Differential Evolution Optimization for Targeting Spacecraft Maneuver Plans | Zendy

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Differential Evolution Optimization for Targeting Spacecraft Maneuver Plans

Author(s) -

Daniel Mattern

Publication year - 2016

Publication title -

aiaa/aas astrodynamics specialist conference

Language(s) - English

Resource type - Conference proceedings

DOI - 10.2514/6.2016-5511

Subject(s) - spacecraft , differential evolution , computer science , differential (mechanical device) , aerospace engineering , control theory (sociology) , mathematical optimization , engineering , mathematics , artificial intelligence , control (management)

Previous analysis identified specific orbital parameters as being safer for conjunction avoidance for the TDRS fleet. With TDRS-9 being considered an at-risk spacecraft, a potential conjunction concern was raised should TDRS-9 fail while at a longitude of 12W. This document summarizes the analysis performed to identify if these specific orbital parameters could be targeted using the remaining drift-termination maneuvers for the relocation of TDRS-9 from 41W longitude to 12W longitude.

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