NASA NTRS · 20160011243
Differential Evolution Optimization for Targeting Spacecraft Maneuver Plans
Abstract
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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Mattern, Daniel. 2016-09-13. Differential Evolution Optimization for Targeting Spacecraft Maneuver Plans. https://ntrs.nasa.gov/citations/20160011243
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