The primary objective of the system acceptance test is to establish that the missileborne autopilot system operates satisfactorily by acceptable authorized drawings, specifications and reports. (Author)
Xsm-65D Autopilot System Acceptance Test Plan
1959
26 pages
Report
No indication
English
Navigation, Guidance, & Control , Missile Technology , Surface to surface missiles , Automatic pilots , Flight control systems , Performance(Engineering) , Inertial guidance , Hydraulic servomechanisms , Gyro stabilizers , Calibration , Torque , Hydraulic actuators , Signal generators , Monitors , Recording systems , Reliability , Voltage , Frequency , Response , Atlas , Xsm-65d missiles
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