Sub-Optimal Missile Guidance with Impulse-Motor Control Logic
50th, Israel annual conference on aerospace sciences ; 2010 ; Tel Aviv, Israel
2010-01-01
16 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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SUB-OPTIMAL MISSILE GUIDANCE WITH PULSE-MOTOR CONTROL LOGIC USING THE SINGULAR PERTURBATIONS METHOD
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