A paper describes algorithms for guidance and control (G&C) of a spacecraft maneuvering near a planet, moon, asteroid, comet, or other small astronomical body. The algorithms were developed following a model-predictive-control approach along with a convexification of the governing dynamical equations, control constraints, and trajectory and state constraints.
Pseudo-Waypoint Guidance for Proximity Spacecraft Maneuvers
2007-06-01
Miscellaneous
No indication
English
Waypoint-Optimized Closed-Loop Guidance for Spacecraft Rendezvous in Relative Motion
BASE | 2017
|British Library Conference Proceedings | 2012
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