AUG 1998
9808.0
ARC SET
----+----1----+----2----+----3----+----4----+----5----+----6----+----7----+----8
THRDRG 7603901
----+----0----+----0----+----0----+----0----+----0----+----0----+----0----+----0
COLUMNS FORMAT DESCRIPTION DEFAULT VALUE & UNITS
1-6 A6 THRDRG - Requests thermal drag
application.
7 Card number indicator (1 or 2). 1
The second card is used to request
adjustment of the satellite spin
axis.
8 I1 > 0 Indicates that partials are 0
to be calculated but the thermal
drag force will not be applied.
18-24 I7 Satellite ID (Required) 0
25-44 D20.8 Scaling parameter D -11.836**-12 MS**-2
(see model below)
45-59 D15.3 Model variable parameter
1.2
(see model description below) unitless
60-72 D13.1 Colatitude of the satellite's 22 DEG
spin axis
If there is a 2 in column 7
(if this is the second THRDRG
card), then this field is for
the standard deviation of the
a priori spin axis colatitude.
The default standard deviation
is zero.
73-80 D8.2 The right ascension of the 313 DEG
satellite's spin axis
If there is a 2 in column 7 (if
this is the second THRDRG card),
then this field is for the
standard deviation of the a priori
spin axis right ascencion. The
default standard deviation is zero.
Note [1]: The option to adjust the spin axis will not work in a run with
more than one satellite or more than one arc.
Note [2]: The thermal drag acceleration is computed from the equation
(for detailed description see section 8.12, Vol. 1) :
UNITS: KM =Kilometers; M =Meters ; S =Seconds ; M/S=Meters per second
DEG=Degrees ; RAD=Radians ; AS =Arc seconds; MAS=Milli-arc seconds
IF CARD OMITTED : Thermal drag acceleration will not be included.