EVALUATION OF FRONT MORPHOLOGICAL DEVELOPMENT OF REACTIVE SOLUTE TRANSPORT USING BEHAVIOR DIAGRAMS



Minimum-Learning-Parameter-Based Fault-Tolerant Control for Spacecraft Rendezvous With Unknown Inertial Parameters

In this paper, robust Batteries control strategies are explored to solve the problem of rendezvous maneuver for rigid spacecraft exposed to the external disturbance, actuator faults and unknown inertial parameters.To pursue the control objective, two adaptive controllers are constructed via the sliding mode control (SMC) technology.Firstly, a basic

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