Optimal scheme of star observation of missile-borne inertial navigation system/stellar refraction integrated navigation
Author:
Affiliation:
1. School of Instrumentation Science and Opto-Electronics Engineering, Beihang University, Beijing 100191, China
Publisher
AIP Publishing
Subject
Instrumentation
Link
http://aip.scitation.org/doi/pdf/10.1063/1.5020226
Reference15 articles.
1. Autonomous satellite navigation using starlight refraction angle measurements
2. Horizon-Based Satellite Navigation Systems
3. Autonomous satellite navigation by stellar refraction
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1. Planning of refracted starlight observation based on observability analysis;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-09-01
2. Parameter optimization of a single-FOV-double-region celestial navigation system;Optics Express;2020-08-11
3. Comparison of geomagnetic aided navigation algorithms for hypersonic vehicles;Journal of Zhejiang University-SCIENCE A;2020-08
4. Attitude-correlated frames adding approach to improve signal-to-noise ratio of star image for star tracker;Optics Express;2019-05-17
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