Jianting Lv

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In this paper we consider coordinated control problem of a spacecraft formation consisting of two spacecrafts. Two sliding control schemes are designed to guarantee attitude tracking and synchronization of formation spacecrafts under uncertainty in spacecraft inertia parameters and external disturbance. The second adaptive sliding mode tracking control(More)
In this paper we consider attitude coordination control problem of spacecraft formation flying. Two coordinated attitude tracking control schemes subject to control input constraints are addressed here. We first present the full-state feedback control scheme that allows each spacecraft to align their attitude and track the desired trajectory. Then the(More)
This paper deals with the problem of attitude tracking control of rigid satellite subject to external disturbance, and parametric uncertainty. An adaptive controller is designed to implement real-time identification for inertia parameters and control parameter is adjusted dynamically. A detail stability analysis of the close loop system is included and(More)
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