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Titlebook: Satellite Formation Flying; Relative Dynamics, F Danwei Wang,Baolin Wu,Eng Kee Poh Book 2017 Springer Science+Business Media Singapore 2017

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Dynamic Models of Satellite Relative Motion Around an Oblate Earth,Accurate dynamic model of relative motion is basic and critical to the study of satellite formation flying. So accurate nonlinear and linear dynamic models of satellite relative motion considering .. perturbation are derived in this chapter.
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Nonlinear Optimization of Low-Thrust Trajectory for Satellite Formation,This chapter presents a method to determine fuel-optimal trajectories for satellite formation maneuver using low-thrust continuous propulsion.
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Decentralized Control for Attitude Synchronization Under Undirected Communication Topology,This chapter developed two decentralized coordinated attitude control laws for attitude synchronization and tracking problem with undirected (it is also named bidirectional) inter-satellite communication topology.
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Decentralized Control for Attitude Synchronization Under Directed Communication Topology,This chapter developed two decentralized coordinated attitude control laws for attitude synchronization and tracking problem with directed inter-satellite communication topology. Firstly, an adaptive sliding mode control law is developed against inertia matrix uncertainties and external disturbances.
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Conclusions,The primary motivation for satellite formation flying is that multiple small satellites can work together in a group to accomplish the mission of a larger, usually more expensive, satellite.
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Danwei Wang,Baolin Wu,Eng Kee PohSystematically describes the concepts and principles for satellite formation from relative dynamics, formation design, and formation maneuvers to formation keeping and attitude synchronization.Propose
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