| Document Date: 2011-06-05 16:48:18
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Company Payload Systems Inc. / Microsoft / / / Facility GLPK library / TPF observatory / Microsoft Visual Studio / / IndustryTerm stage algorithm / well developed algorithms / online / feasible initial solution / transition algorithm / energy consumption / aerospace applications / path planning algorithm / feasible solution / randomized motion planning algorithms / approximate solution / formation flying technology / final solution / energy energy leads / level mission management / monolithic satellite / eventual online implementation / path planning algorithms / search algorithm / control law / energy / / Organization MIT / National Aeronautics and Space Administration / / Person Georges S. Aoude / Jonathan P. How / J. P. How / / Position RRT-GPM planner / Professor / bidirectional RRT planner / RRT-GPM path planner / planner / / Product Pentax K-x Digital Camera / / ProgrammingLanguage MATLAB / C++ / / PublishedMedium la Nature / la Recherche / / Technology formation flying technology / two-stage algorithm / radiation / two-stage planning algorithm / transition algorithm / return Failure In Algorithm / Laser / WAP / RAM / RRT-GPM algorithm / X-ray / 3-D / path planning algorithms / search algorithm / randomized motion planning algorithms / planning algorithm / 2.2 GHz processor / planning algorithms / Space Communications / dom / well developed algorithms / two-stage path planning algorithm / RRT algorithm / path planning algorithm / nonlinear optimization problem Algorithm / stage algorithm / /
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Two-Stage Path Planning Approach for Designing Multiple Spacecraft Reconfiguration Maneuvers Georges S. Aoude, Jonathan P. How and Ian M. Garcia Abstract— The paper presents a two-stage approach for designing optimal r