A Novel SINS/CNS Integrated Navigation Algorithm used in a Ballistic Missile

The position and velocity errors are divergent of traditional navigation algorithms used in ballistic missile for it cannot estimate the bias of accelerometer precisely. To solve this problem, a novel SINS/CNS integrated navigation algorithm is proposed in this paper, which adds high angle error, az...

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Bibliographic Details
Published inInternational Journal of Security and Its Applications Vol. 9; no. 9; pp. 65 - 76
Main Authors Yang, Lihua, Li, Baolin, Ge, Lei
Format Journal Article
LanguageEnglish
Published 30.09.2015
Subjects
bias of accelerometer
azimuth angle
integrated navigation
height angle
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ISSN1738-9976
DOI10.14257/ijsia.2015.9.9.07

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Table of Contents:
  • Abstract 1. Introduction 2. The Definition of Reference Frames 3. Operating Principle of System 4. System Model 4.1. State Equation 4.2. Measurement Equation 5. Simulations and Analysis 5.1. Simulation Conditions 5.2. Simulation Results and Analysis 6. Conclusions References