Multiple spacecraft rendezvous maneuvers by differential drag and low thrust engines
From MaRDI portal
Publication:642338
DOI10.1007/S10569-009-9240-3zbMath1223.70071OpenAlexW2130845747MaRDI QIDQ642338
Marcello Romano, Riccardo Bevilacqua, Jason S. Hall
Publication date: 26 October 2011
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10569-009-9240-3
Related Items (5)
Unnamed Item ⋮ Distributed optimal formation algorithm for multi-satellites system with time-varying performance function ⋮ Closed relative trajectories for formation flying with single-input control ⋮ Time-varying transformations for Hill-Clohessy-Wiltshire solutions in elliptic orbits ⋮ Hybrid planning for LEO long-duration multi-spacecraft rendezvous mission
Cites Work
This page was built for publication: Multiple spacecraft rendezvous maneuvers by differential drag and low thrust engines