Adaptive Control of Large Space Structure (LSS)

概要

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A set of closely related topics, concerning the methodology of an optimal attitude maneuver control of satellite with flexible appendages, has been investigated : Such as mathematic model of coupled motion, pulse-mode control, optimal and programed maneuver, appendages' vibration damping through adaptive control and conventional control, adaptive identification (deterministic and stochastic) algorithm of time-varying modal coordinate parameters. A distinctive feature of the research was that only the actuators of central satellite attitude control system were assumed to perform both satellite attitude control and appendages' deformation control. Some aspects of interaction between control system characteristics and structure/configuration design parameters were outlined.
宇宙航空研究開発機構の論文