首页> 外国专利> HWIL FLIGHT OBJECT GUIDANCE AND CONTROL HWIL SIMULATION SYSTEM INCLUDING INERTIAL NAVIGATION SYSTEM AND CONFIGURATION METHODS OF THE SAME

HWIL FLIGHT OBJECT GUIDANCE AND CONTROL HWIL SIMULATION SYSTEM INCLUDING INERTIAL NAVIGATION SYSTEM AND CONFIGURATION METHODS OF THE SAME

机译:包括惯性导航系统的飞行目标制导控制仿真系统及其配置方法

摘要

The present invention provides a flight attitude simulator for generating rotational motion data of a vehicle from an inertial navigation device; A vehicle real-time simulation module for generating translational motion data of the vehicle from a software model and controlling the flight attitude simulator; A data integration module including a time synchronization generator for compensating a deviation in generation time between data when integrating rotational motion data and translational motion data; Disclosed is a vehicle guided steering apparatus that guides and manipulates a vehicle based on integrated data, and transmits the resultant data of the guided vehicle to a software model in a vehicle real-time simulation module. According to the present invention, it overcomes the data synchronization problem that occurs during the integration of the motion data of the aircraft, and provides specific guidelines for the system configuration for the aircraft real-time simulation module and data integration module based on the complexity and fidelity.
机译:本发明提供了一种飞行姿态模拟器,用于从惯性导航装置生成车辆的旋转运动数据。车辆实时仿真模块,用于从软件模型生成车辆的平移运动数据并控制飞行姿态模拟器;一种数据集成模块,包括时间同步发生器,用于在对旋转运动数据和平移运动数据进行积分时补偿数据之间的生成时间偏差;公开了一种车辆引导转向装置,其基于集成数据来引导和操纵车辆,并将所引导车辆的结果数据传输至车辆实时仿真模块中的软件模型。根据本发明,它克服了在飞机的运动数据的集成期间发生的数据同步问题,并基于复杂性和复杂性为飞机实时仿真模块和数据集成模块的系统配置提供了特定的指导。保真。

著录项

  • 公开/公告号KR101994441B1

    专利类型

  • 公开/公告日2019-09-30

    原文格式PDF

  • 申请/专利权人 국방과학연구소;

    申请/专利号KR20170076680

  • 发明设计人 이아영;

    申请日2017-06-16

  • 分类号G09B9/08;G05B17/02;

  • 国家 KR

  • 入库时间 2022-08-21 11:48:20

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