Aircraft information input device
By designing an aircraft information input device that includes a key input module and a vernier control module based on a pressure sensor, the problem that existing equipment cannot quickly input commands and control cursors is solved, and more efficient interaction between pilots and aircraft is achieved.
Patent Information
- Application Number
- CN202311270454.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2023-09-28
- Publication Date
- 2025-03-28
AI Technical Summary
Existing aircraft information input devices cannot quickly enter commands and cannot control the integrated display cursor, which makes it inconvenient for pilots to control the aircraft.
An aircraft information input device is designed, including a key input module and a cursor control module based on a pressure sensor. The key input module has quick switching, command input, digital input and coordinate quick input functions; the cursor control module uses the pressure sensor to sample the sliding direction and force of the finger to control the movement of the instructor.
It realizes that in the environment of small aircraft space, quickly enter commands and control cursors without travel, improving the efficiency of command interaction between pilots and aircraft.
Smart Images
Figure CN119718092A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to an information input device, in particular to an aircraft information input device. Background Art
[0002] With the development of aircraft cockpit display and control technology, more and more aircraft no longer use instruments + control switches to process and display flight information, but use integrated displays for processing and display. Based on the interactive needs of the aircraft, the pilot inputs different instructions to the aircraft to control the aircraft's attitude, heading, altitude and mission. The current mainstream input form is to use a conventional keyboard. However, the input method of a conventional keyboard is not suitable for the input instructions of the aircraft, and it is impossible to input instructions quickly to control the aircraft, and it does not have the function of controlling the cursor of the integrated display. In view of the above, it is urgent to design a new type of aircraft information input device. Summary of the invention
[0003] The purpose of the present invention is to solve the problem in the prior art that instructions cannot be input quickly and to provide a novel aircraft information input device.
[0004] In order to achieve the above-mentioned purpose, the present invention provides a technical solution: an aircraft information input device, comprising: a key input module, and a cursor control module based on a pressure sensor; the key input module has an interface quick switching key input area, a command input key input area, a number input key input area, a longitude and latitude quick input key input area, an X-coordinate quick input key, and a Y-coordinate quick input key; the cursor control module based on the pressure sensor is used to control the indicating cursor of the display device.
[0005] As a preferred solution for the aircraft information input device, the key input module and the pressure sensor-based cursor control module are arranged up and down.
[0006] As a preferred solution for the aircraft information input device, the input key layout of the key input module is 10 rows × 4 columns; the four input keys in the first row are, from left to right: "Attitude", "Navigation", "Electromechanical", "Plug-in"; the four input keys in the second row are, from left to right: "A", "B", "C", "D"; the four input keys in the third row are, from left to right: "F", "G", "H", "I"; the four input keys in the fourth row are, from left to right: "J", "K", "L", "M"; the four input keys in the fifth row are, from left to right: "O", "P", "Q", "R"; the four input keys in the sixth row are, from left to right: "T", "U", "V", "Z"; the four input buttons in the seventh row are from left to right: "7", "8", "9", "E"; the four input buttons in the eighth row are from left to right: "4", "5", "6", "W"; the four input buttons in the ninth row are from left to right: "1", "2", "3", "S"; the four input buttons in the tenth row are from left to right: "X", "0", "Y", "N"; among them, the input buttons "Posture", "Navigation", "Electromechanical", and "Hook" together constitute the interface quick switching button input area, and the input buttons "Posture", "Navigation", "Electromechanical", and "Hook" are respectively configured as: Switch to the posture setting interface interface, navigation setting interface, electromechanical setting interface, plug-in setting interface; among them, the input buttons "A", "B", "C", "D", "F", "G", "H", "I", "J", "K", "L", "M", "O", "P", "Q", "R", "T", "U", "V", "Z" together constitute the command input button input area; among them, the input buttons "7", "8", "9", "4", "5", "6", "1", "2", "3", "0" together constitute the digital input button input area; among them, the input buttons "E", "W", "S", "N" together constitute the longitude and latitude shortcut input button input area, the longitude and latitude shortcut input button The input area is configured as follows: by pressing any input button, the input mode is switched to the longitude and latitude input mode, and the input buttons in the numeric input button input area can be used directly to quickly input the longitude and latitude; wherein, the input button "X" constitutes an X-coordinate quick input button, and the X-coordinate quick input button is configured as follows: by pressing the input button, the input mode is switched to the X-coordinate input mode, and the input buttons in the numeric input button input area can be used directly to quickly input the X-coordinate; wherein, the input button "Y" constitutes a Y-coordinate quick input button, and the Y-coordinate quick input button is configured as follows: by pressing the input button, the input mode is switched to the Y-coordinate input mode, and the input buttons in the numeric input button input area can be used directly to quickly input the Y-coordinate.
[0007] As a preferred solution for the aircraft information input device, the control method of the cursor control module based on the pressure sensor includes: sampling the pressure direction and pressure intensity acting on the pressure sensor; and determining the moving direction and moving speed of the indicating cursor based on the pressure direction and pressure intensity.
[0008] The present invention also provides an aircraft information input device, comprising: an input device key area and an input device touch area; the input device key area has an interface quick switching key area, a command input key area, a number input key area, a longitude and latitude quick input key area, an X-coordinate quick input key, and a Y-coordinate quick input key; the input device touch area is used to control an indication cursor of a display device.
[0009] As a preferred solution for the aircraft information input device, the input device key area and the input device touch area are arranged up and down.
[0010] As a preferred solution for the aircraft information input device, the input key layout of the input device key area is 10 rows × 4 columns; the four input keys in the first row are, from left to right: "Attitude", "Navigation", "Electromechanical", and "External Plug-in"; the four input keys in the second row are, from left to right: "A", "B", "C", and "D"; the four input keys in the third row are, from left to right: "F", "G", "H", and "I"; the four input keys in the fourth row are, from left to right: "J", "K", "L", and "M"; the four input keys in the fifth row are, from left to right: "O", "P", "Q", and "R"; the four input keys in the sixth row are, from left to right: The four input keys in the seventh row are from left to right: "7", "8", "9", "E"; the four input keys in the eighth row are from left to right: "4", "5", "6", "W"; the four input keys in the ninth row are from left to right: "1", "2", "3", "S"; the four input keys in the tenth row are from left to right: "X", "0", "Y", "N"; among them, the input keys "posture", "navigation", "electromechanical" and "plug-in" together constitute the interface quick switching key area, and the input keys "posture", "navigation", "electromechanical" and "plug-in" are respectively configured as: switch to posture The state setting interface, navigation setting interface, electromechanical setting interface, and plug-in setting interface; among them, the input buttons "A", "B", "C", "D", "F", "G", "H", "I", "J", "K", "L", "M", "O", "P", "Q", "R", "T", "U", "V", and "Z" together constitute the command input button area; among them, the input buttons "7", "8", "9", "4", "5", "6", "1", "2", "3", and "0" together constitute the number input button area; among them, the input buttons "E", "W", "S", and "N" together constitute the longitude and latitude shortcut input button area, and the longitude and latitude shortcut input button area The input key area is configured as follows: by pressing any input key, the mode of longitude and latitude input is switched, and the input keys in the numeric input key area can be used directly to quickly input longitude and latitude; wherein, the input key "X" constitutes an X-coordinate quick input key, and the X-coordinate quick input key is configured as follows: by pressing the input key, the mode of longitude and latitude input is switched, and the input keys in the numeric input key area can be used directly to quickly input X-coordinate; wherein, the input key "Y" constitutes a Y-coordinate quick input key, and the Y-coordinate quick input key is configured as follows: by pressing the input key, the mode of longitude and latitude input is switched, and the input keys in the numeric input key area can be used directly to quickly input Y-coordinate.
[0011] As a preferred solution of the aircraft information input device, the touch control area of the input device has a touch screen, and the touch screen is configured to control an indicating cursor.
[0012] As a preferred solution for the aircraft information input device, the control method of the indicating cursor includes: sampling the finger sliding direction and finger sliding force acting on the touch screen; and determining the moving direction and moving speed of the indicating cursor based on the finger sliding direction and finger sliding force.
[0013] Compared with the prior art, the beneficial effects of the present invention are at least that: the functional modules commonly used under aircraft flight conditions are integrated, a quick input method for such functional modules is set, and through cursor control based on a pressure sensor or a touch screen, the cursor can be controlled without travel under the premise of a small aircraft space, thereby better solving the problem of command interaction between the pilot and the aircraft. BRIEF DESCRIPTION OF THE DRAWINGS
[0014] Figure 1 This is a schematic diagram of the structure of Example 1 of the present invention.
[0015] Figure 2 This is a schematic diagram of the structure of Example 2 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 each embodiment of the present invention described below can be combined with each other as long as they do not conflict with each other. Example
[0017] See also Figure 1 , the figure shows an aircraft information input device. The aircraft information input device is arranged in the aircraft cockpit and is used for aircraft information input.
[0018] The aircraft information input device includes: a key input module and a cursor control module based on a pressure sensor. Preferably, the key input module and the cursor control module based on a pressure sensor are arranged up and down.
[0019] The input key layout of the key input module is 10 rows×4 columns.
[0020] The four input buttons in the first row are from left to right: "Attitude", "Navigation", "Electromechanical", and "Plug-in".
[0021] The four input buttons in the second row are from left to right: "A", "B", "C", and "D".
[0022] The four input keys in the third row are from left to right: "F", "G", "H", and "I".
[0023] The four input keys in the fourth row are, from left to right: "J", "K", "L", and "M".
[0024] The four input keys in the fifth row are, from left to right: “O”, “P”, “Q”, and “R”.
[0025] The four input keys in the sixth row are, from left to right: "T", "U", "V", "Z". The four input keys in the seventh row are, from left to right: "7", "8", "9", "E".
[0026] The four input keys in the eighth row are, from left to right: “4”, “5”, “6”, and “W”.
[0027] The four input keys in the ninth row are, from left to right: “1”, “2”, “3”, and “S”.
[0028] The four input buttons in the tenth row are, from left to right: "X", "0", "Y", and "N".
[0029] Among them, the input buttons "posture", "navigation", "electromechanical", and "plug-in" together constitute the interface quick switching button input area 1. The input buttons "posture", "navigation", "electromechanical", and "plug-in" are respectively configured to: switch to the posture setting interface, the navigation setting interface, the electromechanical setting interface, and the plug-in setting interface.
[0030] Among them, the input keys "A", "B", "C", "D", "F", "G", "H", "I", "J", "K", "L", "M", "O", "P", "Q", "R", "T", "U", "V", and "Z" together constitute the command input key input area 2.
[0031] Among them, the input keys "7", "8", "9", "4", "5", "6", "1", "2", "3", and "0" together constitute the digital input key input area 3.
[0032] Among them, the input keys "E", "W", "S" and "N" together constitute the longitude and latitude quick input key input area 4. The longitude and latitude quick input key input area is configured as follows: by pressing any input key, the longitude and latitude input mode is switched to, and the input keys of the digital input key input area can be directly used to quickly input the longitude and latitude.
[0033] The input key "X" constitutes the X-coordinate quick input key 5. The X-coordinate quick input key is configured such that: by pressing the input key, the X-coordinate input mode is switched to, and the input keys in the numeric input key input area can be used to quickly input the X-coordinate.
[0034] The input key "Y" constitutes the Y coordinate quick input key 6. The Y coordinate quick input key is configured such that: by pressing the input key, the input mode is switched to the Y coordinate input mode, and the input keys in the numeric input key input area can be used to quickly input the Y coordinate.
[0035] The cursor control module 7 based on the pressure sensor is used to control the indicating cursor of the display device. The pressure sensor can be a pressure sensor with an i²C communication function. The pressure sensor can control the moving direction and moving speed of the indicating cursor by sampling the pressure action direction and the pressure action strength. The control method of the indicating cursor includes: sampling the pressure action direction and the pressure action strength acting on the pressure sensor; determining the moving direction and moving speed of the indicating cursor based on the pressure action direction and the pressure action strength. Among them, the moving direction of the indicating cursor corresponds to the pressure action direction, and the moving speed of the indicating cursor corresponds to the pressure action strength (the greater the strength, the faster the moving speed).
[0036] The aircraft information input device integrates the commonly used functional modules under the flight conditions of the aircraft, sets a quick input method for such functional modules, and through the cursor control based on the touch screen, it can control the indicating cursor without travel under the premise of small space in the aircraft, and better solves the problem of command interaction between the pilot and the aircraft. Example
[0037] See also Figure 2 , the figure shows an aircraft information input device. The aircraft information input device is arranged in the aircraft cockpit and is used for aircraft information input.
[0038] The aircraft information input device comprises: an input device key area and an input device touch area. Preferably, the input device key area and the input device touch area are arranged vertically.
[0039] The input key layout of the input device key area is 10 rows×4 columns.
[0040] The four input buttons in the first row are from left to right: "Attitude", "Navigation", "Electromechanical", and "Plug-in".
[0041] The four input buttons in the second row are from left to right: "A", "B", "C", and "D".
[0042] The four input keys in the third row are from left to right: "F", "G", "H", and "I".
[0043] The four input keys in the fourth row are, from left to right: "J", "K", "L", and "M".
[0044] The four input keys in the fifth row are, from left to right: “O”, “P”, “Q”, and “R”.
[0045] The four input keys in the sixth row are, from left to right: "T", "U", "V", "Z". The four input keys in the seventh row are, from left to right: "7", "8", "9", "E".
[0046] The four input keys in the eighth row are, from left to right: “4”, “5”, “6”, and “W”.
[0047] The four input keys in the ninth row are, from left to right: “1”, “2”, “3”, and “S”.
[0048] The four input buttons in the tenth row are, from left to right: "X", "0", "Y", and "N".
[0049] Among them, the input buttons "posture", "navigation", "electromechanical", and "plug-in" together constitute the interface quick switching button area 1. The input buttons "posture", "navigation", "electromechanical", and "plug-in" are respectively configured to: switch to the posture setting interface, the navigation setting interface, the electromechanical setting interface, and the plug-in setting interface.
[0050] Among them, the input keys "A", "B", "C", "D", "F", "G", "H", "I", "J", "K", "L", "M", "O", "P", "Q", "R", "T", "U", "V", and "Z" together constitute the command input key area 2.
[0051] Among them, the input keys "7", "8", "9", "4", "5", "6", "1", "2", "3", and "0" together constitute the digital input key area 3.
[0052] Among them, the input keys "E", "W", "S" and "N" together constitute the longitude and latitude quick input key area 4. The longitude and latitude quick input key area is configured so that: by pressing any input key, the longitude and latitude input mode is switched to, and the input keys in the number input key area can be directly used to quickly input longitude and latitude.
[0053] The input key "X" constitutes the X-coordinate quick input key 5. The X-coordinate quick input key is configured such that: by pressing the input key, the X-coordinate input mode is switched to, and the input keys in the numeric input key area can be used to quickly input the X-coordinate.
[0054] The input key "Y" constitutes the Y coordinate quick input key 6. The Y coordinate quick input key is configured such that: by pressing the input key, the input mode is switched to the Y coordinate input mode, and the input keys in the numeric input key area can be used to quickly input the Y coordinate.
[0055] The input device touch area 7 is used to control the indicator cursor of the display device. The input device touch area has a touch screen. The touch screen can perform peripheral communication based on CAN or other communication methods. The touch screen is configured to: control the indicator cursor. The control method of the indicator cursor includes: sampling the finger sliding direction and finger sliding force acting on the touch screen; determining the moving direction and moving speed of the indicator cursor based on the finger sliding direction and finger sliding force. Among them, the moving direction of the indicator cursor corresponds to the finger sliding direction, and the moving speed of the indicator cursor corresponds to the finger sliding force (the greater the force, the faster the moving speed).
[0056] The aircraft information input device integrates the commonly used functional modules under the flight conditions of the aircraft, sets a quick input method for such functional modules, and through the cursor control based on the touch screen, it can control the indicating cursor without travel under the premise of small space in the aircraft, and better solves the problem of command interaction between the pilot and the aircraft.
[0057] 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. An aircraft information input device, characterized in that: include: A key input module and a cursor control module based on a pressure sensor; the key input module has an interface quick switching key input area, a command input key input area, a number input key input area, a longitude and latitude quick input key input area, an X-coordinate quick input key, and a Y-coordinate quick input key; the cursor control module based on a pressure sensor is used to control the indicating cursor of the display device.
2. The aircraft information input device according to claim 1, characterized in that: The key input module and the pressure sensor-based cursor control module are arranged vertically.
3. The aircraft information input device according to claim 1, characterized in that: The input key layout of the key input module is 10 rows × 4 columns; the four input keys in the first row are, from left to right: "Posture", "Navigation", "Electromechanical", and "Plug-in"; the four input keys in the second row are, from left to right: "A", "B", "C", and "D"; the four input keys in the third row are, from left to right: "F", "G", "H", and "I"; the four input keys in the fourth row are, from left to right: "J", "K", "L", and "M"; the four input keys in the fifth row are, from left to right: "O ", "P", "Q", "R"; the four input keys in the sixth row are, from left to right: "T", "U", "V", "Z"; the four input keys in the seventh row are, from left to right: "7", "8", "9", "E"; the four input keys in the eighth row are, from left to right: "4", "5", "6", "W"; the four input keys in the ninth row are, from left to right: "1", "2", "3", "S"; the four input keys in the tenth row are, from left to right: "X", "0", "Y", "N"; Among them, the input buttons "Posture", "Navigation", "Electromechanical", and "Hook" together constitute the interface quick switching button input area, and the input buttons "Posture", "Navigation", "Electromechanical", and "Hook" are respectively configured to: switch to the posture setting interface, the navigation setting interface, the electromechanical setting interface, and the hook setting interface; among them, the input buttons "A", "B", "C", "D", "F", "G", "H", "I", "J", "K", "L", "M", "O", "P", "Q", "R", "T", "U", "V", and "Z" together constitute the command input button input area; among them, the input buttons "7", "8", "9", "4", "5", "6", "1", "2", "3", and "0" together constitute the number input button input area; among them, the input buttons " "E", "W", "S", and "N" together constitute the longitude and latitude quick input key input area, and the longitude and latitude quick input key input area is configured as follows: pressing any input key switches to the longitude and latitude input mode, and the input keys in the numeric input key input area can be used directly to quickly input the longitude and latitude; wherein, the input key "X" constitutes the X coordinate quick input key, and the X coordinate quick input key is configured as follows: pressing the input key switches to the X coordinate input mode, and the input keys in the numeric input key input area can be used directly to quickly input the X coordinate; wherein, the input key "Y" constitutes the Y coordinate quick input key, and the Y coordinate quick input key is configured as follows: pressing the input key switches to the Y coordinate input mode, and the input keys in the numeric input key input area can be used directly to quickly input the Y coordinate.
4. The aircraft information input device according to any one of claims 1 to 3, characterized in that: The control method of the cursor control module based on the pressure sensor includes: sampling the pressure direction and pressure intensity acting on the pressure sensor; and determining the moving direction and moving speed of the indicating cursor based on the pressure direction and pressure intensity.
5. An aircraft information input device, characterized in that: include: An input device key area and an input device touch area; the input device key area has an interface quick switching key area, a command input key area, a number input key area, a latitude and longitude quick input key area, an X coordinate quick input key, and a Y coordinate quick input key; the input device touch area is used to control the indicator cursor of the display device.
6. The aircraft information input device according to claim 5, characterized in that: The input device key area and the input device touch area are arranged vertically.
7. The aircraft information input device according to claim 5, characterized in that: The input key layout of the input device key area is 10 rows × 4 columns; the four input keys in the first row are, from left to right: "Posture", "Navigation", "Electromechanical", and "Plug-in"; the four input keys in the second row are, from left to right: "A", "B", "C", and "D"; the four input keys in the third row are, from left to right: "F", "G", "H", and "I"; the four input keys in the fourth row are, from left to right: "J", "K", "L", and "M"; the four input keys in the fifth row are, from left to right: "O ", "P", "Q", "R"; the four input keys in the sixth row are, from left to right: "T", "U", "V", "Z"; the four input keys in the seventh row are, from left to right: "7", "8", "9", "E"; the four input keys in the eighth row are, from left to right: "4", "5", "6", "W"; the four input keys in the ninth row are, from left to right: "1", "2", "3", "S"; the four input keys in the tenth row are, from left to right: "X", "0", "Y", "N"; Among them, the input buttons "Posture", "Navigation", "Electromechanical", and "Plug-in" together constitute the interface quick switching button area, and the input buttons "Posture", "Navigation", "Electromechanical", and "Plug-in" are respectively configured to: switch to the posture setting interface, the navigation setting interface, the electromechanical setting interface, and the plug-in setting interface; among them, the input buttons "A", "B", "C", "D", "F", "G", "H", "I", "J", "K", "L", "M", "O", "P", "Q", "R", "T", "U", "V", and "Z" together constitute the command input button area; among them, the input buttons "7", "8", "9", "4", "5", "6", "1", "2", "3", and "0" together constitute the digital input button area; among them, the input buttons "E", "W", "S", and "N" together constitute the longitude and latitude quick input key area, and the longitude and latitude quick input key area is configured as follows: pressing any input key switches to the longitude and latitude input mode, and the input keys in the numeric input key area can be used directly to quickly input the longitude and latitude; among them, the input key "X" constitutes the X coordinate quick input key, and the X coordinate quick input key is configured as follows: pressing the input key switches to the X coordinate input mode, and the input keys in the numeric input key area can be used directly to quickly input the X coordinate; among them, the input key "Y" constitutes the Y coordinate quick input key, and the Y coordinate quick input key is configured as follows: pressing the input key switches to the Y coordinate input mode, and the input keys in the numeric input key area can be used directly to quickly input the Y coordinate.
8. The aircraft information input device according to claim 5 or 7, characterized in that: The touch control area of the input device has a touch control screen, and the touch control screen is configured to control a pointing cursor.
9. The aircraft information input device according to claim 8, characterized in that: The control method of the pointing cursor includes: sampling a finger sliding direction and a finger sliding force acting on the touch screen; and determining a moving direction and a moving speed of the pointing cursor based on the finger sliding direction and the finger sliding force.