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Prospective 3-axis attitude control using solar radiation pressure
Automatic Control in Aerospace, Volume # 18 | Part# 1
Authors
Okano, Yoshinobu; Sahara, Hironori; Funase, Ryu
Digital Object Identifier (DOI)
10.3182/20100906-5-JP-2022.00040
Page Numbers:
229-233
Index Terms
solar radiation pressure,3-axis attitude control,reflectivity control device
Abstract
Developing higher level 3-axis attitude control mechanics is desired in recent satellite attitude control systems, so that we propose an innovative 3-axis attitude control for recent and future satellites by using Reflectivity Control Device, RCD, which is capable of changing its reflectance according to applied voltage. This paper shows some examples of the high accuracy and stability 3-axis attitude control method using RCD, and indicates usefulness of this method with the 3-axis attitude control simulation including the torques generated by solar radiation pressure.
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