Altitude measurement and simulation based on double-star position system

被引：0

作者：

Lin Xueyuan ^{[1
]}

Li Tingjun ^{[1
]}

Lin Yu ^{[1
]}

机构：

[1] Naval Aeronaut Engn Inst, Yantai 264001, Peoples R China

来源：

Proceedings of the First International Symposium on Test Automation & Instrumentation, Vols 1 - 3 | 2006年

关键词：

altitude determination; Double-Star positioning system; satellite simulator;

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：

Based on the satellite simulator, this paper introduces the basic principles of altitude determination using Double-Star positioning system, and deduces three double differential measurement equations. The long-short baseline method and sequence optimization method are synthetically used to estimate carrier phase ambiguity The simulation results show that the technique of altitude determination using Double-star position system is feasible.

引用

页码：1597 / 1600

页数：4