摘要
提出了具有三个剖面的导弹协同作战四维制导控制构架。以BTT控制形式的导弹为例进行了四维制导控制方法研究。在分析总能量控制理论的基础上,设计了适于具有过载自动驾驶仪内回路的BTT导弹的速度/高度解耦控制器,实现了四维制导构架中速度和高度剖面的解耦,最后进行了仿真验证。仿真结果表明,四维制导控制器能够根据任务规划系统的指令控制导弹实现协同作战。
This paper proposed a control framework of four-dimensional guidance for the cooperative engagement of missile with three profiles. Taking a missile with BTT control mode as an example, research on the control method of four-dimensional guidance was conducted. The velocity/altitude decoupling controller suitable for the BTT missile with overload autopilot inner-loop was designed based on total energy control theory analysis, which implemented the decoupling for velocity and altitude profiles in four-dimensional guidance control framework. In the end, simulation verification was performed to show that the four-dimensional guidance controller is able to implement the cooperative engagement by controlling a missile according to instructions of the task planning system.
出处
《飞行力学》
CSCD
北大核心
2010年第2期63-66,共4页
Flight Dynamics
基金
航天科技创新基金资助(CASC0209)
关键词
四维制导
协同作战
总能量控制
解耦
内回路
four-dimensional guidance
cooperative engagement
total energy control
decoupling
inner-loop
