Analysis of Star Tracker/Accelerometer Inertial Navigation System in Theory

机译：明星跟踪器/加速度计惯性导航系统的分析

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In the star tracker/accelerometer inertial navigation system, the star tracker will be used to calculate the attitude matrix. The accelerometer is analyzed and integral utilizing the attitude matrix, to get the velocities and position of carrier, the feedback is formative. After star tracker/accelerometer inertial navigation system in theory is resolved, the errors will be discussed and the result will be proved by the simulation test.

机译：在星形跟踪器/加速度计惯性导航系统中，星形跟踪器将用于计算姿态矩阵。通过姿态矩阵分析和积分加速度计，以获得载波的速度和位置，反馈是形成性的。在理论上解决明星跟踪器/加速度计惯性导航系统后，将讨论错误，并通过仿真测试证明结果。

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《International Conference on Mechatronics and Automation》|2011年||共5页
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作者
Yingbo Cai; Qiuying Wang; Xuetong Wei; Debiao Li;
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中图分类 TP2-53;
关键词
Star tracker; Inertial navigation system; Gyros-free; Accelerometer;

机译：星追踪器;惯性导航系统;自由陀螺;加速度计;

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专利

1. Adaptive robust ultra-tightly coupled global navigation satellite system/inertial navigation system based on global positioning system/BeiDou vector tracking loops [J] . Fei Xie, Jianye Liu, Rongbing Li, Radar, Sonar & Navigation, IET . 2014,第7期

机译：基于全球定位系统/北斗矢量跟踪环的自适应鲁棒超紧耦合全球导航卫星系统/惯性导航系统
2. Calibrating accelerometers for space-stable inertial navigation systems at system level [J] . He Qianen, Zeng Congjie, He Xiaoxia, Measurement . 2018,第期

机译：校准系统级空间稳定惯性导航系统的加速度计
3. Robust in-field estimation and calibration approach for strapdown inertial navigation systems accelerometers bias acting on the vertical channel [J] . Radar, Sonar & Navigation, IET . 2020,第3期

机译：捷联惯性导航系统加速度计偏置作用于垂直通道的鲁棒性现场估计和校准方法
4. Analysis of star tracker/accelerometer inertial navigation system in theory [C] . Cai Yingbo, Wang Qiuying, Wei Xuetong, 2011 IEEE International Conference on Mechatronics and Automation . 2011

机译：恒星跟踪器/加速度计惯性导航系统的理论分析
5. Modeling navigation system performance of a satellite-observing star tracker tightly integrated with an Inertial Measurement Unit. [D] . Pierce, Scott J. 2015

机译：与惯性测量单元紧密集成的卫星观测恒星跟踪器的导航系统性能建模。
6. A Three-Stage Accelerometer Self-Calibration Technique for Space-Stable Inertial Navigation Systems [O] . Qiuping Wu, Ruonan Wu, Fengtian Han, 2018

机译：空间稳定惯性导航系统的三阶段加速度计自校准技术
7. A method for testing the dynamic accuracy of Microelectro-Mechanical Systems (MEMS) Magnetic, Angular Rate, and Gravity (MARG) sensors for Inertial Navigation Systems (INS) and human motion tracking applications [O] . Cookson Jeremy L. 2010

机译：一种用于惯性导航系统（INS）和人体运动跟踪应用的微机电系统（MEMS）磁，角速率和重力（MARG）传感器的动态精度测试方法
8. Modeling Navigation System Performance of a Satellite-Observing Star Tracker Tightly Integrated with an Inertial Measurement Unit. [R] . Pierce, S. J. 2015

机译：卫星观测星跟踪器导航系统性能建模与惯性测量单元紧密结合。

Analysis of Star Tracker/Accelerometer Inertial Navigation System in Theory

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