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
The AIAA/AAS Astrodynamics Specialist Conference ; 2016 ; Long Beach, CA, United States
2016-09-13
Miscellaneous
No indication
English
DIFFERENTIAL EVOLUTION OPTIMIZATION FOR TARGETING SPACECRAFT MANEUVER PLANS
British Library Conference Proceedings | 2016
|