摘要
在简化条件下,讨论了闭路制导中如何确定推力方向,以达到“燃料消耗最小”条件下的准最优,并以某型导弹为例进行了仿真计算。仿真计算结果表明,所提出的方法是有效的,可以达到“燃料消耗最小”条件下的准最优。
In order to get the near-optimum control under the conditions of minimum consummation of fuel, the technique how to calculate the thrust direction under the simplified conditions was presented in this paper. Simulation results show that the technique under the conditions of minimum consummation of fuel is efficient.
出处
《飞行力学》
CSCD
北大核心
2005年第3期64-66,共3页
Flight Dynamics
关键词
闭路制导
最优控制
推力方向
closed guidance
optimal control
thrust direction
