Method for investigation of the optimal redundant gyros number based on reliability analysis

[1] Osder S.Practical view of redundancy management application and theory[J].Joural of Guidance,Control and Dynamics,1999,22(1):12-21 [2] 高飞,张洪钺.带马尔可夫参数容错控制系统的可靠性分析[J].北京航空航天大学学报,2007,33(3):302-306 Gao Fei,Zhang Hongyue.Reliability fault tolerant control system with Markovian parameters[J].Journal of Bejing University of Aeronautics and Astronautics,2007,33(3):302-306(in Chinese) [3] 张树侠,孙静.捷联式惯性导航系统[M].北京:国防工业出版社,1992:107-113 Zhang Shuxia,Sun Jing.Strapdown inertial navigation system[M].Beijing: National Defense Industry Press,1992:107-113(in Chinese) [4] Evans F A.Experimental strapdown redundant sensor inertial navigation system[J].J Spacecraft,1970,7(9):1070-1074 [5] Gilmore J P.A redundant strapdown inertial reference unit(SIRU)[J].J Spacecraft,1972,9(1):39-47 [6] Wilcox J C.Competitive evaluation of failure detection algorithms for strapdown redundant inertial instruments[J].J Spacecraft,1974,11(7): 525-530 [7] Seong Yun Cho,Chan Gook Park.Calibration of a redundant IMU .AIAA 2004-5123,2004(in Korea) [8] Vanderwerf K,Wefald K.Fault tolerant inertial navigation system .AIAA 88-4024-CP,1988 [9] Goodstein R.Failure detection technique for the inertial upper stage inertial navigation system .AIAA-1982-1622,1982 [10] Itzhack Y,Itzhack B,Harman R R.In-space calibration of a skewed gyro quadruplet .AIAA-2001-4152,2001 [11] 夏克寒,牟建华,夏至寒.多惯性仪表冗余系统方案设计及其关键技术 [J].导弹与航天运载技术,2007(6):21-24 Xia Kehan,Mu Jianhua,Xia Zhihan.Design of redundant system with multiple inertial measurement units and its key technologies[J].Missile And Space Vehcile,2007(6):21-24(in Chinese) [12] 王珍熙.可靠性、冗余及容错技术[M].北京:航空工业出版社,1991:1-5 Wang Zhenxi.Reliability,redundancy and fault tolerant techniques[M].Beijing:Aviation Industry Press,1991:1-5(in Chinese)