CN-122008915-A - Method, device, electronic equipment and program product for assisting in air power supply of aerocar

CN122008915ACN 122008915 ACN122008915 ACN 122008915ACN-122008915-A

Abstract

The invention discloses an air electricity supplementing and assisting method, device, electronic equipment and program product for a flying car, wherein when the residual electric quantity of a target flying car is insufficient, an electricity supplementing and assisting request is generated according to equipment identification, a first current position, a current flying path and the residual electric quantity, and the electricity supplementing and assisting request is uploaded to a cloud platform; the method comprises the steps of obtaining an assisting aerocar through cloud platform matching, determining a corresponding air merging position, sending a device identifier and the air merging position to the assisting aerocar through the cloud platform, returning the air merging position to a target aerocar, determining an optimal flight path and expected arrival time according to the air merging position through the assisting aerocar, sending the expected arrival time to the target aerocar, and controlling the assisting aerocar to be in air butt joint with the target aerocar and supplementing electricity when the assisting aerocar and the target aerocar reach the air merging position. The invention improves the running safety and reliability of the aerocar and can be applied to the technical field of aerocars.

Inventors

ZHAN XIAOZHI
DONG HAOXUAN
Zhai youbang

Assignees

广汽本田汽车有限公司
广汽本田汽车研究开发有限公司

Dates

Publication Date: 20260512
Application Date: 20260310

Claims (10)

1. The air electricity supplementing assisting method for the aerocar is characterized by comprising the following steps of: When the residual electric quantity of the target flying automobile is insufficient, generating a power-supplementing help request according to the equipment identifier, the first current position, the current flying path and the residual electric quantity of the target flying automobile, and uploading the power-supplementing help request to a cloud platform; matching the cloud platform according to the power-up help request to obtain a help aerocar, and determining a corresponding air merging position; issuing the equipment identifier and the air merging position to the aid aerocar through the cloud platform, and returning the air merging position to the target aerocar; Determining an optimal flight path and an estimated arrival time according to the air merging position by the aid aerocar, and sending the estimated arrival time to the target aerocar according to the equipment identifier; when the aid aerocar and the target aerocar reach the air converging position, controlling the aid aerocar and the target aerocar to carry out air butt joint, and supplementing electricity to the target aerocar through the aid aerocar.
2. The method for assisting the electric power supplement of the air of the aerocar according to claim 1, wherein the assisting aerocar is obtained by matching according to the electric power supplement request, and the method specifically comprises the following steps: Determining the battery capacity of the target aerocar according to the equipment identifier, and determining the required electric quantity of the target aerocar according to the battery capacity and the residual electric quantity; Determining a plurality of alternative aerocars of a corresponding airspace according to the first current position and the current flight path, and determining a second current position and residual power supplementing capacity of each alternative aerocar; Determining the position matching degree of each alternative aerocar according to the second current position and the first current position, and determining the electric power supplementing capability matching degree of each alternative aerocar according to the residual electric power supplementing capability and the required electric quantity; the position matching degree and the power supplementing capability matching degree are weighted and summed according to preset weight parameters, and the comprehensive matching degree of each alternative aerocar is obtained; and determining the alternative aerocar with the highest comprehensive matching degree as the aid aerocar.
3. A method of assisting in the air-lift power supply of a flying vehicle according to claim 1, characterized in that said determining the corresponding air junction position comprises in particular: determining a flying distance of the target flying automobile according to the residual electric quantity, and determining a farthest flying position of the target flying automobile on the current flying path according to the first current position and the flying distance; Determining a combinable position interval on the current flight path according to the first current position and the farthest flight position, and determining a plurality of candidate merging positions according to the combinable position interval; determining an assistance flight distance of the assistance-flying vehicle according to the candidate merging position and a second current position of the assistance-flying vehicle; and determining the candidate merging position which makes the aid flight distance shortest as the air merging position.
4. A method of air-assisted power assistance for a flying vehicle according to claim 1, wherein said determining an optimal flight path and an estimated time of arrival from said air junction location comprises: Determining weather condition information, air traffic information and airspace control information corresponding to the airspace according to the air merging position and the second current position of the aid flying vehicle; carrying out flight path planning on the assisted flight vehicle according to the meteorological condition information, the air traffic information and the airspace control information to obtain a plurality of candidate flight paths; Determining the path smoothness, the flying height change rate and the flying energy consumption of each candidate flying path, and determining the priority of each candidate flying path according to the path smoothness, the flying height change rate and the flying energy consumption; and determining the candidate flight path with the highest priority as the optimal flight path, and determining the expected arrival time according to the optimal flight path and the flight speed of the auxiliary flying automobile.
5. The method for assisting in the air power supply of a flying car according to claim 1, wherein the step of controlling the assisting flying car to perform the air docking with the target flying car and performing the power supply of the target flying car through the assisting flying car specifically comprises the following steps: controlling the assisting aerocar and the target aerocar to conduct gesture alignment through a relative motion coordination system until the assisting aerocar and the target aerocar keep relatively static; The air docking of the aid aerocar and the target aerocar is realized through a mechanical docking mechanism; and determining the charging parameters of the target aerocar according to the equipment identification, and controlling the electric energy transmission device of the aid aerocar to supplement electricity to the target aerocar according to the charging parameters.
6. The method according to claim 5, wherein the relative motion coordination system comprises a laser radar positioning unit, an inertia measurement unit and a flight control coordination unit, wherein the laser radar positioning unit is used for determining the relative position and the relative speed of the aid aerocar and the target aerocar, the inertia measurement unit is used for determining attitude change data of the aid aerocar and the target aerocar, and the flight control coordination unit is used for adjusting the flight attitudes of the aid aerocar and the target aerocar through a PID control algorithm according to the relative position, the relative speed and the attitude change data.
7. A method of air-lift power assistance for a flying car as claimed in any one of claims 1 to 6, further comprising the steps of: And stopping supplementing electricity when the battery electric quantity of the target flying automobile reaches a preset electric quantity threshold value or the electric energy transmission device of the assisting flying automobile reaches a preset upper output limit, and feeding back electricity supplementing completion information to the cloud platform through the assisting flying automobile.
8. An air electricity supplementing aid device for a flying automobile, comprising: The power-supplementing help-seeking module is used for generating a power-supplementing help-seeking request according to the equipment identifier, the first current position, the current flight path and the residual electric quantity of the target flight automobile when the residual electric quantity of the target flight automobile is insufficient, and uploading the power-supplementing help-seeking request to a cloud platform; The auxiliary aerocar matching module is used for obtaining an auxiliary aerocar through matching of the cloud platform according to the power-supplementing help request and determining a corresponding air merging position; the power supply task issuing module is used for issuing the equipment identifier and the air merging position to the aid aerocar through the cloud platform and returning the air merging position to the target aerocar; the flight path planning module is used for determining an optimal flight path and expected arrival time according to the air converging position through the aid aerocar and sending the expected arrival time to the target aerocar according to the equipment identifier; And the aerial electricity supplementing module is used for controlling the auxiliary aerocar to be in aerial butt joint with the target aerocar when the auxiliary aerocar and the target aerocar reach the aerial merging position, and supplementing electricity to the target aerocar through the auxiliary aerocar.
9. An electronic device, comprising: At least one processor; at least one memory for storing at least one program; When the at least one program is executed by the at least one processor, the at least one processor is caused to implement a method of electric power assisted in the air of a flying car as claimed in any one of claims 1 to 7.
10. A computer program product comprising a computer program, characterized in that the computer program, when executed by a processor, implements a method of electric power supply in the air for a flying car according to any one of claims 1 to 7.

Description

Method, device, electronic equipment and program product for assisting in air power supply of aerocar Technical Field The invention relates to the technical field of aero-automobiles, in particular to an air electricity supplementing and assisting method, an air electricity supplementing and assisting device, electronic equipment and a program product for the aero-automobiles. Background With the rapid development of low-altitude economy, aerocars are gradually spreading as vehicles with double functions of ground running and low-altitude flight. The operation of the aerocar depends on the electric energy provided by the power battery, however, the aerocar is limited by the current battery energy density and endurance technology, and the aerocar is extremely easy to have the condition of electric quantity emergency under long-distance flight or high-load operation scenes. In the prior art, the electricity supplementing of the aerocar mainly depends on a fixed ground electricity supplementing station or an electricity supplementing facility matched with an air parking apron, when the sudden electric quantity of the aerocar is urgent in the flight process, and the nearest electricity supplementing station exceeds the endurance range of the residual electric quantity, the emergency landing risk is faced, the life safety of drivers and passengers is threatened, and potential safety hazards are possibly caused to ground personnel and facilities. Therefore, there is a need to design a scheme capable of rapidly responding to the air electric quantity emergency requirement of the aerocar and realizing safe and efficient air electricity supplement. Disclosure of Invention The present invention aims to solve at least one of the technical problems existing in the prior art to a certain extent. Therefore, an object of the embodiment of the invention is to provide an air electricity supplementing assistance method for a flying car, which solves the emergency electricity supplementing problem when the electric quantity of the flying car is urgent and the electricity supplementing station cannot be reached in the flying process, realizes the full-flow closed-loop guarantee from the issuing of help to the completion of electricity supplementing, and improves the running safety and reliability of the flying car. Another object of the embodiments of the present invention is to provide an air electricity-supplementing aid device for a flying car. In order to achieve the technical purpose, the technical scheme adopted by the embodiment of the invention comprises the following steps: in one aspect, the embodiment of the invention provides a flying car air electricity supplementing and assisting method, which comprises the following steps: When the residual electric quantity of the target flying automobile is insufficient, generating a power-supplementing help request according to the equipment identifier, the first current position, the current flying path and the residual electric quantity of the target flying automobile, and uploading the power-supplementing help request to a cloud platform; matching the cloud platform according to the power-up help request to obtain a help aerocar, and determining a corresponding air merging position; issuing the equipment identifier and the air merging position to the aid aerocar through the cloud platform, and returning the air merging position to the target aerocar; Determining an optimal flight path and an estimated arrival time according to the air merging position by the aid aerocar, and sending the estimated arrival time to the target aerocar according to the equipment identifier; when the aid aerocar and the target aerocar reach the air converging position, controlling the aid aerocar and the target aerocar to carry out air butt joint, and supplementing electricity to the target aerocar through the aid aerocar. Further, in an embodiment of the present invention, the assisting aerocar is obtained by matching according to the electricity supplementing help request, which specifically includes: Determining the battery capacity of the target aerocar according to the equipment identifier, and determining the required electric quantity of the target aerocar according to the battery capacity and the residual electric quantity; Determining a plurality of alternative aerocars of a corresponding airspace according to the first current position and the current flight path, and determining a second current position and residual power supplementing capacity of each alternative aerocar; Determining the position matching degree of each alternative aerocar according to the second current position and the first current position, and determining the electric power supplementing capability matching degree of each alternative aerocar according to the residual electric power supplementing capability and the required electric quantity; the position matching degree and the power supplementing capability ma