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坐标转换理论及其在半实物仿真姿态矩阵转换中的应用术

陈凯 王翔 刘明鑫 于云峰 闫杰

指挥控制与仿真2017,Vol.39Issue(2):118-122,5.
指挥控制与仿真2017,Vol.39Issue(2):118-122,5.DOI:10.3969/j.issn.1673-3819.2017.02.022

坐标转换理论及其在半实物仿真姿态矩阵转换中的应用术

Coordinate Transformation with Application in HWIL Simulation

陈凯 1王翔 1刘明鑫 1于云峰 1闫杰1

作者信息

  • 1. 西北工业大学航天学院,陕西西安710072
  • 折叠

摘要

Abstract

The relationship between the direction cosine matrix (DCM) in the space field and DCM in the aeronautics field is derived,to meet the demand of hardware-in-the-loop (HWIL) simulation of near space hypersonic vehicle flight control system.Firstly,the coordinate transformation (CT) theory is introduced,and the conversion method between two cartesian coordinate system is Introctuced.As well as the relationship of DCMs between the matrix transformation under two different reference systems is presented.Then,the analyzes the relationship of coordinate frames between the space field and the aeronautics field.How to convert the coordinate frame in the space field to the coordinate frame in the aeronautics field is researched.Finally,the HWIL simulation indicates that the method is correct and feasible.It ensures the HWIL simulation of navigation system of near space hypersonic vehicle.

关键词

坐标转换/姿态矩阵/半实物仿真/捷联惯性导航/临近空间飞行器

Key words

Coordinate transformation/direction cosine matrix (DCM)/Hardware-in-the-loop (HWIL) simulation/strap-down inertial navigation/Near space hypersonic vehicle

分类

航空航天

引用本文复制引用

陈凯,王翔,刘明鑫,于云峰,闫杰..坐标转换理论及其在半实物仿真姿态矩阵转换中的应用术[J].指挥控制与仿真,2017,39(2):118-122,5.

基金项目

国家安全重大基础研究项目(973) (973)

航天科技创新基金 ()

卫星导航系统与装备技术国家重点实验室基金. ()

指挥控制与仿真

OACSTPCD

1673-3819

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