Optimisation of Aerospace System Control with Constraints on Return Trajectories of Spent Elements

Details Optimisation of Aerospace System Control with Constraints on Return Trajectories of Spent Elements Optimisation of Aerospace System Control with Constraints on Return Trajectories of Spent Elements

Feb 2000

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2000esasp.425..325f&link_type=gif

Spacecraft Guidance, Navigation and Control Systems, Proceedings of the 4th ESA International Conference, held 18-21 October, 19

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