Home

Instructions for Authors

Subscribe Guide

Open Access Statement

Publishing Ethical Statements

SINS在小型无人机测控方面的应用

Application of SINS to Miniature Type UAV

Revised:March 27, 2007

HTML View Full Text View/Add Comment Download reader

中文摘要:

为了满足小型无人机航姿系统设计需要,本文对捷联式惯导系统特点及其在小型无人机导航制导领域的应用进行了讨论,特别是对捷联惯导系统通过优化算法及由全球定位系统和捷联惯导系统组建的组合式导航系统进行了分析.讨论结果表明,捷联式惯导系统(包括以捷联式惯导系统为基础组建的组合式导航系统)能够满足无人机导航要求,在小型无人机领域具有很好的应用前景.

英文摘要:

Characteristic of strapdown inertial navigation system(SINS) and its application to guiding,navigation and control(GNC) of miniature type unmanded air vehicle(UAV) are discussed in this paper.As a complementarity,the algorithm of SINS and the SINS/GPS(Global Positoning System)integrated navigation system are analysed.The result indicates that the algorithm and the integrated system based on SINS can meet the GNC-specification of UAV and has a good prospect in this area.

王磊张怀周顾伟黄志毅

[1]同济大学中德学院,上海200092 [2]兰州飞控仪器有限公司,甘肃兰州730070

中文关键词: 捷联式惯导系统组合导航系统小型无人机 SINS 小型无人机测控域的应用 Type 前景无人机导航捷联式惯导系统结果分析导航系统组合式系统组建捷联惯导系统全球定位系统优化算法导航制导系统特点系统设计

英文关键词:strapdown inertial navigation system integrated navigation system miniature type UAV

基金项目:

DOI：