In this paper, the missile guidance with terminal impact Angle constraint and integrated guidance and control design for missile with terminal impact constraint were researched.
在这一背景下，本文研究了带末端攻击角度约束的制导方法设计和制导控制一体化方法设计问题。
In this paper, the missile guidance with terminal impact Angle constraint and integrated guidance and control design for missile with terminal impact constraint were researched.
在这一背景下，本文研究了带末端攻击角度约束的制导方法设计和制导控制一体化方法设计问题。
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