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Accuracy Improvement of Attitude Determination Systems Using EKF-Based Error Prediction Filter and PI Controller

机译：基于EKF的误差预测滤波器和PI控制器的姿态确定系统的准确性改进

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Farzan Farhangian; Rene Landry;
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1. Regularized robust filter for attitude determination system with relative installation error of star trackers [J] . Jiong-qi Wang, Zhang-ming He, Hai-yin Zhou, Acta astronautica . 2013,第junaajula期

机译：具有星跟踪器相对安装误差的姿态确定系统的正则鲁棒滤波器
2. A First-Order Differential Data Processing Method for Accuracy Improvement of Complementary Filtering in Micro-UAV Attitude Estimation [J] . Wen Xudong, Liu Chunwu, Huang Zhiping, Nature reviews Cancer . 2019,第6期

机译：微无人态估计互补滤波精度改善的一阶差分数据处理方法
3. Real-time implementation of PI and fuzzy logic controllers based shunt active filter control strategies for power quality improvement [J] . Suresh Mikkili, A.K. Panda International Journal of Electrical Power & Energy Systems . 2012,第1期

机译：基于PI和模糊逻辑控制器的实时分流有源滤波器控制策略的实时实现，可提高电能质量
4. Design and Simulation of Attitude Determination and Control Subsystem of CubeSat Using Extended Kalman Filtering and Linear Quadratic Gain Controller [C] . Xiao Han, Xiaojun Yang, Naqvi Najam Abbas International Conference on Manufacturing Science and Engineering . 2013

机译：扩展卡尔曼滤波和线性二次增益控制器设计与仿真CubeSat姿态确定与控制子系统
5. In-flight detection of errors for enhanced aircraft flight safety and vertical accuracy improvement using digital terrain elevation data with an inertial navigation system, global positioning system and radar altimeter. [D] . Gray, Robert Anthony. 1999

机译：使用惯性导航系统，全球定位系统和雷达高度计的数字地形高程数据，在空中进行错误检测，以提高飞机的飞行安全性和垂直精度，从而提高飞行效率。
6. A First-Order Differential Data Processing Method for Accuracy Improvement of Complementary Filtering in Micro-UAV Attitude Estimation [O] . Xudong Wen, Chunwu Liu, Zhiping Huang, 2019

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7. A First-Order Differential Data Processing Method for Accuracy Improvement of Complementary Filtering in Micro-UAV Attitude Estimation [O] . Xudong Wen, Chunwu Liu, Zhiping Huang, 2019

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8. Digital filtering methods, with applications to satellite attitude determination in the presence of modelling errors Part I:theory [R] . C. R. Traas 1976

机译：数字滤波方法，应用于存在建模误差的卫星姿态确定第一部分：理论

Accuracy Improvement of Attitude Determination Systems Using EKF-Based Error Prediction Filter and PI Controller

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