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Analytic expansions of luni-solar gravity perturbations along rotating axes for trajectory optimization: Part 1: The dynamic system
Authors:Jean A Kéchichian
Institution:1. University of Southampton, University Road, Southampton SO17 1BJ, United Kingdom;2. Universidad Rey Juan Carlos, Camino del Molino 5, 28943 Fuenlabrada, Madrid, Spain;1. Department of Aeronautics and Astronautics, The University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo, Japan;2. School of Aeronautics and Astronautics, Purdue University, 701 West Stadium Avenue, West Lafayette, IN, USA;3. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA), 3-1-1 Yoshinodai, Chuo-ku, Sagamihara, Kanagawa, Japan;1. Arnold Engineering Development Complex, 100 Kindel Drive, Arnold AFB, TN 37389, USA;2. Arnold Engineering Development Complex, 100 Kindel Drive, Arnold AFB, TN 37389, USA;3. Arnold Engineering Development Complex, 100 Kindel Drive, Arnold AFB, TN 37389, USA;4. Jacobs Technology NASA Johnson, 2101 NASA Parkway, Houston, TX 77058, USA;5. The Aerospace Corporation, 2310 E. El Segundo Blvd, El Segundo, CA 90245, USA;6. NASA Orbital Debris Program Office, 2101 NASA Parkway, Houston, TX 77058, USA
Abstract:
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