Hit-to-kill guidance algorithm for the interception of ballistic missiles during the boost phase
A near-optimal guidance law has been developed using the direct method of calculus of variations that maximizes the kinetic energy transfer from a surface-launched missile upon interception to a ballistic missile target during the boost phase of flight. Mathematical models of a North Korean Taep...
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Monterey California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/2829 |