Flight Dynamics Functions
ï Propagation of DSN-derived orbit for science planning
purposes. Predicted orbit will be forwarded to SwRI and
to NSSDC/Satellite Situation Center.
ï Predicted orbit will be used for long-range DSN scheduling
and uplinked to the spacecraft.
Mission Unique Developments:
ï Calculation of Mass-Balancer adjustments via Matlab
ï RPI antenna deployment calculations done via Matlab