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Vol. 16 No. 1 (2018)
Vol. 16 No. 1 (2018)

AUTONOMOUS NAVIGATION AND ATTITUDE CONTROL OF SPACECRAFTS ON NEAR-EARTH CIRCULAR ORBITS

DOI: 10.5937/jaes16-16479
Andronov Vladimir Germanovitch
Southwest State University, Kursk, Russia
Emelyanov Sergey Gennadievitch
Southwest State University, Kursk, Russia
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Published

2018-03-15

Section

Original Scientific Paper

How to Cite

[1]
A. V. Germanovitch and E. S. Gennadievitch, “AUTONOMOUS NAVIGATION AND ATTITUDE CONTROL OF SPACECRAFTS ON NEAR-EARTH CIRCULAR ORBITS”, JAES, vol. 16, no. 1, Mar. 2018, doi: 10.5937/jaes16-16479.
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Abstract

The paper reviews existing methods of spacecraft navigation and attitude control on near-earth orbits, including the methods utilizing earth-based external trajectory measurement stations, global navigation satellite systems, inertial on-board navigation systems and star trackers. The proposed method  is based on the obtaining and processing of a set of sky images on-board of a spacecraft that is moving along  a near-earth circular orbit.  Image processing results are used to find the coordinates, velocity and attitude of a space craft in inertial space.

Keywords

Star tracker
Autonomous navigation of spacecrafts
DOI: 10.5937/jaes16-16479
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