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A hybrid programming modeling method based on rhapsody tool

A technology of hybrid programming and modeling methods, which is applied in the modeling field of aviation gas turbine engine numerical control system, and can solve the problem of inability to realize the complete support of the conceptual prototype of aviation gas turbine engine numerical control system.

Active Publication Date: 2022-03-04
中国航发控制系统研究所
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Problems solved by technology

[0004] The invention provides a hybrid programming modeling method based on the Rhapsody tool, which solves the problem in the related art that the complete support for the conceptual prototype of the numerical control system of the aviation gas turbine engine cannot be realized

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  • A hybrid programming modeling method based on rhapsody tool
  • A hybrid programming modeling method based on rhapsody tool
  • A hybrid programming modeling method based on rhapsody tool

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[0055] It should be noted that the features and embodiments in the present invention can be bonded to each other in the case of an unable conflict. The present invention will be described in detail below with reference to the accompanying drawings.

[0056] In order to better understand the present invention, the technical solutions in the embodiments of the present invention will become apparent to those skilled in the Embodiments of the invention, not all of the embodiments. Based on the embodiments in the present invention, those of ordinary skill in the art may belong to the scope of the present invention in the range of the present invention without all other embodiments obtained without making creative labor.

[0057] It should be noted that the specification and claims of the present invention and the terms "first", "second", "second", or the like are used to distinguish a similar object without having to describe a particular order or award order. It should be understood ...

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Abstract

The invention relates to the technical field of modeling of aviation gas turbine engine numerical control systems, and specifically discloses a hybrid programming modeling method based on a Rhapsody tool, which includes: creating a Harmony project according to the Rhapsody tool; Create at least two function blocks, data interaction can be performed between the function blocks, and each function block can realize functions different from other function blocks; set up a Simulink model, and the Simulink model can automatically generate code; according to the The code automatically generated by the Simulink model establishes a dll project and generates a dll file; the function block acquires interaction requirement parameters with other function blocks, and calls the matched dll file according to the interaction requirement parameters. The hybrid programming modeling method based on the Rhapsody tool provided by the invention can realize the complete support for the conceptual prototype of the numerical control system of the aviation gas turbine engine.

Description

Technical field [0001] The present invention relates to the modeling technique of aircraft gas turbine engine CNC system, and more particularly to a mixed programming modeling method based on RHAPSODY tools. Background technique [0002] Aviation gas turbine engine CNC system is developed into a field of multidisciplinary, high complexity, strong technological innovation. Constructing the aircraft gas turbine engine CNC system model is the main way for the design and adoption of CNC systems. In the model's content demonstration and program design phase, it relies on supportive modeling tools and modeling languages. [0003] Currently, there are only a variety of modeling language / tool coexistence, in order to achieve full support of the aircraft gas turbine engine CNC system concept. Inventive content [0004] The present invention provides a problem based on a mixed programming method based on Rhapsody tools, solving problems that cannot be implemented in the relevant technol...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F8/34G06F8/30
CPCG06F8/34G06F8/315
Inventor 田迪季春生汪松卢俊杰俞刚贾盼盼
Owner 中国航发控制系统研究所
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