Summaries - Office of Research & Innovation
Research Summaries
Back Optimal Spacecraft Maneuvering in the Proximity of a Circular or Elliptic Reference Orbit
Fiscal Year | 2020 |
Division | Graduate School of Engineering & Applied Science |
Department | Mechanical & Aerospace Engineering |
Investigator(s) | Romano, Marcello |
Sponsor | Department of Defense Space (DoD) |
Summary | Optimal proximity maneuvers enable to change the dynamic state of an orbiting spacecraft. This capability can be critical for many space missions in order to increase their effectiveness and resilience. |
Keywords | |
Publications | Publications, theses (not shown) and data repositories will be added to the portal record when information is available in FAIRS and brought back to the portal |
Data | Publications, theses (not shown) and data repositories will be added to the portal record when information is available in FAIRS and brought back to the portal |