Development of a GPS/INS integrated navigation system for model aircraft

被引：0

作者：

Bach-Phi Duong ^{[1
]}

Vinh-Hao Nguyen ^{[2
]}

机构：

[1] HoChiMinh City Univ Technol, Dept Transportat Engn, Hochiminh, Vietnam

[2] HoChiMinh City Univ Technol, Dept Elect & Elect Engn, Hochiminh, Vietnam

来源：

2014 14TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS (ICCAS 2014) | 2014年

关键词：

Low-cost INS; GPS; GPS/INS integration; extended Kalman filter;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper addresses the development of an integrated navigation system based on MEMS inertial sensors and GPS for model aircraft. The objective of this paper is to propose a loosely coupled GPS/INS integration approach using Extended Kalman filter to estimate aircraft's position, velocity, and attitude. Special attention is paid to the computational performance of the algorithm and the handling of GPS outages. The simulation results based on a typical high dynamic flight trajectory validate that the proposed filter is applicable to flight navigation.

引用

页码：201 / 206

页数：6

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