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The main contribution of this paper is that, to improve the performance properties of satellite attitude manoeuvre controlled by nonlinear stabilizing control law derived from standard adaptive back-stepping method, a hybrid control approach is developed to guarantee the stability of system in global sense while improving control performance of satellite attitude manoeuvre problem in a local region...
In this paper, the Missile Early Warning Satellite Attitude Control problem is introduced, A two step incorporated and systematic method for modeling and control of missile early warning satellite is formulated. Firstly, the nonlinear dynamic and kinematics equation of the missile early warning satellite are reformulated to linear parameter variation (LPV) system. Secondly, based on the LPV model,...
The main contribution of this paper is that, to improve the performance properties of early-warning satellite controlled by standard adaptive back-stepping controller, a hybrid control approach is developed to guarantee the stability of system in global sense while improving control performance of early-warning satellite attitude manoeuvre problem in a local region. Firstly, using the adaptive back-stepping...
The main contribution of this paper is that, for the first time, a two step incorporated and systematic method for modeling and control of large angle maneuvers of a satellite is formulated by using convex optimization. Firstly, the nonlinear dynamic and kinematic equation of the satellite are represented by linear parameter variation (LPV) system. Secondly, by using of the Sum of Squares (SOS) technique,...
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