Development of the German A-4 guidance and control system, 1939 - 1945: A memoir
Abstract
The development by 1943 of a fully inertial navigational system for the German A-4 (V-2) missile is detailed. This flight control system used a triple-axis stabilized platform with two longitudinal accelerometers and one lateral accelerometer.
- Publication:
-
Essays on the History of Rocketry and Astronautics, Vol. 2
- Pub Date:
- September 1977
- Bibcode:
- 1977ehra....2..203S
- Keywords:
-
- Histories;
- Missile Control;
- West Germany;
- Inertial Guidance;
- Inertial Navigation;
- Inertial Platforms;
- Launch Vehicles and Space Vehicles