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In this thesis, a new designcalled Family Swarm was presented, it overcomes the disadvantages of the Fractionated Imaging Satellite Cluster.To select the most suitable attitude and orbit control algorithm for the new swarm mission,a comparison is done between the commonly used control algorithms in attitude and orbit control systems,such as; propor...
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Abstract This paper investigates the attitude‐orbit integrated modeling and robust control of flexible spacecraft with input saturation. First, the dual‐number method is employed to describe the dynamic model of the spacecraft with the flexible appendage. Then, a fast terminal sliding mode control law is designed to stabilize the attitude‐orbit con...