Author:
Ciarcià Marco,Grompone Alessio,Romano Marcello
Reference15 articles.
1. M. Ciarcià, M. Romano, Spacecraft proximity maneuver guidance based on inverse dynamic and sequential gradient-restoration algorithm, in: Proceedings of the AIAA Astrodynamics Specialist Conference, 2011.
2. M. Ciarcià, M. Romano, Suboptimal guidance for orbital proximity maneuver with path constraints capability, in: Proceedings of the AIAA Guidance Navigation and Control Conference, 2012.
3. Optimal rendezvous trajectories of a controlled spacecraft and a tumbling object.;Boyarko;AIAA J. Guid. Control Dynam,2011
4. Online generation of quasi-optimal spacecraft rendezvous trajectories;Bevilacqua;Acta Astronaut.,2009
5. Ad-hoc wireless networking and shared computation based upon linux for autonomous multi-robot systems;Bevilacqua;AIAA J. Aerosp. Comput. Inf. Commun.,2009
Cited by
25 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献