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Development of an Integrated low-cost GPS/rate gyro system for attitude determination

机译：开发用于姿态确定的集成低成本Gps /速率陀螺仪系统

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Chaochao Wang; M. Elizabeth Cannon;
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年度 2015
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1. Development of an Integrated Low-Cost GPS/Rate Gyro System for Attitude Determination [J] . Chaochao Wang, Gerard Lachapelle, M. Elizabeth Cannon The Journal of Navigation . 2004,第1期

机译：集成的低成本GPS /速率陀螺仪姿态确定系统的开发
2. Design of a low-cost attitude determination GPS/INS integrated navigation system [J] . Hwang DH, Oh SH, Lee SJ, GPS Solutions . 2005,第4期

机译：低成本姿态确定GPS / INS组合导航系统的设计
3. Design of a low-cost attitude determination GPS/INS integrated navigation system [J] . Dong-Hwan Hwang, Sang Heon Oh, Sang Jeong Lee, GPS Solutions . 2005,第4期

机译：低成本姿态确定GPS / INS组合导航系统的设计
4. ADAPTIVE KALMAN FILTERING ALGORITHM FOR SMALL SATELLITE ATTITUDE DETERMINATION BY USING GPS/GYRO INTEGRATED SYSTEM [C] . Jianjun Luo, Jianping Yuan, Junwu Wang, 52nd International Astronautical Congress Oct 1-5, 2001 Toulouse, France . 2001

机译：GPS /陀螺仪集成系统的自适应卡尔曼滤波算法在小卫星姿态确定中的应用
5. Tightly integrated attitude determination methods for low-cost inertial navigation: Two-antenna GPS and GPS/magnetometer. [D] . Yang, Yunchun. 2001

机译：用于低成本惯性导航的紧密集成的姿态确定方法：两天线GPS和GPS /磁力计。
6. Deeply Integrated GNSS/Gyro Attitude Determination System [O] . Alexander Perov, Alexander Shatilov 2020

机译：深度集成的GNSS /陀螺仪姿态确定系统
7. Precise attitude determination strategy for spacecraft based on information fusion of attitude sensors: Gyros/GPS/Star-sensor [O] . Xinyuan Mao, Xiaojing Du, Hui Fang 2013

机译：基于信息传感器信息融合的宇宙飞船精确姿态确定策略：陀螺/ GPS /星形传感器

Development of an Integrated low-cost GPS/rate gyro system for attitude determination

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