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Aircraft Modeling and Model Characteristic Analysis System

A characteristic analysis, aircraft technology, applied in the direction of instruments, special data processing applications, geometric CAD, etc., to achieve the effect of improving accuracy, accurate aircraft modeling and model characteristic analysis

Active Publication Date: 2021-06-25
INST OF AUTOMATION CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the above-mentioned problems in the prior art, that is, in order to solve the problem that the existing aircraft modeling and model characteristic analysis system cannot efficiently and accurately perform aircraft modeling and model characteristic analysis, the first aspect of the present invention proposes an aircraft Modeling and model characteristic analysis system, which includes: aerodynamic module, aerodynamic moment module, six-degree-of-freedom motion equation module, reference motion state solution module, motion equation linearization module, longitudinal / lateral motion module, characteristic analysis and Display module and system management module;

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  • Aircraft Modeling and Model Characteristic Analysis System

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Embodiment Construction

[0065] In order to make the purpose, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Obviously, the described embodiments are part of the embodiments of the present invention, rather than Full examples. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0066] The application will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain related inventions, not to limit the invention. It should also be noted that, for the convenience of description, only the parts related to the related invention are sho...

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Abstract

The invention belongs to the field of aircraft design and analysis, and specifically relates to an aircraft modeling and model characteristic analysis system, aiming to solve the problem that the existing aircraft modeling and model characteristic analysis system cannot efficiently and accurately perform aircraft modeling and model characteristic analysis . The system includes: the system management module is configured to initialize the system; the aerodynamic / aerodynamic moment module is configured to calculate the aerodynamic force acting on the center of mass of the aircraft / the aerodynamic moment around the center of mass of the aircraft; the six-degree-of-freedom motion equation module is configured to construct the aircraft Full-dimensional motion state equations; the reference motion state solution module is configured to solve the full-dimensional motion state of the aircraft under reference motion conditions; the motion equation linearization module is configured to generate a state-space full-state linearization model of the aircraft; characteristic analysis and display The module is configured to conduct aircraft model characteristic analysis. The invention realizes efficient and accurate aircraft modeling and model characteristic analysis.

Description

technical field [0001] The invention belongs to the field of aircraft design and analysis, in particular to an aircraft modeling and model characteristic analysis system. Background technique [0002] In recent years, with the rapid development of flight technology, various aircrafts have been widely used in military and civilian fields. In the process of aircraft development, modeling and model characteristic analysis are extremely important tasks, especially in the preliminary design stage of aircraft. In the preliminary design stage of the aircraft, designers need to conduct modeling and model characteristic analysis based on the preliminary design plan. Get a design that meets the requirements. On the other hand, with the complexity and diversification of aircraft operating tasks and environments, the complexity of aircraft design is also increasing. Therefore, how to carry out rapid and accurate aircraft modeling and model characteristic analysis is an urgent need fo...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/15G06F30/28G06F119/14
CPCG06F30/15G06F30/28G06F2119/14Y02T90/00
Inventor 刘振吴士广张天乐蒲志强丘腾海易建强
Owner INST OF AUTOMATION CHINESE ACAD OF SCI