Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints
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DOI: 10.1007/s11633-016-0953-y
Abstract: In order to improve the precision of guidance for the missile intercepting maneuvering targets, this paper proposes a sliding mode guidance law with impact angle constraints based on the equation of the relative motion of… read more here.
Keywords: impact angle; sliding mode; guidance law; guidance ... See more keywords