Clearance Center Inc. / Aeronautics and Astronautics Inc. / /
Currency
USD / GBP / cent / / /
Facility
American Institute / Jonathan P. How‡ Massachusetts Institute of Technology / Eccentric Orbits G¨okhan Inalhan¤ Stanford University / / /
IndustryTerm
control algorithm / equations/solutions / th satellite / differential energy matching conditions / nontrivial periodic solution / energy level / deep-space and orbital applications / differential energy matching / differential energy equalization section / differential energy error / differential energy matching condition / differential energy / closed-form solutions / differential energy errors / periodic solution / unforced closed-form solutions / homogenous solution / differential energy corrections / periodic solutions / no-drift solution / homogenous solutions / zero-differential energy condition / related no-drift solutions / differential energy equalization condition / distributed coordinating satellite concept / closed-form solution / space applications / level mission management / published solutions / monolithic satellite / analytic solution / imaging / energy difference / reference satellite / formation-keeping algorithm / /
Organization
Nanosat Constellation Trailblazer mission / Copyright Clearance Center / U.S. Air Force / American Institute / Earth Orbiter-1 mission / Stanford University / National Aeronautics and Space Administration / Massachusetts Institute of Technology / Department of Aeronautics and Astronautics / /
Person
Michael Tillerson / Cross-Track As / /
Position
Research Assistant / Vp / Assistant / Associate Professor / /
Product
Pyle P32 Television / /
ProgrammingLanguage
C / /
ProvinceOrState
California / Massachusetts / /
SportsLeague
Stanford University / /
Technology
enabling technology / aV / key technology / control algorithm / http / simulation / html / ying technologies / formation-keeping algorithm / /
JOURNAL OF GUIDANCE, CONTROL, AND DYNAMICS Vol. 25, No. 1, January – February 2002 Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits G¨okhan Inalhan¤