[1] ZHANG T G, WANG X P, WANG L X.Strap-down inertial navigation technology[M].Beijing:National Defence Industry Press, 2010.
[2] QIN Y Y.Inertial navigation[M].Beijing:Science Press, 2006.
[3] YANG S, FANG J C.A single sample rotation vector attitude algorithm[J].Journal of Astronautics, 2010, 31(3):780-785.
[4] GUO F S, YU Y F, LIU S P, et al.Study on attitude algorithm for strapdown inertial navigation system[J].Aerospace Control, 2010, 28(1):37-39.
[5] LIU W, XIE X H, LI S Y.Coning algorithm for strap-down inertial navigation system[J].Journal of Nanjing University of Aeronautics & Astronautics, 2004, 36(3):348-352.
[6] LI Z T, WU T J, MA L H.A SINS coning compensation algorithm based on gyro error post compensation[J].Journal of Shanghai Jiaotong University, 2011, 45(3):388-392.
[7] BROTZ J E.A new mathematical formulation for strap-down inertial navigation[J].IEEE Transactions on Aerospace and Electronic System, 1971, 7(1):61-66.
[8] MILLER R B.A new strap-down attitude algorithm[J].Journal of Guidance, Control and Dynamics, 1983, 6(4):287-291.
[9] MAN Z G, ZHOU B L, WU Z Y.An improved extended rotation vector attitude algorithm[J].Fire Control & Command Control, 2009, 34(2):117-119.
[10] ZHOU G H, ZHENG R R, ZHONG L.Research on attitude algorithm of mini unmanned helicopter strapdown inertial navigation system[J].Microcomputer Information, 2010, 26(19):167-168.
[11] HE Y, REN K S, NAN Y.Research on optimal six-sample rotation vector algorithms for SINS attitude updating[J].Journal of Nanchang Hangkong University, 2008, 22(2):35-38.
[12] WEI X H, ZHANG C X, ZHU K B.A high accuracy coning compensate algorithm by angular velocity[J].Journal of Beijing University of Aeronautics & Astronautics, 2005, 31(12):1312-1316.