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Vol. 156, Issue 9, September 2013, pp. 35-39

 

Bullet

 

Error Analysis of Rotary SINS Sensor
 
Zhenguo YUAN, Lin ZHAO

College of Automation, Harbin Engineering University, Harbin 150001, China
Tel.: 15946718088
E-mail: yuanzhenguodaohang@163.com

 

Received: 7 July 2013   /Accepted: 25 August 2013   /Published: 30 September 2013

Digital Sensors and Sensor Sysstems

 

Abstract: Using rotating modulation techniques for strap-down inertial navigation system (SINS) sensor is a self-compensation way to improve the accuracy. Inertial component errors can be effectively inhibited the inertial navigation system. The rotation principle and the error analysis of rotary SINS are presented in this paper, a two-axis rotary scheme is proposed. Simulation of rotary SINS calculation is made and rotation modulation is effective to the output of SINS sensor.

 

Keywords: Error analysis, Rotation, SINS, Rotary scheme.

 

 

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