A Programming Method for Spacecraft All-Phase Rendezvous and Docking Based on Constraint Rules
A programming method based on constraint rules is designed for the rendezvous and docking process in the field of manned spaceflight.The flight program is divided into flight control events based on the correlations,and the event constraints are decoupled from time or cycles to form a planning configuration system suitable for all phase rendezvous and docking.Through a set of configurations,the planning generation of each normal and emergency branch program is achieved.Compared with traditional time-series based programming methods,the designed method improves the adaptability of the configuration and the program design efficiency,and provides reference for subsequent rendezvous and docking program planning program design.
all-phaserendezvous and dockingconstraint ruleprogramming and designspacecraft