Unconstrained Direct Optimization of Spacecraft Trajectories Using Many Embedded Lambert Problems
Sign Up to like & getrecommendations! Published in 2021 at "Journal of Optimization Theory and Applications"
DOI: 10.1007/s10957-021-01884-1
Abstract: Direct optimization of many-revolution spacecraft trajectories is performed using an unconstrained formulation with many short-arc, embedded Lambert problems. Each Lambert problem shares its terminal positions with neighboring segments to implicitly enforce position continuity. Use of… read more here.
Keywords: direct optimization; spacecraft; lambert problems; optimization ... See more keywords