Missile terminal guidance and control against evasive targets
Terminal guidance of the missile against an evasive target is explored. The two main types of guidance laws employed in the majority of missiles, namely proportional navigation and command to line-of-sight are modeled using Matlab(registered) Simulink(Trademark). The two-dimensioned missile-target i...
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| Language: | en_US |
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://handle.dtic.mil/100.2/ADA378653 http://hdl.handle.net/10945/9385 |