Design of an Unaided Aircraft Attitude Reference System with Medium Accurate Gyroscopes for Higher Performance Attitude Requirements

机译：具有中等姿态陀螺仪的无辅助飞机姿态参考系统的设计，可满足更高的姿态要求

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The paper discusses an approach to provide attitude information (roll/pitch) by a medium accurate inertial measurement system without significant drift, even if neither sensors for velocity nor magnetic nor position aiding are applied. The hardware and the algorithm are described as well as the reference measurement systems being used to determine the obtainable accuracy. Test results are provided.

机译：本文讨论了一种通过中等精度的惯性测量系统提供姿态信息（侧倾/俯仰）的方法，即使没有应用速度传感器，磁传感器或位置辅助传感器，也不会出现明显的漂移。描述了硬件和算法，以及用于确定可获得精度的参考测量系统。提供测试结果。

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来源
《Symposium gyro technology 2011 : Inertial sensors and systems 2011》|2011年|p.17.1-17.30|共30页
会议地点 Karlsruhe(DE);Karlsruhe(DE)
作者
P. Kohl; R. Cartarlus; S. Knedlik; E. v. Hinueber;
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作者单位

iMAR Navigation GmbH Systems for Inertial Navigation, Stabilization, Surveying and Control Im Reihersbruch 3 D-66386 St. Ingbert GERMANY;

iMAR Navigation GmbH Systems for Inertial Navigation, Stabilization, Surveying and Control Im Reihersbruch 3 D-66386 St. Ingbert GERMANY;

iMAR Navigation GmbH Systems for Inertial Navigation, Stabilization, Surveying and Control Im Reihersbruch 3 D-66386 St. Ingbert GERMANY;

iMAR Navigation GmbH Systems for Inertial Navigation, Stabilization, Surveying and Control Im Reihersbruch 3 D-66386 St. Ingbert GERMANY;

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原文格式 PDF
正文语种 eng
中图分类 U666.123;
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Design of an Unaided Aircraft Attitude Reference System with Medium Accurate Gyroscopes for Higher Performance Attitude Requirements

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