[1] SABLYNSKI R,PORDON R.A report on the flight of Delta II's redundant inertial flight control assembly (RIFCA)[C]//IEEE 1998 Position Location and Navigation Symposium,1998:98CH36153. [2] 彭蓉,严恭敏,秦永元.箭载捷联惯导系统水平自对准的两种实用方法[J].中国惯性技术学报,2009,17(4):428-435.PENG R,YAN G M,QIN Y Y.Two practical methods of autonomous leveling alignment for launch vehicle SINS[J].Journal of Chinese Inertial Technology,2009,17(4):428-435(in Chinese). [3] 崔潇,秦永元,严恭敏,等.基于矩阵卡尔曼滤波的捷联惯导初始对准算法[J].中国惯性技术学报,2018,26(5):585-590.CUI X,QIN Y Y,YAN G M,et al.Initial alignment algorithm for SINS based on state matrix Kalman filter[J].Journal of Chinese Inertial Technology,2018,26(5):585-590(in Chinese). [4] 郭泽,缪玲娟,赵洪松.一种改进的强跟踪UKF算法及其在大方位失准角初始对准中的应用[J].航空学报,2014,35(1):203-214.GUO Z,MIAO L J,ZHAO H S.An improved strong tracking UKF algorithm and its application in SINS initial alignment under large azimuth misalignment angles[J].Acta Aeronautica et Astronautica Sinica,2014,35(1):203-214(in Chinese). [5] HE H Y,XU J N,LI J S,et al.Improved fast backtracking alignment approach for strapdown inertial navigation system[J].Journal of Chinese Inertial Technology,2015,23(2):179-183. [6] 郭士荦,许江宁,李峰.强跟踪CKF及其在惯导系统初始对准中的应用[J].中国惯性技术学报,2017,25(4):436-441.GUO S L,XU J N,LI F.Strong tracking cubature Kalman filter for initial alignment of inertial navigation system[J].Journal of Chinese Inertial Technology,2017,25(4):436-441(in Chinese). [7] BAR-ITZHACK I Y,HARMAN R R.In-space calibration of a skewed gyro quadruplet[J].Journal of Guidance,Control,and Dynamics,2002,25(5):852-859. [8] PITTELKAU M E.Calibration and attitude determination with redundant inertial measurement units[J].Journal of Guidance,Control,and Dynamics,2005,28(4):743-752. [9] PITTELKAU M E.Cascaded and decoupled RIMU calibration filters[J].The Journal of the Astronautical Sciences,2006,54:449-466. [10] YUKSEL Y,EL-SHEIMY N.An optimal fusion method for skew-redundant inertial measurement units[J].Journal of Applied Geodesy,2011,5(2):99-115. [11] 秦永元,张洪钺,汪叔华.卡尔曼滤波与组合导航原理[M].西安:西北工业大学出版社,2015:63-68.QIN Y Y,ZHANG H Y,WANG S H.Theory of Kalman filter and integrated navigation[M].Xi'an:Northwestern Polytechnical University Press,2015:63-68(in Chinese). [12] GILMORE J P.SIRU development final report[R].Washington,D.C.:NASA,1973:11-16. [13] 秦永元.惯性导航[M].北京:科学出版社,2006:240-241.QIN Y Y.Inertial navigation[M].Beijing:Science Press,2006:240-241(in Chinese). [14] 梅春波,秦永元,游金川.SINS在大失准角条件下的非线性量测初始对准算法[J].宇航学报,2016,37(3):1-7.MEI C B,QIN Y Y,YOU J C.Nonlinear measurement based SINS initial alignment for large misalignment angles[J].Journal of Astronautics,2016,37(3):1-7(in Chinese). [15] 夏益霖,吴家驹.航天发射的低频振动环境及其模拟[J].强度与环境,1998(1):1-8.XIA Y L,WU J J.Low-frequency vibration environment and its simulation for aerospace launch[J].Structure & Environment Engineering,1998(1):1-8(in Chinese). |