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Simulation method, device and equipment for electric vertical take-off and landing aircraft and medium

A technology of vertical take-off and landing and simulation methods, applied in the field of eVTOL aircraft, to improve simulation efficiency and development efficiency, and realize the effect of sharing

Pending Publication Date: 2022-08-02
安胜(天津)飞行模拟系统有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The invention provides a simulation method, device, equipment and medium of an electric vertical take-off and landing aircraft, and improves the simulation efficiency and development efficiency of eVTOL aircraft by solving the problem that different current modeling and simulation products belong to different simulation platforms

Method used

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  • Simulation method, device and equipment for electric vertical take-off and landing aircraft and medium
  • Simulation method, device and equipment for electric vertical take-off and landing aircraft and medium
  • Simulation method, device and equipment for electric vertical take-off and landing aircraft and medium

Examples

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Embodiment 1

[0033] figure 1 It is a flowchart of a simulation method of an electric vertical take-off and landing aircraft provided according to the first embodiment of the present invention. This embodiment can be applied to the situation of performing a simulation operation on an eVTOL aircraft. To execute, the simulation device of the electric vertical take-off and landing aircraft can be implemented in the form of hardware and / or software, and the simulation device of the electric vertical take-off and landing aircraft can be configured in a terminal device. like figure 1 As shown, the method includes:

[0034] S110. Acquire a function description file and an interface definition file corresponding to at least one aircraft component respectively.

[0035] In an embodiment, optionally, a function description file and an interface definition document corresponding to at least one aircraft component imported by the business system are obtained. The document format of the interface def...

Embodiment 2

[0063] Figure 4 This is a flowchart of a simulation method for an electric vertical take-off and landing aircraft provided according to the second embodiment of the present invention. This embodiment further refines the "current modeling and simulation product" in the above-mentioned embodiment. like Figure 4 As shown, the method includes:

[0064] S210. Acquire a function description file and an interface definition file corresponding to at least one aircraft component respectively.

[0065] Among them, the simulation platform is connected with the data transmission interface of the business system by setting the interface, so as to realize the data interaction with the business system. Among them, exemplary business systems include, but are not limited to, original equipment manufacturers, operators, infrastructure providers, air navigation service providers, maintenance service providers, training centers and training solution providers, regulators, and the like. Of th...

Embodiment 3

[0085] Image 6 It is a schematic structural diagram of a simulation device for an electric vertical take-off and landing aircraft provided according to the third embodiment of the present invention. like Image 6 As shown, the apparatus includes: an interface definition document acquisition module 310 , a component simulation model determination module 320 , a current modeling and simulation product determination module 330 and a simulation result determination module 340 .

[0086] Wherein, the interface definition document acquisition module 310 is used to acquire the function description file and the interface definition document corresponding to at least one aircraft part respectively; wherein, the function description file represents the function parameter information of the aircraft part, and the interface definition document represents the interface parameter information of the aircraft part ;

[0087] The component simulation model determination module 320 is config...

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Abstract

The invention discloses a simulation method, device and equipment for an electric vertical take-off and landing aircraft and a medium. The method comprises the steps that a function description file and an interface definition file corresponding to at least one aircraft component are obtained; for each aircraft component, determining a component simulation model corresponding to the aircraft component based on the function description file, the interface definition file and the general simulation component corresponding to the aircraft component; in response to the detected simulation request, determining a current modeling simulation product based on at least one target component simulation model corresponding to the simulation request; and executing a simulation operation on the current modeling simulation product to obtain a simulation result corresponding to the simulation request. According to the embodiment of the invention, the problem that existing different current modeling simulation products belong to different simulation platforms is solved, the sharing of upstream and downstream resource data in the simulation process of the eVTOL aircraft is realized, and the simulation efficiency and development efficiency of the eVTOL aircraft are improved.

Description

technical field [0001] The invention relates to the technical field of eVTOL aircraft, in particular to a simulation method, device, equipment and medium for an electric vertical take-off and landing aircraft. Background technique [0002] eVTOL (Electric Vertical Take-Off and Landing, Electric Vertical Take-Off and Landing) aircraft is a safe and sustainable form of barrier-free aviation, eVTOL aircraft has the potential to revolutionize urban transportation networks and play an indispensable role in future smart cities effect. The entire life cycle of an eVTOL aircraft is a huge and complicated system engineering, involving the coordination of multiple business systems such as equipment manufacturers, operators, infrastructure providers, air navigation service providers, and regulatory agencies. [0003] At present, each business system separately designs a simulation platform and uses a separate data repository according to the aircraft components in the eVTOL aircraft i...

Claims

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Application Information

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IPC IPC(8): G06F30/20G06F8/30G06F8/73
CPCG06F30/20G06F8/30G06F8/73Y02T90/00
Inventor 沈硕刘丽丽卢禹轩刘彧李心然丁元沅
Owner 安胜(天津)飞行模拟系统有限公司