The Kalman filter in transfer alignment of inertial guidance systems.
Author:
Affiliation:
1. The Analytic Sciences Corporation, Reading, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29445
Reference3 articles.
Cited by 26 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
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2. On the error state selection for stationary SINS alignment and calibration Kalman filters – part I: Estimation algorithms;Aerospace Science and Technology;2017-02
3. Transfer alignment problem: Algorithms and design issues;Gyroscopy and Navigation;2013-07
4. Observability Analysis Techniques on Inertial Navigation Systems;Journal of System Design and Dynamics;2012
5. Experimental Feasibility of the In-Drilling Alignment Method for Inertial Navigation in Measurement-While-Drilling;IEEE Transactions on Instrumentation and Measurement;2011-03
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