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Global Optimization of N-Maneuver, High-Thrust Trajectories Using Direct Multiple ShootingThe performance of impulsive, gravity-assist trajectories often improves with the inclusion of one or more maneuvers between flybys. However, grid-based scans over the entire design space can become computationally intractable for even one deep-space maneuver, and few global search routines are capable of an arbitrary number of maneuvers. To address this difficulty a trajectory transcription allowing for any number of maneuvers is developed within a multi-objective, global optimization framework for constrained, multiple gravity-assist trajectories. The formulation exploits a robust shooting scheme and analytic derivatives for computational efficiency. The approach is applied to several complex, interplanetary problems, achieving notable performance without a user-supplied initial guess.
Document ID
20160001644
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Vavrina, Matthew A.
(AI Solutions, Inc. Lanham, MD, United States)
Englander, Jacob A.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Ellison, Donald H.
(Illinois Univ. Urbana-Champaign, IL, United States)
Date Acquired
February 5, 2016
Publication Date
February 14, 2016
Subject Category
Astrodynamics
Report/Patent Number
AAS 16-272
GSFC-E-DAA-TN29107
Report Number: AAS 16-272
Report Number: GSFC-E-DAA-TN29107
Meeting Information
Meeting: AAS/AIAA Spaceflight Mechanics Meeting
Location: Napa, CA
Country: United States
Start Date: February 14, 2016
End Date: February 18, 2016
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNG14VC09C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
optimization
trajectory design
gravity assist
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