Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/7198
Title: SAR motion information sensor based on GNSS/SINS
Other Titles: GNSS/SINS组合SAR运动信息传感器
Authors: Sun, YR
Liu, JY
Chen, W 
Chen, YQ 
Keywords: Integration navigation
Kalman filter
SAR
Motion compensation
Issue Date: 2003
Publisher: Journal of NAI
Source: Transactions of Nanjing University of Aeronautics & Astronautics, Dec. 2003, v. 20, no. 2, p. 172-177
南京航空航天大学学报 (英文版), Dec. 2003, v. 20, no. 2, p. 172-177 How to cite?
Journal: Transactions of Nanjing University of Aeronautics & Astronautics 
Abstract: 提出一种不依赖于机载主惯导的 SAR运动信息传感器方案 ,即改进的基于 GNSS/ SINS组合运动系统。在成像期间 ,输出以纯惯性为主的导航信号 ,以保证较高的相对定位精度。而 GNSS/ SINS组合 ,则保证了长时间的绝对定位精度。本文介绍了这种运动传感器的原理和数学模型等 ,并对实验结果作了分析。多次实验表明 ,本文提出的基于 GNSS/ SINS的运动传感器具有很高的精度 ,完全满足了 SAR成像的精度要求 ,特别适用于没有主惯导或主惯导精度较低的场合
Synthetic aperture radar (SAR) is theoretically based on uniform rectilinear motion. But in real situations, the flight cannot be kept in a uniform rectilinear motion due to many factors. Therefore, the motion compensation is needed to achieve the high-resolution image. This paper proposes an improved motion information sensor (MIS)-based on global navigation statellite system (GNSS) and strapdown inertial navigation system (SINS) for SAR motion compensation. MIS can provide the long-term absolute accuracy, and the short-term high relative accuracy during SAR imaging. Many issues related to MIS, such as system design, error models and navigation algorithms, are stressed. Experimental results show that MIS can provide accurate navigation information (position, velocity and attitude) to meet the requirements of SAR motion compensation. Especially, MIS is suitable for the case: the accuracy of airplane master inertial navigation system is too low or not configured.
URI: http://hdl.handle.net/10397/7198
ISSN: 1005-1120
Rights: © 2003 中国学术期刊电子杂志出版社。本内容的使用仅限于教育、科研之目的。
© 2003 China Academic Journal Electronic Publishing House. It is to be used strictly for educational and research use.
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