----+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8
DYNSEL 2000039 000807000037.00000808000000.00
----+----0----+----0----+----0----+----0----+----0----+----0----+----0----+----0
COLUMNS FORMAT DESCRIPTION DEFAULT VALUE & UNITS
1-6 A6 DYNSEL - Defines the times for which
GEODYN will use external accelerations
to drive the satellite. During these
any accelerometer biases or attitude
parameters become force model parameters.
18-24 I7 Satellite ID (required). 0
25-44 D20.8 Begin time for using external YYMMDDHHMMSS.SS
accelerometer data
45-59 D15.3 End time for using external YYMMDDHHMMSS.SS
accelerometer data.
IF CARD OMITTED: The satellite will be integrated as usual and there will be
no external acceleration contribution.