The Coupling Orbit–Attitude–Structure Evolution of Rubble-Pile Asteroid with Earth Flyby in the Restricted Three-Body Problem.
- Resource Type
- Article
- Source
- Aerospace (MDPI Publishing); Jul2022, Vol. 9 Issue 7, p351, 1p
- Subject
THREE-body problem ASTEROIDS DISCRETE element method TWO-body problem (Physics) LONG-Term Evolution (Telecommunications) TIDAL forces (Mechanics) - Language
- ISSN
- 22264310