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Robust distributed attitude synchronization of multiple three-DOF experimental helicopters
2015
Control Engineering Practice
Multiple experimental three-degrees-of-freedom (three-DOF) helicopters that are equipped with active disturbance systems constitute an attractive platform to validate robust control strategies. In this paper, a distributed synchronization controller is developed for such a platform, where each helicopter is subjected to unknown model uncertainties and external disturbances, and the desired trajectories are generated online, communicated through a network and not accessible by all helicopters.
doi:10.1016/j.conengprac.2014.12.003
fatcat:jpwslvrnafb5pnzxa7qkd4zpma