Now showing items 1-2 of 2
Control of relative attitude dynamics of a formation flight using model-error control synthesis
A robust approach to control, called Model Error Control Synthesis (MECS), is applied to the relative attitude between a formation-flight of spacecraft. This technique combines a nominal controller with a model error ...
Control and Kalman filtering for relative dynamics of a formation of uninhabited autonomous vehicles
An extended Kalman filter for estimation of relative position and relative attitude between a pair of uninhabited autonomous vehicles is developed. Line of sight measurements are taken using visual navigation beacons. ...