CN-122015799-A - Flight navigation method, device, equipment and storage medium

CN122015799ACN 122015799 ACN122015799 ACN 122015799ACN-122015799-A

Abstract

The embodiment of the invention provides a flight navigation method, a device, equipment and a storage medium, wherein the method comprises the steps of controlling a user interface associated with an in-flight body to work in a first display mode when the in-flight body does not detect an obstacle, enabling the user interface in the first display mode to display a satellite map and flight information of the in-flight body, controlling the user interface to work in a second display mode when the in-flight body detects the obstacle, and enabling the user interface in the second display mode to display a three-dimensional map and obstacle prompt information of a flight environment where the in-flight body is located, wherein the obstacle prompt information is used for early warning the obstacle.

Inventors

GUAN CHAOXIONG
JI JIE
LI FAHONG

Assignees

广东汇天航空航天科技有限公司

Dates

Publication Date: 20260512
Application Date: 20241109

Claims (13)

1. A method of navigating a flight, comprising: When an in-flight flying body does not detect an obstacle, controlling a user interface associated with the flying body to work in a first display mode; And when the flying body detects an obstacle in the flying process, controlling the user interface to work in a second display mode, wherein the user interface in the second display mode displays a three-dimensional map of the flying environment where the flying body is located and obstacle prompt information, and the obstacle prompt information is used for early warning the obstacle.
2. The method of claim 1, wherein the user interface in the first display mode further displays the three-dimensional map with a display area that is smaller than a display area that is occupied by the satellite map, and/or wherein the user interface in the second display mode further displays the satellite map with a display area that is smaller than a display area that is occupied by the three-dimensional map.
3. The method according to claim 2, wherein the method further comprises: when the user interface is in the first display mode, if an instruction generated by triggering the three-dimensional map is received, controlling the user interface to work in the second display mode; And/or the number of the groups of groups, And when the user interface is in the second display mode, if an instruction generated by triggering the satellite map is received, controlling the user interface to work in the first display mode.
4. The method according to claim 1, wherein the method further comprises: Determining an early warning level of the obstacle according to the distance between the flying body and the obstacle when the user interface is in the second display mode; and controlling the display state of the obstacle according to the early warning level of the obstacle.
5. The method of claim 4, wherein the step of determining the pre-warning level of the obstacle based on the distance between the flying body and the obstacle comprises: Determining the early warning level of the obstacle as a first early warning when the distance between the flying body and the obstacle is greater than a first distance threshold and less than or equal to a second distance threshold, determining the early warning level of the obstacle as a second early warning when the distance between the flying body and the obstacle is less than or equal to the first distance threshold, or Determining the obstacle avoidance distance of the flying body according to the flying speed of the flying body, determining the early warning level of the obstacle as a first early warning when the sum of the distance between the flying body and the obstacle avoidance distance is larger than a first distance threshold and smaller than or equal to a second distance threshold, determining the early warning level of the obstacle as a second early warning when the sum of the distance between the flying body and the obstacle avoidance distance is smaller than or equal to the first distance threshold, or Determining the residual obstacle avoidance time of the flying body according to the flying speed of the flying body and the distance between the flying body and the obstacle, determining the early warning level of the obstacle as a first early warning when the residual obstacle avoidance time is larger than a first time threshold and smaller than or equal to a second time threshold, and determining the early warning level of the obstacle as a second early warning when the residual obstacle avoidance time is smaller than or equal to the first time threshold; The emergency degree of the secondary early warning is higher than that of the primary early warning.
6. The method of claim 5, wherein the step of controlling the display state of the obstacle according to the pre-warning level of the obstacle comprises: and controlling the obstacle to display the frequency and/or the color corresponding to the early warning level.
7. The method of claim 4, wherein the obstacle cue information comprises at least one of a forward course area of the flying body, a distance between the flying body and the obstacle, and an early warning cue; in the step of controlling the display state of the obstacle according to the early warning level of the obstacle, the display state of the obstacle prompt information is also controlled according to the early warning level of the obstacle.
8. The method of claim 1, wherein upon detection of an obstacle by the flying body in flight, the method further comprises: And when the obstacle avoidance control instruction is received, predicting an obstacle avoidance path of the flying body according to the obstacle avoidance control instruction, and displaying the obstacle avoidance path on a user interface in the second display mode.
9. The method of claim 8, wherein after the user interface in the second display mode presents the obstacle avoidance path, the method further comprises: When an instruction generated by adjusting the obstacle avoidance path is received, determining position information of the selected path point in the obstacle avoidance path after adjustment; and updating the obstacle avoidance path according to the position information of the unselected path points in the obstacle avoidance path and the position information adjusted by the selected path points, and displaying the updated obstacle avoidance path on a user interface in the second display mode.
10. The method according to any one of claims 1-9, further comprising: When the flying body in flight is in a take-off state, controlling the user interface to work in a third display mode, wherein the user interface in the third display mode displays a three-dimensional map of the take-off environment of the flying body, the current height of the flying body and the target height of the flying body; accordingly, when the user interface is operated in the first display mode or the second display mode, the flying body in flight is not in a take-off state.
11. A flying navigation device, comprising: A control module configured to: controlling a user interface associated with an in-flight flying body to operate in a first display mode when no obstacle is detected by the flying body, the user interface in the first display mode exhibiting a satellite map and a flight trajectory of the flying body, and And when the flying body detects an obstacle in the flying process, controlling the user interface to work in a second display mode, wherein the user interface in the second display mode displays a three-dimensional map of the flying environment where the flying body is located and obstacle prompt information, and the obstacle prompt information is used for early warning the obstacle.
12. An electronic device comprising a processor and a memory, the memory storing machine executable instructions executable by the processor to implement the method of any one of claims 1-10.
13. A computer readable storage medium, on which a computer program is stored, which computer program, when being executed by a processor, implements the method according to any one of claims 1-10.

Description

Flight navigation method, device, equipment and storage medium Technical Field The invention relates to the technical field of flying bodies, in particular to a flying navigation method, a device, equipment and a storage medium. Background In order to improve the safety of a manned aircraft during the flight, a plurality of display screens are generally configured in the cockpit of the manned aircraft, and different information is displayed on different display screens, as shown in fig. 1, fig. 1 is a schematic diagram of the cockpit display screen of the manned aircraft in the related art. Therefore, the information arranged in the display screen of the cockpit of the manned aircraft at present is too much, so that a driver cannot pay attention to the information with high emergency degree in time, for example, when the situation that an obstacle appears in front of the manned aircraft is assumed, the driver cannot pay attention to the situation of the obstacle in time due to the fact that the information displayed by the display screen is too much and is not emphasized, and then safety accidents are caused. Disclosure of Invention In view of the above, the present invention aims to at least solve the technical problem of low flight safety of the flying body caused by too much information arranged in the cockpit display screen of the existing manned flying body and no important distinction. In order to achieve the above object, the technical scheme adopted by the embodiment of the invention is as follows: in a first aspect of an embodiment of the present invention, a flight navigation method is provided, including: when an in-flight flying body does not detect an obstacle, controlling a user interface associated with the flying body to work in a first display mode; And when the flying body detects an obstacle in the flying process, controlling the user interface to work in a second display mode, wherein the user interface in the second display mode displays a three-dimensional map of the flying environment where the flying body is located and obstacle prompt information, and the obstacle prompt information is used for early warning the obstacle. In an optional implementation manner, the user interface in the first display mode further displays the three-dimensional map, wherein the display area occupied by the three-dimensional map is smaller than the display area occupied by the satellite map, and/or the user interface in the second display mode further displays the satellite map, and the display area occupied by the satellite map is smaller than the display area occupied by the three-dimensional map. In an alternative embodiment, the method further comprises: when the user interface is in the first display mode, if an instruction generated by triggering the three-dimensional map is received, controlling the user interface to work in the second display mode; And/or the number of the groups of groups, And when the user interface is in the second display mode, if an instruction generated by triggering the satellite map is received, controlling the user interface to work in the first display mode. In an alternative embodiment, the method further comprises: Determining an early warning level of the obstacle according to the distance between the flying body and the obstacle when the user interface is in the second display mode; and controlling the display state of the obstacle according to the early warning level of the obstacle. In an alternative embodiment, the step of determining the pre-warning level of the obstacle according to the distance between the flying body and the obstacle includes: Determining the early warning level of the obstacle as a first early warning when the distance between the flying body and the obstacle is greater than a first distance threshold and less than or equal to a second distance threshold, determining the early warning level of the obstacle as a second early warning when the distance between the flying body and the obstacle is less than or equal to the first distance threshold, or Determining the obstacle avoidance distance of the flying body according to the flying speed of the flying body, determining the early warning level of the obstacle as a first early warning when the sum of the distance between the flying body and the obstacle avoidance distance is larger than a first distance threshold and smaller than or equal to a second distance threshold, determining the early warning level of the obstacle as a second early warning when the sum of the distance between the flying body and the obstacle avoidance distance is smaller than or equal to the first distance threshold, or Determining the residual obstacle avoidance time of the flying body according to the flying speed of the flying body and the distance between the flying body and the obstacle, determining the early warning level of the obstacle as a first early warning when the residual obstacle avoidance time is larger