Aeroservoelastic modelling and control of a slender anti-air missile for active damping of longitudinal bending vibrations
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DOI: 10.1016/j.ast.2017.03.001
Abstract: Abstract Slender anti-air missiles experience longitudinal bending in supersonic flight and yet their autopilots are designed under the rigid-body assumption. Such autopilot design employs notch filters to remove the modal frequencies of the elastic airframe… read more here.
Keywords: anti air; control; slender anti; longitudinal bending ... See more keywords