MEMS IMU: Development and Flight Test Results

A. G. Kuznetsov; V. I. Galkin; A. V. Molchanov; B. I. Portnov; A. M. Yakubovich

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MEMS IMU: Development and Flight Test Results

机译：MEMS IMU：开发和飞行测试结果

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The paper presents a MEMS IMU, being a component of integrated standby instrument system (ISIS). MEMS IMU determines aircraft roll, pitch and heading, when the main inertial navigation system or attitude heading reference system is a failure. Design features, software algorithms, and calibration procedure are outlined. Results from the unit flight tests onboard TU-204 SM aircraft are presented.

机译：本文介绍了MEMS IMU，它是集成备用仪器系统（ISIS）的组成部分。当主要惯性导航系统或姿态航向参考系统出现故障时，MEMS IMU确定飞机的侧倾，俯仰和航向。概述了设计功能，软件算法和校准过程。列出了TU-204 SM飞机的单元飞行测试结果。

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《Gyroscopy and navigation》 |2012年第4期|255-264|共10页
作者
A. G. Kuznetsov; V. I. Galkin; A. V. Molchanov; B. I. Portnov; A. M. Yakubovich;
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Moscow Institute of Electromeehanics and Automatics, Moscow, Russia;

Moscow Institute of Electromeehanics and Automatics, Moscow, Russia;

Moscow Institute of Electromeehanics and Automatics, Moscow, Russia;

Moscow Institute of Electromeehanics and Automatics, Moscow, Russia;

Moscow Institute of Electromeehanics and Automatics, Moscow, Russia;

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MEMS IMU: Development and Flight Test Results

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