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