摘要
在简要分析了舰载直升飞机着舰过程主要特点的基础上,针对着舰过程中的飞行控制问题,提出了基于LQG/LTR方法的控制系统设计。该方法设计的控制系统具有良好的鲁棒性,仿真结果显示了LQG/LTR方法的优越性。
Based on the key characteristics of approaching and landing process, a LQG/LTR control system is designed for the flight control problems. Mathematical simulations have been made and the simulation results have shown strong robustness and good property of LQG/LTR methods.
出处
《科技通报》
北大核心
2011年第5期792-795,共4页
Bulletin of Science and Technology