Partial contents: Tactical Operational Requirements--the unmanned aircraft as a force multiplier, Navy technology requirements for unmanned airborne vehicles; and Design/development tradeoffs to achieve a mission effective SOW(Standoff Weapon) Guidance System; Weapon Systems Concepts, Design Criteria and Integration Issues--Lethal air defense suppression technology base definition; and Midcourse guidance for the US Army's low cost fiber optic guided missile; Tactical Mission Planning and Management; Probabilities de collision de missiles de croisiere volante formation; Strapdown Inertial Systems Applications for Tactical Missiles (Stand-Off Missiles); Computational Techniques and Data Processing; Precision delivery of unguided submunitions from a tactical standoff missile; and High Altitude, long endurance RPV design technology study.
Guidance, Control and Positioning of Future Precision Guided Stand-off Weapons Systems
1986
164 pages
Report
No indication
English
Missile Guidance & Control Systems , Guidance , Guided weapons , Standoff , Symposia , Precision , Weapon delivery , Guided missiles , Midcourse guidance , Fiber optics , Navigation , Strapped down systems , Remotely piloted vehicles , Submunitions , Microcomputers , Control systems , Data processing , Position(Location) , Mission profiles , High altitude , Trade off analysis , Military requirements , Tactical air support , Air defense , Suppression , Foreign technology , Standoff weapons , Defense suppression , Precision guidance , Standoff missiles , NATO furnished
Guidance and control of precision guided weapons : Papers
TIBKAT | 1988
|Tema Archive | 1975
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