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.
制导和控制一体化的设计方法充分考虑了制导和控制回路的不确定性和未建模动态。
Uncertainties and unmodelled dynamics are taking into consideration in this integrated approach to guidance and control.
制导和控制一体化的设计方法充分考虑了制导和控制回路的不确定性和未建模动态。
Uncertainties and unmodelled dynamics are taking into consideration in this integrated approach to guidance and control.
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