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| MIL-G-46858A
TABLE I - C
GYRO PARAMETERS FOR BODY MOUNTED - SHORT TIME, SEVERE ENVIRONMENT APPLICATIONS /1
Input
Sensor Switch Natural
Damp- Char- Vehicle Slaving Com- Drift Random Ac-
Ac-
Slaving
Parameter
Ranges Gain
Operat Frequency ing
acter- Induced Rate
posite Rate Drift
celer- celer-
Error
-ing
Ratio
istic
Acceler
Rate
ation ation-
Point/2
-ation
Error
-
Insen-
Time Effects
Sensi sitive
-tive
Drift
Drift
Gyro
Rate
Type
Rate
Directional
X
X
X
X
X
X
Gyro
Free Gyro
X
X
X
X
S
S
Rate Gyro X
X
X
X
X
X
Rate
X
T
X
X
X
S
S
Integrating
Gyro
Vertical
X
X
X
X
X
X
Gyro
NOTES:
S - Parameter stability specified in addition to its absolute value; T - Where applicable, torquer linearity also specified; X - Parameter
specified
/1 - Defined as gyros affixed to missile airframe during high performance flight environments, i.e., times generally less than 15 minutes
and accelerations greater than 3 g's.
/2 - Parameter applicable for gyro switches only.
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