Reducing Vibration Related Error in INS Performance by Limiting Measurement Bandwidth
Publish place: Second Iranian Conference on Avionics System
Publish Year: 1393
Type: Conference paper
Language: English
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Document National Code:
ICADI02_014
Index date: 1 May 2015
Reducing Vibration Related Error in INS Performance by Limiting Measurement Bandwidth abstract
In this paper, random vibration trial, as the most important environmental test for an inertial navigation system (INS), was investigated from the navigation point of view. Effect of random vibration test on INS performance was inspected to specify how random vibration increased the navigation error. A simple practical solution was proposed to decrease the vibration-related error in position and velocity estimation. Proposed method was simple, compatible, and real-time and had a hardware implementation without needing extra computations and accessories. Side effects of the proposed technique were examined; it was proved that they did not cause any restriction and had no disruptive effect in practice. Actual data of navigation grade INS were used to prove these claims.
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Reducing Vibration Related Error in INS Performance by Limiting Measurement Bandwidth authors
S.H Taghavi
Department of Electrical and Computer Engineering Shahid Rajaee University Lavizan, Tehran,Iran
A Abdoli
Department of Electrical Engineering Iran University of Science and Technology Narmak, Tehran, Iran
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