Fast Attitude Maneuvers for NASA’s Lunar Reconnaissance Orbiter: Practical Flight Application of Attitude Guidance using Birkhoff Pseudospectral Theory and Hamiltonian Programming-Reference-Cited by-同舟云学术

Fast Attitude Maneuvers for NASA’s Lunar Reconnaissance Orbiter: Practical Flight Application of Attitude Guidance using Birkhoff Pseudospectral Theory and Hamiltonian Programming

Published:2024-04 Issue:2 Volume:44 Page:26-54
ISSN:1066-033X
Container-title:IEEE Control Systems
language:
Short-container-title:IEEE Control Syst.

Author:

Karpenko Mark¹^ORCID,Halverson Julie K.²,Tedla Yohannes³,Lippman Travis¹,Han Kyaw¹,Ross I. Michael¹,Barker Michael K.⁴,Robinson Mark S.⁵,Carter Winston⁶,Boyd Aaron K.⁶,Patterson G. Wesley⁷,O’Shea Colleen M.⁸,Turner F. Scott⁷,Poffenbarger Ryan T.⁸,Dennehy Cornelius J.²,VanZwieten Tannen⁹,Wolf Aron A.¹⁰

Affiliation:

1. Naval Postgraduate School, Monterey, CA, USA

2. NASA’s Goddard Space Flight Center Greenbelt, MD, USA

3. KBRwyle, Greenbelt, MD, USA

4. Solar System Exploration Division of NASA’s Goddard Space Flight Center Greenbelt, MD, USA

5. School of Earth and Space Exploration, Arizona State University, Tempe, AZ, USA

6. Lunar Reconnaissance Orbiter Science Operations Center, Arizona State University, Tempe, AZ, USA

7. Johns Hopkins University Applied Physics Laboratory, Laurel, MD, USA

8. Johns Hopkins Applied Physics Laboratory, Laurel, MD, USA

9. NASA John F. Kennedy Space Center, Merritt Island, FL, USA

10. NASA Jet Propulsion Laboratory Pasadena, CA, USA

Publisher