The Restricted Hill Full 4-Body problem: Application to spacecraft motion about binary asteroids

Dynamical Systems

Volumn 20, Issue 1, 2005, Pages 23-44

  Scheeres, D J ^a   Bellerose, J ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

LAGRANGE MULTIPLIERS; MATHEMATICAL MODELS; ORBITS; PERTURBATION TECHNIQUES; PROBLEM SOLVING; SPACE FLIGHT; SPACECRAFT;

MASS DISTRIBUTIONS; MASSLESS PARTICLES; NEAR-EARTH ASTEROIDS (NEA); ORBITAL MOTION;

ASTRONOMY;

EID: 12344317305     PISSN: 14689367     EISSN: None     Source Type: Journal    
DOI: 10.1080/1468936042000281321     Document Type: Review

References (20)

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