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|  MIL-G-46858A
3.5.4.7.3 Altitude Sensors. - When the flight control subsystem employs altitude sensors for
measuring indicated or true missile altitude, these sensors shall comply with the design values
and tolerances of the related parameters established in the detailed specification. These
parameters shall include but not be limited to the following:
a. Input range
b. Sensor gain
c. Characteristic time
d. Accuracy
e. Drift rate
* 3.5.4.7.4 Gyroscopes. - When the flight control subsystem employs free, rate, vertical,
directional, or rate integrating gyroscopes for measuring angular displacements or angular
rates of the missile airframe or of any servo stabilized equipment, these gyroscopes shall
comply with requirements of MIL-G-46857 deemed applicable by the procuring activity.
Further compliance is required with regard to the design values and tolerances of the
applicable parameters listed in Table I and established in the detailed specification.
3.5.4.7.5 Platforms. - When the flight control subsystem employs stabilized platforms for
measuring angular displacements of the missile airframe or to provide a stable reference plane
for any guidance and control equipment, the characteristics of such platforms shall conform to
the requirements of the detail specification.
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