Precision gyroscopes, accelerometers and stabilized platforms described; guidance schemes appropriate to ballistic missiles; problem of gravity computation and effect of instrument errors; missile steering computer and rocket motor shutoff computer given for German V-2 rocket used as example; numerical values of coefficients calculated for sample trajectory.
Inertial guidance for rocket-propelled missiles
Jet Propulsion
Jet Propulsion ; 28 , n 1
1958
8 pages
Article (Journal)
English
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