Efficient parallelization of nonlinear perturbation algorithms for orbit prediction with applications to asteroid deflection and fragmentation

Advances in the Astronautical Sciences

Volumn 136, Issue , 2010, Pages 1845-1860

  Kaplinger, Brian D ^a   Wie, Bong ^a   Dearborn, David ^b  

^a IOWA STATE UNIVERSITY   (United States)

^b LAWRENCE LIVERMORE NATIONAL LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASTEROID DEFLECTION; COMPUTATIONAL ALGORITHM; COMPUTER RESOURCES; CONTROL PROBLEMS; EFFICIENT ALGORITHM; HYDRODYNAMIC SIMULATION; INITIAL CONDITIONS; LINEARIZED METHODS; NONLINEAR EFFECT; NONLINEAR PERTURBATIONS; NUMERICAL INTEGRATOR; ORBIT DETERMINATION; ORBIT PREDICTION; PARALLELIZATIONS; RELATIVE EFFICIENCY; RELATIVE MOTION EQUATIONS;

ALGORITHMS; ASTEROIDS; EQUATIONS OF MOTION; EXPLOSIVES; MECHANICS; NUCLEAR EXPLOSIONS; SPACE FLIGHT;

NONLINEAR EQUATIONS;

EID: 80053392641     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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