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THE CORRECTION FOR THE BASIC AXIS ERROR OF THE INERTIAL TERMINAL GUIDANCE ON THE ANTIRADAR MISSILE
Author(s): 
Pages: 30-37
Year: Issue:  1
Journal: Aerospace Control

Keyword:  Antiradar missile Kalmanfilter Guidance error Correction;
Abstract: In this paper, a generalized kalman filtering method is used on an air to ground antiradar missile to slove the correction problem for the basic axis direction error of inertial terminal gnidance. Finally, a practical example about the missile motion model is given.
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