New Principle for Missile Guidance and Control
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چکیده
ted to allow efficient ballistic missiles , the paper describes a recently developed ted estimation/guidance design paradigm n several innovative concepts that provides satisfactory homing performance against ly maneuvering targets. The new paradigm veloped and tested first by using a simplified constant speed interception scenario model. paper the integrated estimation/guidance m is validated by simulations of generic tmospheric theatre ballistic missile defense ption scenarios against two types of stressing target maneuvers.
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