Autonomous fault-tolerant attitude reference system using DTGs in symmetrically skewed configuration

Murugesan S.; Goel P.S.

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Autonomous fault-tolerant attitude reference system using DTGs in symmetrically skewed configuration

机译：在对称偏斜配置中使用DTG的自主容错姿态参考系统

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A novel symmetrically skewed configuration for an attitude reference system (ARS) using three dynamically tuned gyros (DTGs) is developed. Simple schemes for autonomous detection and identification of a faulty DTG in real time and subsequent reconfiguration of the attitude estimation algorithm are proposed. The performance of the present configuration is shown to be better than that of configurations proposed earlier, and it is shown to have better features. It tolerates all types of failures of DTG failures, requires very simple computations, and gives less error in attitude estimate than the other configurations.

机译：开发了一种新颖的对称偏斜配置，用于使用三个动态调谐陀螺仪（DTG）的姿态参考系统（ARS）。提出了一种用于实时自动检测和识别故障DTG的简单方案，以及随后对姿态估计算法的重新配置。示出了本配置的性能优于早先提出的配置的性能，并且示出具有更好的特征。与其他配置相比，它可以容忍所有类型的DTG故障，需要非常简单的计算，并且姿态估计的误差较小。

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《IEEE Transactions on Aerospace and Electronic Systems》 |1989年第2期|P.302-307|共6页
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Murugesan S.; Goel P.S.;
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正文语种 eng
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1. Dry Tuned Gyro (DTG) based Redundant Attitude Reference System (REARS) for IRS-1C [J] . M.Krishnaswamy, Robert Devasahayam, Jose George, Journal of Spacecraft Technology . 1995,第2期

机译：基于干调谐陀螺（DTG）的IRS-1C冗余姿态参考系统（REARS）
2. Robust attitude fault-tolerant control for unmanned autonomous helicopter with flapping dynamics and actuator faults [J] . Yan Kun, Chen Mou, Wu Qiangxian, Transactions of the Institute of Measurement and Control . 2019,第5期

机译：振动动力学和执行器故障的无人自主直升机的鲁棒态度容错控制
3. On fault-tolerant control configurations for a class of nonlinear systems [J] . Lia Linlin, Yang Ying, Ding Steven X., Journal of the Franklin Institute . 2015,第4期

机译：一类非线性系统的容错控制配置
4. Autonomous Strapdown Attitude and Heading Reference System for a Small Agile UAV [C] . Alexander Markov Saint Petersburg International Conference on Integrated Navigation Systems . 2020

机译：小型敏捷无人机的自主捷联姿态和航向参考系统
5. On Waring's Problem for Systems of Skew-Symmetric Forms. [D] . Wan, Jia. 2013

机译：关于偏对称形式系统的Waring问题。
6. Research on Adaptive Multi-Source Information Fault-Tolerant Navigation Method Based on No-Reference System Diagnosis [O] . Ling Zhang, Yuchen Cui, Zhi Xiong, 2019

机译：基于无参考系统诊断的自适应多源信息容错导航方法研究
7. Autonomous controller design system and its application to attitude control system reconfiguration. [O] . Shinichi NAKASUKA 1990

机译：自主控制器设计系统及其在姿态控制系统重新配置的应用。
8. Design and Laboratory Testing of Self-Contained High Altitude Navigation System. Phase I. The Space Sextant Autonomous Navigation Attitude Reference System (SS-ANARS). [R] . mikelson, a. dale 1977

机译：自给式高空导航系统的设计与实验室测试。第一阶段空间六分仪自主导航姿态参考系统（ss-aNaRs）。

Autonomous fault-tolerant attitude reference system using DTGs in symmetrically skewed configuration

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