Analysis of the attitude dynamics of a spacecraft on a stationary orbit around an asteroid via Poincaré section

Author:

Wang YueORCID,Xu Shijie

Funder

Graduate Innovation Practice Foundation of BUAA

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference21 articles.

1. Space missions to small bodies: asteroids and cometary nuclei;Barucci;Astron. Astrophys. Rev.,2011

2. Invariant manifolds, Lagrangian trajectories and space mission design;Belló,2010

3. On the use of Poincaré surfaces of section in rigid-body motion;Broucke;J. Astronaut. Sci.,1993

4. Numerical integration of periodic orbits in the main problem of artificial satellite theory;Broucke;Celest. Mech. Dyn. Astron.,1994

5. Analysis of gravity-gradient-perturbed rotational dynamics at the collinear Lagrange points;Brucker;J. Astronaut. Sci.,2007

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