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Attitude Control and Perturbation Analysis of a Crewed Spacecraft with a Lunar Lander in Near Rectilinear Halo Orbit
By: Clark P. Newman, Jacob R. Hollister, Frederick S. Miguel, Diane C. Davis and Daniel J. Sweeney.
Pub. 2020,
12pgs.
PDF File.
AAS 20-046.
Price: $29.00
Reprinted from Advances in the Astronautical Sciences AAS Guidance, Navigation, and Control 2020, Volume 172
This item is an
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