SUN Zhi-ming.Applications of silicon accelerometer in guided projectile test[J].Journal of Projectiles,Rockets,Missiles and Guidance,2003,23(1):91-93.(in Chinese)
[6]
FLECK V,SOMMER E.Study of real-time filtering for an inertial measurement unit with magnetometer in a 155 mm projectile[C]//IEEE/ION Position,Location and Navigation Symposium.Coronado,USA:IEEE,2006:83-87.
[7]
BROWN T G.Harsh military environments and microelectromechanical devices[C]//The Second IEEE International Conference on Sensors.Toronto:IEEE,2003:753-760.
[8]
杨慧娟.旋转稳定弹轴向加速度测量误差模型分析[J].弹道学报,2013,25(4):48-52.
[9]
YANG Hui-juan.Measnrement error model analysis of axial acceleration for rotational stability bomb[J].Journal of Ballistics,2013,25(4):48-52.(in Chinese)
[10]
CRASSIDIS J L,MARKLEY F L.Unscented filtering for spacecraft attitude estimation[J].Journal of Guidance,Control,and Dynamics,2003,26(4):536-542.
[11]
SIMON H.Kalman filtering and neural networks[M].New York:John Wiley & Sons,Inc,2001:215-218.
[12]
LEONARD C.Modified projectile linear theory for rapid trajectory prediction[J].Journal of Guidance,Control,and Dynamics.2005,28(5):375-377.
