文件名称:Indirect_Cancel
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- 上传时间：2013-03-16
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Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are
explained, and the main equations are described. A mathematical model of SINS is established, and its Matlab implementation
is developed. The theory is illustrated by six examples which are static status, straight line movement, circle movement, s-shape
movement, and two sets of real static data.
1. Introduction
explained, and the main equations are described. A mathematical model of SINS is established, and its Matlab implementation
is developed. The theory is illustrated by six examples which are static status, straight line movement, circle movement, s-shape
movement, and two sets of real static data.
1. Introduction
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Indirect_Cancel.m