机译:程序四元数在航天器姿态调节控制中的解析算法
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China,Beijing Aerospace Automatic Control Institute, Beijing 100854, China;
Beijing Aerospace Automatic Control Institute, Beijing 100854, China;
Key Laboratory of Education Ministry for Image Processing and Intelligent Control, Department of Control Science and Engineering, Huazhong University of Science and Technology Wuhan 430074, China;
Key Laboratory of Education Ministry for Image Processing and Intelligent Control, Department of Control Science and Engineering, Huazhong University of Science and Technology Wuhan 430074, China;
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;
Key Laboratory of Education Ministry for Image Processing and Intelligent Control, Department of Control Science and Engineering, Huazhong University of Science and Technology Wuhan 430074, China;
space vehicle; dynamic modeling; program quaternion; attitude control;
机译:使用季铵刚体(航天器)重新定向问题的解析解决方案
机译:基于四元数模型的航天器控制系统LQR解析设计
机译:用于航天器姿态控制的四元流的广义超扭曲算法
机译:具有离散变换结构的航天器对控制算法的计算机辅助建模与分析合成
机译:航天器姿态控制程序:航天器姿态确定和控制模拟程序。
机译:一种新的基于四元的Kalman滤波器用于使用最优季脉算法的第二估计和具有惯性和磁传感器的关节角约束方法的人体运动跟踪
机译:航天器接近操作的双季度分析LQR控制设计