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机译:无陀螺姿态确定系统的联邦非线性预测滤波
State Key Laboratory of Astronautic Dynamics, China Xi'an Satellite Control Center, Xi'an 710043, China,College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China, 63778 Unit of PLA, Jiamusi 154002, China,State Key Laboratory of Astronautic Dynamics, China Xi'an Satellite Control Center, Xi'an 710043, China;
State Key Laboratory of Astronautic Dynamics, China Xi'an Satellite Control Center, Xi'an 710043, China;
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China;
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China;
Gyroless spacecraft; Federated filter; Nonlinear predictive filter; Attitude determination;
机译:采用仿射LPV方法的航天器姿态确定系统的鲁棒H无限滤波
机译:用新型滤波方法确定船舶姿态的GPS / INS系统研究
机译:带有迭代非线性滤波器的单乘神经元模型预测发动机系统的可靠性和故障
机译:多传感器无陀螺姿态确定系统的联邦非线性预测滤波
机译:无陀螺航天器姿态确定系统的开发。
机译:适用于AUV综合导航系统的Adaptive Federated IMM滤波器
机译:使用联合Unscented Kalman滤波器的卫星容错系统姿态估算
机译:一种基于pC的磁力计专用无陀螺航天器姿态和速率确定系统