惯性导航系统
惯性测量装置
惯性基准装置
惯性参考系
有效载荷(计算)
计算机科学
全球定位系统
计量单位
工程类
人工智能
电信
物理
计算机网络
量子力学
网络数据包
作者
Ronald E. Cox,Shao Wei
标识
DOI:10.1109/auv.1994.518648
摘要
Inertial navigation reference units are often thought of as simply a navigation device which must be augmented by another device to damp the Schuler oscillation and characteristic long-term drift. Emerging applications of AUVs, however, demonstrate a need for increasingly sophisticated inertial sensors. These inertial sensors are used not only for navigation, but as importantly, they provide data for sensor stabilization. Inertial systems have also traditionally represented a significant hotel load, been heavy, bulky and a source of acoustic and structure-borne noise. This paper presents an overview of two new inertial systems that are now in production at the Guidance and Control Systems Division of Litton Systems, Inc. These units are small, lightweight, require little power, and are silent. Data are presented that show long-term performance as well as short-term attitude, attitude rate, position, and velocity reference data for the two systems. Attitude, velocity and body axis rate data are required for stabilization of such devices as laser line scanners and long baseline side-scan sonars. The relationship between the characteristics of these sensors and inertial type errors is explored. This analysis shows that it is not sufficient to specify the inertial system only in terms of its navigation CEP. The specification of the inertial unit must also be based on the needs of the sensor payload and include such considerations as the noise content, phase, and bandwidth of the stabilization reference.
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