The object of the memorandum was to explain why a rapid sequential, mechanically lobed, tracking and guidance system in which the spacing between pulses from separate magnetrons on different frequencies conveys to the missile the basic sense information was constructed instead of a single pulse system.
History of the Interim Guidance Radar
1947
7 pages
Report
No indication
English
Nonlinear optimal guidance algorithms Interim report
NTRS | 1969
|Minimum impulse guidance Interim scientific report
NTRS | 1968
|Optimum rendezvous guidance study Interim report
NTRS | 1968
|Nonlinear Optimal Guidance Algorithms Interim Report
NTIS | 1969
|Optimum Rendezvous Guidance Study Interim Report
NTIS | 1968
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