Regularized equations of motion can improve numerical integration
for the propagation of orbits, and simplify the treatment of
mission design problems. This monograph discusses standard
techniques and recent research in the area. While each scheme is
derived analytically, its accuracy is investigated numerically.
Algebraic and topological aspects of the formulations are studied,
as well as their application to practical scenarios such as
spacecraft relative motion and new low-thrust trajectories.
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