A novel set of moment wheel actuators is proposed to control a reentry warhead with indifferently static stability. 摘要提出了一种以动量轮为执行机构的具有中性静稳定气动布局的再入弹头姿态控制新方案。
Applying the optimal guidance law in this paper to a reentry warhead, this optimal control law was proved effective through computer simulation. 将此最优制导算法应用到某型再入弹头,通过计算机仿真验证了算法的正确性。