Research Summaries

Back Dynamics, Guidance and Experimentation of Small Satellite Attitude and Proximity Maneuvers

Fiscal Year 2011
Division Graduate School of Engineering & Applied Science
Department Mechanical & Aerospace Engineering
Investigator(s) Romano, Marcello
Sponsor Air Force Research Laboratory (Air Force)
Summary The objective of this research is to support the modeling and simulation efforts of spacecraft dynamics and control within RVES. The research focuses on the autonomous guidance and control of a spacecraft for proximity maneuvering and attitude control. Inverse dynamics based guidance approach will be extensively studied through numerical simulations and experiment on the Spacecraft Robotics Laboratory flat floor.
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