SMALL-SIZED INTEGRATED NAVIGATION AND ATTITUDE DETERMINATION SYSTEM

机译：小型综合导航和姿态确定系统

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An experimental sample of small-sized integrated navigation and attitude determination system is represented in the report. Micromechanical strapdown inertial navigation system, multiantenna satellite attitude determination system, a microme-chanical magnetic compass are included in the structure of integrated system, and an opportunity of micromechanical baro-altimeter connection is also stipulated. The developed experimental sample of integrated system is presented in photos. The results of tests showing state vector estimation accuracy in stationary conditions are resulted.

机译：报告中展示了小型综合导航和姿态确定系统的实验样本。集成系统的结构中包括微机械捷联惯性导航系统，多天线卫星姿态确定系统，微机械磁罗盘，并规定了微机械气压高度表的连接机会。图片展示了已开发的集成系统的实验样本。得出了在静态条件下显示状态矢量估计精度的测试结果。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20070528-30; Saint Petersburg(RU)》|2007年|P.165-169|共5页
会议地点 Saint Petersburg(RU)
作者
D. A. Antonov; K. K. Veremeenko; M. V. Zharkov; R. Yu. Zimin;
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作者单位

Moscow Aviation Institute (State Technical University) 125993, Moscow, A-80, GSP-3, Volokolamskoye sh., 4, MAI, dept. 305;

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会议组织
原文格式 PDF
正文语种 eng
中图分类导航设备;
关键词
inertial navigation; satellite navigation; integrated navigation system; kalman filter;

机译：惯性导航卫星导航组合导航系统卡尔曼滤波;

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机译：GPS / VISNAV集成的相对导航和姿态确定系统，用于超近距离航天器编队飞行
2. GPSNISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying [J] . Xiaoliang Wang, Xiaowei Shao, Deren Gong, 系统工程与电子技术：英文版 . 2011,第002期

机译：GPSNISNAV集成的相对导航和姿态确定系统用于超近距离航天器编队飞行
3. GPS/VISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying [J] . Xiaoliang Wang, Xiaowei Shao, Deren Gong, 系统工程与电子技术（英文版） . 2011,第002期

机译：GPS / VISNAV集成的相对导航和姿态确定系统，用于超近距离航天器编队飞行
4. SMALL-SIZED INTEGRATED NAVIGATION AND ATTITUDE DETERMINATION SYSTEM [C] . D. A. Antonov, K. K. Veremeenko, M. V. Zharkov, Saint Petersburg International Conference on Integrated Navigation Systems . 2007

机译：小型集成导航和姿态确定系统
5. Relative navigation and attitude determination using a GPS/INS integrated system near the International Space Station. [D] . Um, Jaeyong. 2001

机译：使用国际空间站附近的GPS / INS集成系统进行相对导航和姿态确定。
6. SINS/Landmark Integrated Navigation Based on Landmark Attitude Determination [O] . Shuqing Xu, Haiyin Zhou, Jiongqi Wang, 2019

机译：基于地标姿态确定的SINS /地标组合导航
7. Multilevel Systems Engineering for the Functional Stability of the Small-Sized Spacecraft Movement nd Navigation Control Systems [O] . S. N. Firsov 2015

机译：用于小型航天器运动的功能稳定性的多级系统工程ND导航控制系统

SMALL-SIZED INTEGRATED NAVIGATION AND ATTITUDE DETERMINATION SYSTEM

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