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IssuesArchive of Issues2019-2pp.157-168

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Yu.N. Chelnokov, "Inertial Navigation in Space Using the Regular Quaternion Equations of Astrodynamics," Mech. Solids. 54 (2), 157-168 (2019)
Year 2019 Volume 54 Number 2 Pages 157-168
DOI 10.3103/S0025654419030063
Title Inertial Navigation in Space Using the Regular Quaternion Equations of Astrodynamics
Author(s) Yu.N. Chelnokov (Institute of Precision Mechanics and Control, Russian Academy of Sciences, Saratov, 410028 Russia, ChelnokovYuN@gmail.com)
Abstract Quaternion equations are proposed for the ideal operation of spatial inertial navigation systems with an azimuthally stabilized platform and a gyrostabilized platform that keeps its orientation invariant in inertial space, quaternion equations for the ideal operation of strapdown inertial navigation systems in the regular four-dimensional Kustaanheimo–Stiefel variables with consideration of zonal, tesseral, and sectorial harmonics of the Earth’s gravitational field. The equations are dynamically similar to the regular equations of perturbed spatial two-body problem in the Kustaanheimo–Stiefel variables, which enables to use the results obtained in regular celestial mechanics and astrodynamics theory in inertial astronavigation. The development of operational algorithms for these navigation systems using these equations is considered.
Keywords astrodynamics, spacecraft, inertial navigation, platform and strapdown inertial navigation systems, regular quaternion equations of inertial navigation, Kustaanheimo–Stiefel variables
Received 03 June 2018
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