Local Eigenmotion Control for Near Rectilinear Halo Orbits-Reference-Cited by-同舟云学术

Local Eigenmotion Control for Near Rectilinear Halo Orbits

Published:2022-06-08 Issue: Volume: Page:
ISSN:
Container-title:2022 American Control Conference (ACC)
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Author:

Elango Purnanand¹,Di Cairano Stefano²,Kalabic Uros²,Weiss Avishai²

Affiliation:

1. University of Washington,William E. Boeing Department of Aeronautics and Astronautics,Seattle,WA,98195

2. Mitsubishi Electric´ Research Laboratories (MERL),Cambridge,MA,USA,02139

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9866948/9867142/09867672.pdf?arnumber=9867672

Reference26 articles.

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2. Stationkeeping monte carlo simulation for the James Webb Space Telescope;dichmann;Proceedings 24th International Symposium on Space Flight Dynamics–24 th ISSFD,2014

3. Incorporation of mission design constraints in Floquet mode and Hamiltonian structure-preserving orbital maintenance strategies for libration point orbits;tajdaran;Ph D Dissertation,2015

4. Station keeping of a quasiperiodic halo orbit using invariant manifolds;gómez;Proceed 2nd Internat Symp on spacecraft flight dynamics Darmstadt,1986

5. Control Strategies for Formation Flight In the Vicinity of the Libration Points

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