Integrated unmanned aerial vehicle command and control square cabin based on multi-screen fusion

Abstract

The invention discloses an integrated unmanned aerial vehicle command and control square cabin based on multi-screen fusion. And a direction panel operating table, a flight control rocker operating table, a keyboard and mouse operating table, a control handle operating table, a middle I-type seat display screen, a middle II-type seat display screen, a middle III-type seat display screen, a track and external view fusion display screen, a dynamic map display screen, a radar display screen and a contact monitoring display screen are arranged in the command and control square cabin. The command and control square cabin is further provided with an equipment integration cabinet and a bottom storage box. The command and control square cabin is further provided with a reinforcing seat. The advanced command and control square cabin has the beneficial effects that the advanced command and control square cabin in an integrated state is jointly constructed by various types of operating tables, display screens, seats, storage spaces, lighting environments and the like.

Description

Technical Field

[0001] The present invention relates to an unmanned aerial vehicle ground station, in particular to an integrated unmanned aerial vehicle command and control cabin based on multi-screen fusion. Background Art

[0002] With the technological development in the field of UAV equipment in recent years, the demand for the development of UAV ground station cabins has increased, and the display and control screens used for interactive control have also increased day by day. The ergonomics problem caused by information redundancy needs to be solved urgently. Taking the conventional display and control content of the UAV ground station as an example, it includes the flight control interface, flight status interface, flight data recording and playback interface, track and dynamic map display interface, link monitoring interface, etc. Among them, the functions related to UAV flight control belong to specific functions, and their information can be displayed independently by each command seat, while the track and dynamic map, as well as the link relationship with other external equipment, belong to the global command function, and its interface content is more suitable for a larger and wider display area, thereby improving the efficiency of multi-seat joint observation and collaboration. The conventional layout of the existing UAV ground station command cabin is composed of a number of independent control consoles and seats to form a command unit, and different command units have multiple display screens. The overly dispersed displays can easily cause the internal layout of the command cabin to be messy, the multi-screen display information is cumbersome, and there is a lack of unified planning, resulting in low efficiency in information reading, recognition and command operation. Summary of the invention

[0003] The purpose of the present invention is to solve the technical problems in the prior art and to provide a novel integrated UAV command and control cabin based on multi-screen fusion.

[0004] In order to achieve the above-mentioned purpose, the technical solution provided by the present invention is: an integrated UAV command and control cabin based on multi-screen fusion, which has a steering wheel operating console, a flight control joystick operating console, a keyboard and mouse operating console, a control handle operating console and the corresponding central type I seat display screen, central type II seat display screen, central type III seat display screen, track and external view fusion display screen, dynamic map display screen, radar display screen and communication monitoring display screen; the command and control cabin further has an equipment integration cabinet and a bottom storage box; the command and control cabin further has an equipment reinforced seat.

[0005] As a preferred solution for an integrated UAV command and control cabin based on multi-screen fusion, the command and control cabin consists of a cabin frame beam and a cabin wall panel. The cabin frame beam is made of high-strength steel profiles, and the cabin wall panel is made of aluminum-plastic alloy plate.

[0006] As a preferred solution for an integrated UAV command and control cabin based on multi-screen fusion, the command and control cabin has a main cabin door, bulkhead ventilation louvers and top ventilation louvers.

[0007] As a preferred solution for an integrated UAV command and control cabin based on multi-screen fusion, the lighting environment of the command and control cabin consists of a top lighting floodlight panel, a top atmosphere light strip, and a bottom atmosphere light strip.

[0008] As a preferred solution for an integrated UAV command and control cabin based on multi-screen fusion, the command and control cabin adopts two ceiling-mounted air conditioners and is integrated into the top decorative panel.

[0009] Compared with the prior art, the beneficial effect of the present invention is at least that: various types of operating tables, display screens, seats, storage spaces, lighting environments, etc. are used to jointly construct an advanced command and control cabin in an integrated state. BRIEF DESCRIPTION OF THE DRAWINGS

[0010] Figure 1 A top view of the integrated UAV command and control cabin based on multi-screen fusion provided in an embodiment of the present invention.

[0011] Figure 2 A front view of an integrated UAV command and control cabin based on multi-screen fusion provided in an embodiment of the present invention.

[0012] Figure 3 A side view of an integrated UAV command and control cabin based on multi-screen fusion provided in an embodiment of the present invention.

[0013] Figure 4 A 45° stereoscopic view of the front side of an integrated drone command and control cabin based on multi-screen fusion provided in an embodiment of the present invention.

[0014] Figure 5 A 45° stereoscopic image of the rear side of the integrated UAV command and control cabin based on multi-screen fusion provided in an embodiment of the present invention.

[0015] Figure 6 A top view of an integrated drone command and control cabin based on multi-screen fusion provided in an embodiment of the present invention. Implementation

[0016] The present invention is further described in detail below by means of specific embodiments in combination with the accompanying drawings. It should be noted that the description of these embodiments is used to help understand the present invention, but does not constitute a limitation of the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other.

[0017] See also Figures 1 to 6 The figure shows an integrated UAV command and control cabin based on multi-screen fusion. The purpose is to solve the problems of the overall layout being messy due to the excessive dispersion of displays in the existing UAV command and control cabin, the cumbersome multi-screen information display, the lack of unified planning, and the low efficiency of information reading and recognition and command and control operations.

[0018] The control cabin 1 is composed of a cabin frame beam 11 and a cabin wall plate 12. The cabin frame beam 11 is made of high-strength steel profiles, and the cabin wall plate 12 is made of aluminum-plastic alloy plate to ensure cabin strength and environmental adaptability.

[0019] The described charging cabin 1 has a main door 13, a bulkhead ventilation louver 14 and a top ventilation louver 15, which ensure the convenience of entering and exiting the cabin and the safety of air circulation in the cabin.

[0020] In order to solve the problem of the messy internal layout and lack of unified planning of the command cabin 1, the command cabin 1 adopts an operation table with a relatively close size and installation position, and fully considers the task requirements and ergonomics, and arranges the steering wheel operation table 211, the flight control rocker operation table 212, the keyboard and mouse operation table 213, the control handle operation table 214 and other operation tables. Correspondingly, the middle type I seat display screen 221, the middle type II seat display screen 222, and the middle type III seat display screen 223 provide display functions for flight control, flight status, flight data, etc., and the operating seats formed can realize waypoint information query, change and entry. The flight status display can obtain the flight status information of the drone by parsing the telemetry data of the drone platform status, and display it in the form of dynamic tables, graphics, etc., to realize the real-time monitoring function of the flight status information. Correspondingly, the track and external view fusion display screen 224 provides a drone observation display function with a wider field of view, thereby providing operators with a more intuitive flight status observation. Correspondingly, the dynamic map display screen 225, the radar display screen 226 and the contact monitoring display screen 227 provide more auxiliary operation display and control functions, including real-time monitoring and control of data link equipment and ground tracking equipment.

[0021] The control cabin 1 further has an equipment integration cabinet 3 and a bottom storage box 4 to improve the utilization rate of the space in the cabin.

[0022] The command cabin 1 is further equipped with reinforced seats 5 corresponding to the seats of each operating table to improve the safety of the seat operating environment.

[0023] The lighting environment of the command cabin 1 is composed of a top lighting floodlight panel 61, a top atmosphere light strip 62, and a bottom atmosphere light strip group 63, providing a lighting environment with functions such as "natural light simulation lighting", "scene lighting", and "alert lighting".

[0024] The control cabin 1 adopts two ceiling-mounted air conditioners 7, which are integrated into the top decorative panel.

[0025] The above only expresses the implementation mode of the present invention, and its description is relatively specific and detailed, but it cannot be understood as limiting the scope of the invention patent. It should be pointed out that for ordinary technicians in this field, several modifications and improvements can be made without departing from the concept of the present invention, which all belong to the protection scope of the present invention. Therefore, the protection scope of the patent of the present invention shall be based on the attached claims.

Claims

1. The integrated UAV command and control cabin based on multi-screen fusion is characterized by: The command cabin is equipped with a steering wheel control panel, a flight control joystick control panel, a keyboard and mouse control panel, a control handle control panel and the corresponding central type I seat display screen, central type II seat display screen, central type III seat display screen, track and external view fusion display screen, dynamic map display screen, radar display screen and communication monitoring display screen; the command cabin further has an equipment integration cabinet and a bottom storage box; the command cabin is further equipped with reinforced seats.

2. The integrated UAV command and control cabin based on multi-screen fusion according to claim 1 is characterized in that: The command cabin is composed of a cabin frame beam and a cabin wall plate. The cabin frame beam is made of high-strength steel profiles, and the cabin wall plate is made of aluminum-plastic alloy plate.

3. The integrated UAV command and control cabin based on multi-screen fusion according to claim 1 is characterized in that: The command cabin has a main cabin door, a bulkhead ventilation louver and a top ventilation louver.

4. The integrated UAV command and control cabin based on multi-screen fusion according to claim 1 is characterized in that: The lighting environment of the command cabin is composed of a top lighting floodlight panel, a top atmosphere light strip, and a bottom atmosphere light strip.

5. The integrated UAV command and control cabin based on multi-screen fusion according to claim 1 is characterized in that: The command cabin adopts two ceiling-mounted air conditioners, which are integrated into the top decorative panel.

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