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|  MIL-G-46858A
n.
Deviations from specified test conditions (see 4.3)
o.
Deviations from specified environmental testing procedures (see 4.7)
p.
When flight tests are required (see 4.8)
q.
Applicable level of preservation, packaging and packing required
6.3 Definitions.
6.3.1 Acceleration-insensitive drift rate. - The acceleration-insensitive drift rate of a
gyroscope consists of those components of systematic drift rate that have no
correlation with acceleration.
* 6.3.2 Acceleration-sensitive drift rate. - The accleration-sensitive drift rate of
gyroscope consists of those components of systematic drift rate that are correlated with
translational acceleration applied to the gyro case.
6.3.3 Accessory unit. - A part, subassembly or assembly designed for use in
conjunction with or to supplement another assembly, or a unit or set, contributing to
the effectiveness thereof without extending or varying the basic function of the
assembly or set. An accessory unit may be used for testing, adjusting or calibrating
purposes.
6.3.4 Accuracy. - Accuracy for a missileborne sensor defines the range about the
actual value of an input parameter which the output of the sensor is likely to indicate.
6.3.5 Actuator gain. - Actuator gain is the ratio of the output force or torque of the
actuator to the level of the corresponding control signal.
* 6.3.6 Characteristic time. - Characteristic time is the time required for the output of a
device to reach 63.2 percent of its final steady state value in response to a step input.
6.3.7 Command guidance equipment types. - The command guidance systems and
equipment covered by this specification can be classified in terms of the applicable
transmission link (see 6.3.29), under the following types:
a. Radar Command - Command guidance equipment utilizing radar sets for the
reception of incoming command signals and for the transimssion of any
corresponding reply.
b. Radio Command - Command guidance equipment utilizing a radio receiver
for the reception of incoming command signals.
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