The role of invariant manifolds in low thrust trajectory design (Part II)

Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference

Volumn 3, Issue , 2004, Pages 1348-1368

  Anderson, Rodney L ^a,c   Lo, Martin W ^b,d  

^a UCB 450   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^c Aerospace Engineering Sciences   (United States)

^d Navigation and Mission Design   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

GRAVITATION; MATHEMATICAL MODELS; MOON; OPTIMIZATION; ORBITS; PROBLEM SOLVING; RESONANCE; SATELLITES; SPACE FLIGHT; VELOCITY MEASUREMENT;

EURAOPA ORBIT INSERTION (EOI); GRAVITY FLYBYS; INVARIANT MANIFOLDS; PLANAR CIRCULAR RESTRICTED THREE-BODY PROBLEM (PCRTBP); TRAJECTORY DESIGN;

TRAJECTORIES;

EID: 19644366798     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5305     Document Type: Conference Paper

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