STRAPDOWNINERTIAL ATTITUDE REFERENCE SYSTEM FOR ARBITRARY ORIENTED ORBITAL SPACECRAFT: OPTIMIZING THE CALIBRATION METHOD IN GROUND CONDITIONS

机译：任意定向太空航天器的腕上姿态参考系统：优化地面条件下的标定方法

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

The paper considers a strapdown inertial attitude reference system (SIARS) based on electrostatic gyros with solid rotors. The system in-flight calibration method is optimized using the ground tests. Preliminary estimates of drift model coefficients and misalignment angles between ESG and IMU frames are given. Results from ground calibration are presented.

机译：本文考虑了基于带有固体转子的静电陀螺仪的捷联惯性姿态参考系统（SIARS）。使用地面测试对系统的飞行中校准方法进行了优化。给出了ESG和IMU框架之间的漂移模型系数和未对准角度的初步估计。给出了地面校准的结果。

著录项

来源
《Saint Petersburg international conference on integrated navigation systems》|2012年|127-135|共9页
会议地点
作者
B.E. Landau; S.L. Levin; S.S. Gurevich; G.I. Yemelyantsev; V.I. Zavgorodny; S.G. Romanenko; B.V. Odintsov;
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类
关键词
strapdown inertial attitude reference system; electrostatic gyro; calibration; inertial and orbital orientation;

机译：捷联惯性姿态参考系统;静电陀螺仪校准;惯性和轨道取向;

相似文献

外文文献
中文文献
专利

1. Integrated Attitude Reference and Navigation System for Orbital Spacecraft [J] . G. I. Emelyantsev, B. E. Landau, S. L. Levin, Gyroscopy and navigation . 2011,第3期

机译：轨道航天器综合姿态参考与导航系统
2. Control-oriented modelling and simulation of spacecraft attitude and orbit dynamics [J] . MARCO LOVERA Mathematical and Computer Modelling of Dynamical Systems . 2006,第1期

机译：面向控制的航天器姿态和轨道动力学建模与仿真
3. Vector-Aided In-Field Calibration Method for Low-End MEMS Gyros in Attitude and Heading Reference Systems [J] . Li X., Li Z. Instrumentation and Measurement, IEEE Transactions on . 2014,第11期

机译：姿态和航向参考系统中低端MEMS陀螺仪的矢量辅助现场校准方法
4. STRAPDOWNINERTIAL ATTITUDE REFERENCE SYSTEM FOR ARBITRARY ORIENTED ORBITAL SPACECRAFT: OPTIMIZING THE CALIBRATION METHOD IN GROUND CONDITIONS [C] . B.E. Landau, S.L. Levin, S.S. Gurevich, Saint Petersburg international conference on integrated navigation systems . 2012

机译：随意取向轨道航天器的塑料姿态参考系统：优化地面条件下的校准方法
5. Attitude Dependent De-Orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite. [D] . Tarantini, Vincent Claudio Franco. 2012

机译：气动拖航演示航天器的姿态相关离轨寿命分析和极轨通信纳米卫星的详细热子系统设计。
6. Maximizing the Reliability of Genomic Selection by Optimizing the Calibration Set of Reference Individuals: Comparison of Methods in Two Diverse Groups of Maize Inbreds (Zea mays L.) [O] . R. Rincent, D. Laloë, S. Nicolas, 2012

机译：通过优化参考个体的校准集来最大化基因组选择的可靠性：两种玉米自交系（Zea mays L.）中方法的比较
7. Object-oriented modelling of spacecraft attitude and orbit dynamics [O] . Marco Lovera 2003

机译：面向对象的航天器姿态和轨道动力学建模
8. Global Matrix of Thermospheric Density Values for Selected Solar/Geomagnetic Conditions and Spacecraft Orbital Attitudes [R] . Johnson, D. L. 1984

机译：选定的太阳/地磁条件和航天器轨道姿态的全球热密度值矩阵

STRAPDOWNINERTIAL ATTITUDE REFERENCE SYSTEM FOR ARBITRARY ORIENTED ORBITAL SPACECRAFT: OPTIMIZING THE CALIBRATION METHOD IN GROUND CONDITIONS

摘要

著录项

相似文献

相关主题

期刊订阅