Wahba, G.A Least-Squares Estimation of Satellite Attitude. Problem 65-1[J].SIAM Review,1965,Vol.7,(No.3):409-409 [2] Gai, E, Daly, K., Harrison, J., and Lemos, L..Star-Sensor-Based Satellite Attitude/Attitude Rate Estimator[J].Journal of Guidance, Control, and Dynamics,1995,Vol. 8(No. 5):560-565 [3] Psiaki, M L., Martel F., Pal, P. K..Three-Axis Attitude Determination via Kalman Filtering of Magnetometer [J].DataJournal of Guidance, Control, and Dynamics,1990,Vol. 13( No. 3):506-514 [4] Challa, M, Natanson, G., and Wheeler, C..Simultaneous Determination of Spacecraft Attitude and Rates Using Only a Magnetometer[J].[C], Proceedings of the AIAA/AAS Astrodynamics Specialist Conference, AIAA, San Diego, CA,1996,:544-553 [5] Crassidis, J L., and Markley, F. L..Unscented Filtering for Spacecraft Attitude Estimation[J].Journal of Guidance, Control, and Dynamics,2003,Vol. 26(No. 4):536-542 [6] Cheng, Y, and Crassidis, J. L..Particle Filtering for Sequential Spacecraft Attitude [J].EstimationAIAA Guidance, Navigation, and Control Conference and Exhibit,2004,:1-18 [7] Oshman, Y, and Carmi, A..Attitude Estimation from Vector Observations Using a Genetic Algorithm-Embedded Quaternion Particle Filter[J].Journal of Guidance, Control, and Dynamics,2006,Vol. 29(No. 4):879-891 [8] Lu, P.Nonlinear Predictive Controllers for Continuous Systems[J].Journal of Guidance, Control, and Dynamics,1994,Vol. 17(No. 3):553-560 [9] Mook, D J., and Junkins, J. L..Minimum Model Error Estimation for Poorly Modeled Dynamic Systems [J].Journal of Guidance, Control, and Dynamics,1988,Vol. 3(No. 4):367-375 [10] Crassidis, J L., and Markley, F. L..Predictive Filtering for Attitude Estimation Without Rate Sensors[J].Journal of Guidance, Control, and Dynamics,1997,Vol. 20(No. 3):522-527 [11] Arulampalam, M S., Maskell, S., Gordon, N., and Clapp, T..A tutorial on Particle Filters for Online Nonlinear/Non-Guassian Bayesian Tracking[J].IEEE Transactions on Signal Processing,2002,Vol. 50(No. 2):174-185 [12] 姜雪原, 马广富, 胡庆雷.基于粒子滤波和UKF联合滤波的卫星姿态估计[J].哈尔滨工业大学学报,2007,Vol. 39(No. 3):337-341 [13]Jiang Xue Yuan, Ma Guang Fu, Hu Qing Lei..Spacecraft attitude estimation from vector measurements using particle filter integrated with unscented Kalman filter[J].Journal of Harbin Institute of Technology,2007,Vol. 39(No. 3):337-341
