Micro-vibration caused by disturbance sources onboard spacecraft can severely degrade
the working environment of high-precision space optical instruments (HPSOIs) in orbit …

The attitude tracking control problem of a rigid spacecraft with external disturbances and an
uncertain inertia matrix is addressed using the adaptive control method. The adaptive …

In the past decade there has been an upswing in the interest of flywheel energy storage
systems for space applications. This interest has been driven by limitations of chemical …

In this paper, we consider the leader-following consensus problem for a multiple rigid
spacecraft system whose attitude is represented by the unit quaternion. Most results on this …

In this technical note, we deal with the attitude tracking and disturbance rejection problem of
spacecraft for a class of persistent disturbances with unbounded energy which include the …

This paper presents a unified synchronization framework with application to precision
formation flying spacecraft. Central to the proposed innovation, in applying synchronization …

A SINGLE-GIMBAL control moment gyro (CMG) system is regarded as an effective torque
generator for attitude control both for large space stations and small agile satellites because …

This book discusses all spacecraft attitude control-related topics: spacecraft (including
attitude measurements, actuator, and disturbance torques), modeling, spacecraft attitude …

Attitude control and power storage subsystems are two of the essential utilities provided on a
spacecraft. As they comprise a significant fraction of a spacecraft mass, a synergism concept …

Abstract Combined Energy and Attitude Control System (CEACS) reduces the size and
mass budgets of typical satellites and consequently, increases their payload capacity …