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Flight performance analyzing system and the method for helicopter

机译:直升机飞行性能分析系统及方法

摘要

PURPOSE: A helicopter flying characteristics interpretive system and an interpretive method thereof are provided to offer an interpretative code for interpreting helicopter flying characteristics by using object dynamics. CONSTITUTION: A model construction module unit(10) constructs a model file for interpreting helicopter flying characteristics according to a helicopter modeling element by reflecting multi-objects dynamics. A model generation unit(20) generates a flying characteristics interpretive model by using the model file by connecting to the model construction module unit. A flying characteristics interpretive module unit(30) interprets flying characteristics by connecting to the model generation unit. The helicopter modeling element is a dynamic modeling element, an attack modeling element, and a forwarding modeling element. [Reference numerals] (10) Model construction module unit; (20) Model generation unit; (30) Flying characteristics interpretive module unit
机译:目的:提供一种直升机飞行特性解释系统及其解释方法,以提供用于利用物体动力学来解释直升机飞行特性的解释代码。构成:模型构建模块单元(10)通过反映多对象动力学来根据直升机建模元素构建用于解释直升机飞行特性的模型文件。模型生成单元(20)通过连接到模型构建模块单元,使用模型文件来生成飞行特性解释模型。飞行特性解释模块单元(30)通过连接到模型生成单元来解释飞行特性。直升机建模元素是动态建模元素,攻击建模元素和转发建模元素。 [附图标记](10)模型构建模块单元; (20)模型产生单元; (30)飞行特性说明模块单元

著录项

  • 公开/公告号KR101333205B1

    专利类型

  • 公开/公告日2013-12-02

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20110075136

  • 发明设计人 권순용;

    申请日2011-07-28

  • 分类号G06F19;B64C27/04;

  • 国家 KR

  • 入库时间 2022-08-21 15:44:12

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