Title :
Comparison of Three Transfer Alignment Methods in Marine Missile SINS
Author :
Zhou Nai-xin ; Wang Si ; Deng Zheng-long
Author_Institution :
Dept. of Control Sci. & Eng., Harbin Inst. of Technol., China
Abstract :
Three transfer alignment methods in marine missile SINS are compared by simulations. Simulation results show that velocity plus angular rate matching method is better than velocity matching method. Adopting simple velocity matching method, although eastern and northern level wander angles can be estimated accurately, azimuth wander angle isn´t estimated ideally. This method is suitable to level directional alignment; velocity plus angular rate matching and velocity plus attitude change matching both are faster in transfer alignment, but velocity plus angular rate matching is sensitive to the noise and the structure flexibility deform greatly, the alignment accuracy of this method is lower, it is suitable to SINS in tactical missile that require lower alignment accuracy; Velocity plus attitude change matching can quicken convergence speed, decrease oscillation range of the filtered value, and increase estimation accuracy. Simulation results show that this method can solve transfer alignment question on moving base successfully.
Keywords :
angular velocity control; attitude control; inertial navigation; inertial systems; marine systems; missile control; Kalman filter; SINS; angular rate matching method; attitude change matching; azimuth wander angle; marine missile; tactical missile; three transfer alignment methods; velocity matching method; Azimuth; Convergence; Differential equations; Earth; Inertial navigation; Marine technology; Master-slave; Missiles; Noise level; Silicon compounds; Dynamic base; Kalman filter; Matching method; SINS; Transfer alignment;
Conference_Titel :
Control Conference, 2006. CCC 2006. Chinese
Conference_Location :
Harbin
Print_ISBN :
7-81077-802-1
DOI :
10.1109/CHICC.2006.280967