Analytical approach presented is applicable to optimization of systems operating in presence of radar noise; factors considered are target evasive maneuver, radar glint noise, missile maneuverability, and inherent time varying character of kinematics; method of finding approximate solutions utilizing time varying control systems.
Synthesis of optimum homing missile guidance systems with statistical inputs
NASA Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 2-13-59A
1959
57 pages
Report
Englisch
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Optically aided homing missile guidance
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|Final-value homing missile guidance.
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Engineering Index Backfile | 1958