作者: Ying Siang Ban , Renuganth Varatharajoo , Michael Ovchinnikov
DOI: 10.1016/J.ACTAASTRO.2012.02.013
关键词: Attitude control system 、 Engineering 、 Energy (signal processing) 、 Optimal control 、 Control theory 、 Work (physics) 、 Control engineering 、 Attitude control
摘要: Abstract This addendum is an extension of a series research work on the combined energy and attitude control system (CEACS) for small satellites. Previous works appeared in Acta Astronautica showed that CEACS able to simultaneously perform storage task. focuses enhancement by employing H 2 optimal method. Governing equations describing architecture are established. Numerical treatments performed order validate option.