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Page Title:
Table 1- D. Gyro Parameters for Body Mounted |
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|  MIL-G-46858A
TABLE I - D
GYRO PARAMETERS FOR BODY MOUNTED - LONG TIME, MILD 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
Ratio
-ing
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
T
X
N
X
S
S
Rate Gyro X
X
X
X
X
Rate
X
T
X
X
S
S
Integrating
Gyro
Vertical
X
X
X
X
X
X
Gyro
NOTES:
N - Parameter specified when no torquer is used; 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 greater than 15
minutes and accelerations less than 3 g's.
/2 - Parameter applicable for gyro switches only.
18
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