@inproceedings{c7cc3367f6bb4af2b6261c7bc3f6d66e,
title = "Simulating gyro of strapdown inertial navigation system based on star sensor",
abstract = "In inertial navigation system, gyro is used to measure the angular velocity of carrier relative to inertial space for achieve attitude matrix updated in real time. Gyro difficult to eliminate the error, results in strapdown inertial navigation system precision decrease with time. Star sensor is a high-precision attitude measuring instrument and don't require any priori information, the attitude date can be provided by star sensor. Thus, gyro is simulated by star sensor in order to improve the precision of strapdown inertial navigation system.",
keywords = "Angular velocity, Gyro, Star sensor, Strapdown inertial navigation system",
author = "Wei Gao and Lei Zhang",
year = "2012",
doi = "10.4028/www.scientific.net/AMM.182-183.1090",
language = "英语",
isbn = "9783037854266",
series = "Applied Mechanics and Materials",
pages = "1090--1094",
booktitle = "Applied Mechanics and Mechatronics Automation",
note = "2012 International Applied Mechanics, Mechatronics Automation Symposium, IAMMAS 2012 ; Conference date: 07-09-2012 Through 09-09-2012",
}