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OCR
Secured to fuselage
1 - GYROSCOPE
7
2 - AZIMUTH CONTROL AIR JET
3 - COMPASS
4 - ELECTRO - PHNEUMATIC DIAPHRAGM SWITCH
5 - AZIMUTH ELECTROMAGNET
6 - AZIMUTH SERVO MOTOR
7 - AZIMUTH RATE GYRO
2
8 - PITCH RATE GYRO
9 - PITCH CONTROL AIR JET
10 - PITCH SERVO MOTOR
0
<<<<<<<<
11 - BAROMETRIC ALTITUDE CONTROL
Direction of flight
12 - ELEVATOR
13 - RUDDER
11
Gyro Housing 5
Extension
9
Gyro
housing
13
8
1
3
6
10
4
Battery
12
Fig. 2-7. Schematic diagram of the control system of the FZG-76 (V-1,
(Wright Field photo).
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Context sent to Scholar
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Page context
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"ocrText": "Secured to fuselage\n1 - GYROSCOPE\n7\n2 - AZIMUTH CONTROL AIR JET\n3 - COMPASS\n4 - ELECTRO - PHNEUMATIC DIAPHRAGM SWITCH\n5 - AZIMUTH ELECTROMAGNET\n6 - AZIMUTH SERVO MOTOR\n7 - AZIMUTH RATE GYRO\n2\n8 - PITCH RATE GYRO\n9 - PITCH CONTROL AIR JET\n10 - PITCH SERVO MOTOR\n0\n<<<<<<<<\n11 - BAROMETRIC ALTITUDE CONTROL\nDirection of flight\n12 - ELEVATOR\n13 - RUDDER\n11\nGyro Housing 5\nExtension\n9\nGyro\nhousing\n13\n8\n1\n3\n6\n10\n4\nBattery\n12\nFig. 2-7. Schematic diagram of the control system of the FZG-76 (V-1,\n(Wright Field photo)."
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