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With respect to a kind of missile with morphing wings, six-degree-of-freedom dynamics mathematical model including morphing wing dynamic was established using momentum principle, and guidance system model was presented, at the same time the whole attitude control system for missile with morphing wings was designed based on variable structure control theory. In order to prove the correctness of the...
With respect to a kind of missile with deflectable nose, six-degree-of-freedom dynamics mathematical model including deflectable nose dynamic was established using momentum principle, and guidance system model was presented, at the same time the whole attitude control system with deflectable nose was designed based on variable structure control theory. In order to prove the correctness of the validity...
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