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Spacecraft position and attitude formation control using line-of-sight observations
2014
53rd IEEE Conference on Decision and Control
This paper studies formation control of an arbitrary number of spacecraft based on a serial network structure. The leader controls its absolute position and absolute attitude with respect to an inertial frame, and the followers control its relative position and attitude with respect to another spacecraft assigned by the serial network. The unique feature is that both the absolute attitude and the relative attitude control systems are developed directly in terms of the line-of-sight observations
doi:10.1109/cdc.2014.7039507
dblp:conf/cdc/WuL14
fatcat:yupbkstorjc3fdpbodedf3ptuu