Fuel-/Time-Optimal Relative Trajectories for a Satellite near a Perturbed, Elliptical Orbit
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33365
Reference29 articles.
1. AlfriendK. T.VadaliS. R.GurfilP.HowJ. P.BregerL. S., Spacecraft Formation Flying—Dynamics, Control and Navigation, Elsevier Astrodynamics Series, Butterworth-Heinemann, Burlington, MA, 2010, p. 8.
2. Variability of the bottom-simulating reflector (BSR) and its association with tectonic structures in the Chilean margin between Arauco Gulf (37°S) and Valdivia (40°S)
3. A decade of the Super Dual Auroral Radar Network (SuperDARN): scientific achievements, new techniques and future directions
4. State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference Orbit
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