Frequent GEODYN Problems --------------------------- 1) Light Time Problems in Interplanetary Runs: 1a) RANGE AND/OR DOPPLER OBSERVATIONS NEAR THE INITIAL EPOCH: It is important to remember that DSN Doppler and range measurements are time tagged at the epoch when the signal is received at the tracking station. When any measurement is processed, the epoch(s) at which the signal are at the satellite must be modeled using satellite positions and/or velocities. The satellite epoch will be a light time earlier than the DSN Doppler or range time tag. The satellite positions and velocities are computed by numerical integration and are only available epochs after the initial epoch specified on the EPOCH card. Range and doppler observations that are within a light time of the initial epoch should be deleted. 1b) MIXING RANGE AND/OR DOPPLER OBSERVATIONS WITH ALTIMETRY OR CAMERA DATA IN INTERPLANETARY RUNS: To avoid problems limit the maximum number of observations in a block (columns 11-14 of the VECOPT card) and maximize the numerical integrator's window of interpolation (columns 15-17 of the VECOPT card). The detailed explanation follows: GEODYN (TDF and IIS) will order observations in order of their nominal time tag. It is important to remember that range and Doppler observations are time tagged at the epoch that the tracking station receives the signal while camera and altimeter ranges are time tagged at satellite time. As a result, range and Doppler can have large light time issues while altimeter and camera observations do not. When Doppler and range observations are mixed with satellite time tagged observations in interplanetary runs, light time issues force GEODYN to model satellite epochs out of chronological order. The problem is compounded by the fact that GEODYN TDF & IIS group observations into blocks. GEODYN will not integrate backwards to accommodate satellite times that are not in chronological order. Even so, problems can be avoided by using settings on the VECOPT card. GEODYN can successfully process satellite epochs that are not in chronological order, but only if the window of interpolation associated with the integrator is large enough to span events that are out of order. The window (time interval) of interpolation is the number of back values carried by the integrator (columns 15-17 of the VECOPT card) multiplied by the integration step size. The worst case of out of order observations will occur if a block of Doppler observations follows a large block of altimeter or camera observations. First the integrator will have been advanced to the time tag of the final altimeter or camera observation in the block. After the altimeter or camera observation have been processed, the block of Doppler observations will be processed. The earliest satellite event will be for the first Doppler observation in the block at the beginning of the counting interval. This will occur at a time earlier than the observation time tag by the counting interval plus the light time. This earliest satellite event time for the Doppler is likely to be significantly earlier than the time tag of the final altimeter of camera observation of the previous block. This interval can be particularly long because GEODYN TDF and IIS tend to group long passes of altimeter observations together into large blocks. The problem can be mitigated by using the minimum value (11) of the maximum number of observations in a block (columns 11-14 of the VECOPT card). In addition to limiting the number of observations in a block, the window of interpolation should be maximized (columns 15-17 of the VECOPT card) to cover the light time plus some extra.