Multi-Satellite Formation Trajectory Design with Topological Constraints over a Region of Interest using Differential Evolution

Multi-Satellite Formation Trajectory Design with Topological Constraints over a Region of Interest using Differential Evolution

Satellite formation missions allow for scientific measurement opportunities that are only otherwise possible with the use of unrealistically large satellites. This work applies the Evolutionary Algorithm (EA), Differential Evolution (DE), to a 4-satellite mission design that borrows heavily from the...

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Bibliographic Details
Main Author: Hinckley, David William
Format: Others
Language:en
Published: ScholarWorks @ UVM 2015
Subjects:
Differential Evolution
Evolutionary Algorithms
Formation
Trajectory
Aerospace Engineering
Computer Sciences
Mechanical Engineering
Online Access:http://scholarworks.uvm.edu/graddis/404
http://scholarworks.uvm.edu/cgi/viewcontent.cgi?article=1403&context=graddis

Internet

http://scholarworks.uvm.edu/graddis/404
http://scholarworks.uvm.edu/cgi/viewcontent.cgi?article=1403&context=graddis

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