Features of command type radioinertial guidance system in which ground-based radar continuously determines position of missile during powered flight and digital computer accepts data; this is done by reference to previously stored trajectory information for particular target, computing appropriate orders to maintain missile on proper flight path; corrective orders are transmitted by radio to missile and applied to missile's autopilot and control system.
Missile guidance
Bell Laboratories Rec
Bell Laboratories Record ; 37 , n 6
1959
5 pages
Aufsatz (Zeitschrift)
Englisch
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