The innovative nature of dynamical systems theory and its applications in trajectory design enabled many recent missions by opening up new transfer and capture opportunities to meet mission requirements, reduce fuel costs, and address various launch constraints and contingencies. With a combination of proven numerical methods and an advanced understanding of the dynamics, an ‘experienced’ user can rapidly design multibody and cislunar missions such as Lunar IceCube and Artemis/Themis and relatively quickly conceive trajectory concepts for Sun-Earth mission orbits, such as the Space Weather Follow On-L1 Lissajous orbit—one that can be achieved and maintained.
Evolution of Astrodynamics for Multibody Environments, Numerical Precision and Dynamical Understanding
AAS/AIAA Astrodynamics Specialist Conference ; 2023 ; Big Sky, MT, US
Miscellaneous
No indication
English
Online Contents | 1995
Online Contents | 2012
Online Contents | 2009
Online Contents | 1994
TIBKAT | 2008
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