Terminal One Axis Stabilization Properties of a Spinning Satellite Employing Simple Magnetic Attitude Control
نویسندگان
چکیده
A spin stabilized satellite reorientation maneuver in the inertial space is investigated. Spin axis pointing and nutation damping magnetic attitude control algorithms are utilized. Evolutionary equations for oscillations of a symmetrical near required position derived. The exact solution wobble amplitude obtained averaged motion. angles relative to direction analyzed. Optimal gain found maneuver. Theoretical results verified with numerical simulation.
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ژورنال
عنوان ژورنال: Mathematics
سال: 2023
ISSN: ['2227-7390']
DOI: https://doi.org/10.3390/math11061530