Analysis is made of command errors and performance degradation resulting from tracker errors and angles of attack in two types of systems employing roll autopilot control equation; it is shown that much smaller command errors are expected to occur in system in which roll autopilot keeps time integral of roll rate equal to zero.
Missile orientation errors in command guidance systems
ARS -- J
ARS Journal ; 30 , n 1
1960
5 pages
Article (Journal)
English
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