Trajectory Design Employing Convex Optimization for Landing on Irregularly Shaped Asteroids
Author(s) -
Robin Pinson,
Ping Lu
Publication year - 2018
Publication title -
journal of guidance control and dynamics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 1.573
H-Index - 143
eISSN - 1533-3884
pISSN - 0731-5090
DOI - 10.2514/1.g003045
Subject(s) - asteroid , descent (aeronautics) , propellant , trajectory , spacecraft , trajectory optimization , computer science , thrust , convex optimization , optimization problem , rocket (weapon) , regular polygon , control theory (sociology) , mathematical optimization , optimal control , aerospace engineering , mathematics , physics , algorithm , engineering , geometry , artificial intelligence , control (management) , astronomy
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