Spacecraft Adaptive Attitude and Power Tracking with Variable Speed Control Moment Gyroscopes

By Hyungjoo Yoon, Panagiotis Tsiotras. 2002

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Inverse optimal adaptive control for attitude tracking of spacecraft (2005, background): “In comparison with the work of [8]–[13], the adaptive control law in this paper is inverse optimal with respect to a meaningful cost functional involving tracking errors and control efforts.”
Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control (2009, background): “A TTITUDE control of spacecraft systems has been a benchmark control problem and has been extensively studied under various assumptions and scenarios [1], [6], [12], [17], [20], [21].”
Survey of Theory and Steering Laws of Single-Gimbal Control Moment Gyros (2007, methodology): “Recently, variable-speed CMGs (VSCMG), which were once studied as integrated power and attitude control devices [10], have been revived for their singularity avoidance capability [11–15].”
Application of Synchronization to Formation Flying Spacecraft: Lagrangian Approach (2008, background): “First, we introduce the generalized form to explore the increasing interest in agile imaging spacecraft using a control moment gyroscope (CMG) [25] and a variable speed control moment gyroscope (VSCMG) [38].”