MIL-G-46858A
TABLE I - C
GYRO PARAMETERS FOR BODY MOUNTED - SHORT TIME, SEVERE ENVIRONMENT APPLICATIONS /1
Ac-
Damp- Char- Vehicle Slaving Com- Drift Random Ac-
Slaving
Sensor Switch Natural
Input
celer- celer-
acter- Induced Rate
posite Rate Drift
Error
Operat Frequency ing
Ranges Gain
Parameter
ation ation-
Rate
Acceler
istic
Ratio
-ing
Point/2
-
Insen-
-ation
Error
Sensi sitive
Time Effects
-tive
Drift
Drift
Rate
Gyro
Rate
Type
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.
17
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