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.
Differential Evolution Optimization for Targeting Spacecraft Maneuver Plans
2016
31 pages
Report
Keine Angabe
Englisch
DIFFERENTIAL EVOLUTION OPTIMIZATION FOR TARGETING SPACECRAFT MANEUVER PLANS
British Library Conference Proceedings | 2016
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