Mathematical Model and Matlab Simulation of Strapdown Inertial Navigation System | Zendy

Wen Zhang | Zendy; Mounir Ghogho | Zendy; Baolun Yuan | Zendy

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Mathematical Model and Matlab Simulation of Strapdown Inertial Navigation System

Author(s) -

Wen Zhang,

Mounir Ghogho,

Baolun Yuan

Publication year - 2012

Publication title -

modelling and simulation in engineering

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.264

H-Index - 20

eISSN - 1687-5591

pISSN - 1687-5605

DOI - 10.1155/2012/264537

Subject(s) - matlab , accelerometer , inertial navigation system , movement (music) , inertial frame of reference , control theory (sociology) , inertial measurement unit , computer science , control engineering , line (geometry) , simulation , engineering , artificial intelligence , mathematics , physics , acoustics , classical mechanics , geometry , control (management) , operating system

Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros andaccelerometers 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, straightline movement, circle movement, s-shape movement, and two sets of real static data

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