DESIGN AND REALIZATION OF SINS/TWO-ANTENNA GPS INTEGRATED NAVIGATION SYSTEM

作     者：王直 刘建业 刘波 Wang Zhi;Liu Jianye;Liu Bo

作者机构：南京航空航天大学自动化学院 江苏科技大学电子信息学院 

出 版 物：《Transactions of Nanjing University of Aeronautics and Astronautics》 (南京航空航天大学学报（英文版）)

年 卷 期：2006年第23卷第1期

页      码：41-46页

摘      要：The strapdown inertial navigation system （SINS）/two-antenna GPS integrated navigation system is discussed. Corresponding error and the measurement models are built, especially the double differenced GPS carrier phase model. The extended Kalman filtering is proposed. And the hardware composition and connection are designed to simulate the SINS/two-antenna GPS integrated navigation system. Results show that the performances of the system, the precision of the navigation and the positioning, the reliability and the practicability are im proved.

主 题 词：strapdown inertial navigation system GPS Kalman filtering pseudorange carrier phase 

学科分类：08[工学] 081105[081105] 0811[工学-水利类] 

核心收录：

D　O　I：10.3969/j.issn.1005-1120.2006.01.007

馆 藏 号：203603124...