system in the embodiment of the utility model;

[0039] Fig.13 A top view of the working state of the UAV system in the embodiment of the utility model;

[0040] Fig.14 It is a side view of the working state of the UAV system in the embodiment of the utility model;

[0041] Fig.15 This is a schematic diagram of the working state of the drone in the embodiment of the utility model;

[0042] Fig.16 This is a schematic diagram of the horizontal free movement of the drone in the embodiment of the utility model;

[0043] Fig.17 Schematic diagram of the structure of the remote controller in the embodiment of the utility model.

[0044] In the figure: 1-UAV body; 2-connecting arm; 3-driving motor; 4-propeller; 5-positioning assembly; 6-reflector; 7-reflecting lens; 8-lower light source; 9-reflected light; 10-center line of the lower light beam; 11-positioning bracket; 12-positioning hole; 13-remote controller; 14-switch button; 15-azimuth adjustment button; 16-lifting control lever; 17-rotation control lever. DETAILED DESCRIPTION

[0045] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0046] The purpose of the utility model is to provide a reflective lighting mechanism and a UAV system to solve the problems existing in the above-mentioned prior art, which can effectively reduce the load of the UAV, extend the flight time of the UAV, and improve the lighting effect.

[0047] In order to make the above-mentioned purposes, features and advantages of the present invention more obvious and easy to understand, the present invention is further described in detail below in conjunction with the accompanying drawings and specific implementation methods.

[0048] Embodiment 1

[0049] like Figure 1-Figure 17 As shown, in this embodiment, a reflective lighting mechanism is provided, which mainly includes a lower light source 8 and a reflector 6, wherein the lower light source 8 is used to emit a lower light beam to the UAV, and the reflector 6 is used to be installed on the UAV, and the reflector 6 is a three-dimensional structure, and a reflective lens 7 is provided on the surface of the reflector 6, which is used to reflect the lower light beam emitted by the lower light source 8 to multiple directions.

[0050] The lower light source 8 described in this embodiment can be placed directly on the ground or fixed on a mounting bracket according to work needs, and can emit a lower light beam to the drone, and the drone is provided with a reflector 6, which is mounted on the drone and can reflect the lower light beam emitted by the lower light source 8, producing a unique light effect. Compared with the solution of mounting the light source and the battery required for the light source on the drone in the prior art, it can effectively reduce the load of the drone and extend the flight time of the drone. Furthermore, in this embodiment, the reflector 6 is a three-dimensional structure, and a reflective lens 7 is laid on the surface, which can reflect the lower light beam emitted by the lower light source 8 in multiple directions to improve the light effect.

[0051] It should be further explained that the shape of the reflector 6 in this embodiment can be selected according to specific working requirements, and can be a polygonal column, a cone or a spherical structure, or even an irregular shape structure.

[0052] As a preferred embodiment, Figure 1 and Figure 5 As shown, in this embodiment, the reflector 6 is a spherical structure, that is, a part of a hollow sphere, and the spherical surface of the spherical structure faces downward, and the reflective lens 7 is laid on the spherical surface; wherein, the spherical surface is provided with a plurality of circles of the reflective lenses 7 in sequence along its radial direction, and any circle of the reflective lenses 7 has a plurality of lenses evenly distributed along the circumference, and the reflective lens 7 is preferably circular, but is not limited to a circle, and shapes such as a regular polygon or an arc can also be selected as needed.

[0053] In this embodiment, the reflector 6 is preferably made of resin material by 3D printing, which is easy to process and light in weight.

[0054] In this embodiment, a silver-plated layer is further provided on the reflective surface of the reflective lens 7, which can improve the reflectivity and make the intensity of the reflected light 9 higher, so as to achieve a better visual effect.

[0055] In this embodiment, if Figure 7 As shown, the lower light source 8 is preferably a beam lamp, which can provide a high-intensity light source to achieve a better visual effect, and the beam lamp is connected to a driving system, which can drive the beam lamp to follow the rotation of the drone to adjust the angle of the beam lamp emitting the lower light beam.

[0056] As a preferred implementation, in this embodiment, the driving system mainly includes a base, a mounting frame, a first servo motor and a second servo motor, wherein the mounting frame is a U-shaped bracket with an opening at the top, and the beam lamp is rotatably mounted on the mounting frame via a horizontal rotating shaft, and the output shaft of the first servo motor is connected to the horizontal rotating shaft, which can drive the horizontal rotating shaft to rotate, thereby driving the beam lamp to rotate around the axis of the horizontal rotating shaft; the mounting frame is rotatably mounted on the base via a vertical rotating shaft, and the second servo motor can drive the vertical rotating shaft to rotate, thereby driving the mounting frame and the beam lamp to rotate around the axis of the vertical rotating shaft.

[0057] In this embodiment, the above-mentioned driving system is used to give the lower light source 8 two degrees of freedom, which can realize rotation in two directions, so as to better adjust the emission angle; wherein, the driving system can also select other structures according to work needs, as long as it can meet the emission angle adjustment needs of the lower light source 8.

[0058] This embodiment also provides a drone system, such as Figure 1-Figure 5 As shown, it mainly includes a drone and the reflective lighting mechanism as described above; wherein, the drone includes a drone body 1 located in the center, the reflector 6 is installed at the bottom of the drone body 1, and a plurality of connecting arms 2 are also arranged on the drone body 1, wherein the connecting arms 2 extend along the radial direction of the drone body 1, and a plurality of the connecting arms 2 are evenly distributed along the circumference, and a driving motor 3 and a propeller 4 are arranged on the end of any one of the connecting arms 2 away from the drone body 1, and the corresponding propeller 4 is driven to rotate by the driving motor 3 to provide lift for the drone.

[0059] The drone system in this embodiment reflects the light from the lower light source 8 through the reflector 6 installed on the drone, producing a unique light effect, which can be applied to outdoor light shows, outdoor performances and other scenes.

[0060] In this embodiment, the number of connecting arms 2 can be selected according to specific work needs, preferably four; wherein the connecting arm 2 is a hollow carbon fiber tube, which can reduce weight while ensuring strength. Figure 5As shown, one end of the connecting arm 2 away from the UAV body 1 extends beyond the reflector 6, and the excess length is preferably 1.5-2.5 times the rotation radius of the propeller 4. Using a longer connecting arm 2 can ensure that there is no interference between the downward airflow generated by the propeller 4 and the reflector 6.

[0061] In this embodiment, if Figure 8 As shown, the UAV system further includes a positioning bracket 11, a central through hole is provided in the middle of the positioning bracket 11, and a plurality of positioning holes 12 are further provided on the positioning bracket 11, and the positioning holes 12 are arranged around the central through hole; and a positioning rod is provided at the bottom of one end of any connecting arm 2 away from the UAV body 1, and the positioning rod is arranged in a one-to-one correspondence with the positioning holes 12 on the positioning bracket 11;

[0062] like Figure 9-11 As shown, in the initial state, the positioning bracket 11 is located directly above the lower light source 8, and the positioning rod of the UAV body 1 is located in the corresponding positioning hole 12, so that it can be located in the center of the positioning bracket 11. When the center line 10 of the lower light beam emitted by the lower light source 8 is facing upward, it can pass through the center through hole and face the UAV body 1.

[0063] In this embodiment, the flight control chip and battery of the UAV are both installed in the UAV body 1, and the battery is used to power the entire UAV; a positioning component 5 is also installed on the UAV body 1, and the positioning component 5 is signal-connected to the flight control chip for realizing the positioning of the UAV, and the flight control chip is also signal-connected to the lower light source 8; wherein, the positioning component 5 is preferably a GPS-RTK positioning component 5, and is installed above the UAV body 1. By using the GPS-RTK positioning component 5, the positioning accuracy of the UAV reaches the centimeter level, so that the positional relationship between the reflector 6 and the lower light source 8 reaches the required accuracy.

[0064] In this embodiment, the position of the drone in the air is transmitted to the controller of the lower light source 8 through the wireless communication module, and the two angles of the emitted lower light beam relative to the vertical line in space are calculated, and the driving system is controlled to move automatically, driving the lower light source 8 to adjust the emission angle so that the center line 10 of the lower light beam passes through the lower end point of the reflector 6 in real time. Fig.16 As shown, the lower light source 8 illuminates the reflector 6 in the best range to achieve the best visual effect.

[0065] Furthermore, in this embodiment, the drone system further includes a remote controller 13, and the remote controller 13 is connected to the flight control chip signal, wherein Fig.17As shown, the remote controller 13 is provided with a switch button 14 for controlling the switch of the remote controller 13, an azimuth adjustment button 15 for controlling the horizontal movement of the drone in four directions of front, back, left, and right, a lifting control rod 16 for controlling the ascent and descent of the drone, and a rotation control rod 17 for controlling the clockwise and counterclockwise rotation of the drone.

[0066] In this embodiment, it should be noted that the spatial movement and horizontal rotation of the drone can be controlled by manually operating the remote controller 13, or by programming the flight control chip for automatic control.

[0067] Implementation II

[0068] This embodiment discloses a working method of the drone system in Embodiment 1, which mainly includes the following steps:

[0069] Step 1: Set the lower beam direction of the beam light to face upwards, manually place and adjust the position of the positioning bracket 11 so that the positioning bracket 11 is located directly above the beam light, and place the drone so that the four positioning rods of the drone are located in the corresponding positioning holes 12 on the positioning bracket 11. At this time, the initial state layout is completed, as shown in the figure below: Figure 9-11 shown.

[0070] Step 2: Turn on the drone. Press the switch button 14 on the remote controller 13 to turn on the remote controller 13 , and control the drone to rise to a desired height through the lifting control rod 16 .

[0071] Step 3, turn on the beam light. At this time, because the drone has a positioning accuracy of several centimeters, the center line 10 of the lower beam and the center of the reflector 6 are not completely aligned, and there is a deviation of several centimeters between the two. Manually adjust the horizontal position of the drone through the azimuth adjustment button 15 until the two are aligned. At this time, the reflector lens 7 on the drone reflects the beam of the beam light, and the reflected beam is a number of small beams, producing a unique light visual effect, such as Figure 12-Figure 15 shown.

[0072] Step 4: According to the needs of visual effects, the drone is moved up and down by the lifting control rod 16, and the drone is rotated horizontally by the rotating control rod 17. Both of these movements bring unique light visual effects.

[0073] Step 5: When the performance is over, turn off the beam light, manually place the positioning bracket 11 at the initial position, remotely control the drone to land back on the positioning bracket 11 through the lifting control rod 16; turn off the drone, and press the switch button 14 to turn off the remote controller 13.

[0074] Embodiment 3

[0075] This embodiment discloses another working method of the drone system in the first embodiment, which mainly includes the following steps:

[0076] Step 1: Set the lower beam direction of the beam light to face upwards, manually place and adjust the position of the positioning bracket 11 so that the positioning bracket 11 is located directly above the beam light, and place the drone so that the four positioning rods of the drone are located in the corresponding positioning holes 12 on the positioning bracket 11. At this time, the initial state layout is completed, as shown in the figure below: Figure 9-11 shown.

[0077] Step 2: Turn on the drone. Press the switch button 14 on the remote controller 13 to turn on the remote controller 13 , and control the drone to rise to a desired height through the lifting control rod 16 .

[0078] Step 3, turn on the beam light. At this time, because the drone has a positioning accuracy of several centimeters, the center line 10 of the lower beam and the center of the reflector 6 are not completely aligned, and there is a deviation of several centimeters between the two. Manually adjust the horizontal position of the drone through the azimuth adjustment button 15 until the two are aligned. At this time, the reflector lens 7 on the drone reflects the beam of the beam light, and the reflected beam is a number of small beams, producing a unique light visual effect, such as Figure 12-Figure 15 shown.

[0079] Step 4: According to the needs of visual effects, the remote controller 13 is used to control the drone to move freely in space, and the lower light source 8 automatically adjusts the emission angle to illuminate the reflector 6 in real time; at the same time, the drone can be controlled to rotate horizontally by rotating the control rod 17. The whole movement process brings a more unique light visual effect.

[0080] Step 5: When the performance is over, turn off the beam light, manually place the positioning bracket 11 at the initial position, and use the remote controller 13 to remotely control the drone to land back on the positioning bracket 11; turn off the drone, and press the switch button 14 to turn off the remote controller 13.

[0081] The present invention uses specific examples to illustrate the principle and implementation of the present invention. The above examples are only used to help understand the method and core idea of ​​the present invention. At the same time, for those skilled in the art, according to the idea of ​​the present invention, there will be changes in the specific implementation and application scope. In summary, the content of this specification should not be understood as limiting the present invention.

Claims

1. A light reflection mechanism, characterized in that: include: A lower light source, the lower light source is used to emit a lower light beam to the drone; A reflector is used to be installed on the drone, and the reflector is a three-dimensional structure. A reflective lens is laid on the surface of the reflector to reflect the lower light beam emitted by the lower light source in multiple directions.

2. The reflective lighting mechanism according to claim 1, characterized in that: The reflector is a spherical structure, and the spherical surface of the spherical structure faces downward, and the reflective lens is laid on the spherical surface; Wherein, a plurality of circles of the reflective lenses are sequentially arranged on the spherical surface along its radial direction, and a plurality of the reflective lenses in any circle are evenly distributed along the circumference.

3. The reflective lighting mechanism according to claim 2, characterized in that: The reflector is a spherical structure formed by 3D printing using resin material.

4. The reflective lighting mechanism according to any one of claims 1 to 3, characterized in that: A silver-plated layer is arranged on the reflective surface of the reflective lens.

5. The reflective lighting mechanism according to claim 1, characterized in that: The lower light source is a beam lamp, and the beam lamp is connected to a driving system, and the driving system can drive the beam lamp to follow the rotation of the drone to adjust the angle at which the beam lamp emits the lower light beam.

6. The reflective lighting mechanism according to claim 5, characterized in that: The driving system includes a base, a mounting frame, a first servo motor and a second servo motor, wherein the beam lamp is rotatably mounted on the mounting frame via a horizontal rotating shaft, and the first servo motor is used to drive the beam lamp to rotate around the axis of the horizontal rotating shaft; the mounting frame is rotatably mounted on the base via a vertical rotating shaft, and the second servo motor is used to drive the mounting frame and the beam lamp to rotate around the axis of the vertical rotating shaft.

7. An unmanned aerial vehicle system, characterized in that: It comprises a drone and a reflective lighting mechanism as described in any one of claims 1 to 6; wherein, the drone comprises a drone body, the reflector is installed at the bottom of the drone body, and a plurality of connecting arms are also provided on the drone body, and a propeller is provided at one end of any connecting arm away from the drone body.

8. The UAV system according to claim 7, characterized in that: It also includes a positioning bracket, wherein a central through hole is provided in the middle of the positioning bracket, and a plurality of positioning holes are also provided on the positioning bracket, and the positioning holes are arranged around the central through hole; A driving motor is provided at the top of one end of any of the connecting arms away from the UAV body, and the driving motor is used to drive the corresponding propeller to rotate; and a positioning rod is provided at the bottom of one end of any of the connecting arms away from the UAV body, and the positioning rod is provided in one-to-one correspondence with the positioning hole on the positioning bracket; In the initial state, the positioning bracket is located directly above the lower light source, the positioning rod of the drone body is located in the corresponding positioning hole, and the lower light beam emitted by the lower light source can pass through the central through hole and face the drone body.

9. The UAV system according to claim 7 or 8, characterized in that: The connecting arm is a hollow carbon fiber tube, and one end of the connecting arm away from the UAV body exceeds the reflector.

10. The UAV system according to claim 7, characterized in that: The flight control chip and battery of the drone are both installed in the drone body, and the battery is used to power the drone; a positioning component is also installed on the drone body, and the positioning component is connected to the flight control chip signal to realize the positioning of the drone, and the flight control chip is also connected to the drive system signal of the lower light source; Wherein, the positioning component is a GPS-RTK positioning component, and is installed above the UAV body; The drone system also includes a remote controller, which is connected to the flight control chip signal, wherein the remote controller is provided with a switch button, an azimuth adjustment button, a lifting control lever and a rotating control lever.