Time Shift Governor for Constrained Control of Spacecraft Orbit and Attitude Relative Motion in Bicircular Restricted Four-Body Problem
Author:
Affiliation:
1. University of Michigan,Department of Aerospace Engineering,Ann Arbor,MI,USA,48109
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10644130/10644150/10644260.pdf?arnumber=10644260
Reference17 articles.
1. Targeting cislunar near rectilinear halo orbits for human space exploration;Williams;AAS/AIAA Space Flight Mechanics Meeting,2017
2. Stationkeeping analysis for spacecraft in lunar near rectilinear halo orbits;Guzzetti,2017
3. Coupled position and attitude control of a servicer spacecraft in rendezvous with an orbiting target
4. Rendezvous in Cis-Lunar Space near Rectilinear Halo Orbit: Dynamics and Control Issues
5. Preliminary results on the dynamics of large and flexible space structures in Halo orbits
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