This note presents preliminary analysis results for terminal homing guidance against a stationary ground target. The nominal descent trajectory is vertical. Items examined are proportional navigation constant variations, pull-in capability, heading variations, blind range guidance, and a modified form of proportional navigation guidance. The digital simulation program used in the study is documented. (Author)
Surface Target Terminal Homing Guidance
1969
61 pages
Report
No indication
English
Missile Technology , Radiofrequency Detection , Computer Hardware , Surface to surface missiles , Descent trajectories , Terminal guidance , Impact prediction , Computer programs , Pursuit courses , Proportional navigation , Detectors , Radar homing , Radio homing , Infrared equipment , Optical equipment , Flow charting , Mathematical models , Acceleration , Circular error probable , Drag , Computer programming , Computer analysis , Computerized simulation
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