摘要
从分析人类神经控制系统的特点出发,采用类比的方法,根据分层递阶的思想,提出一种我国下一代战斗机的飞行控制平台结构。该递阶结构分为三层,即决策层、组织协调层和执行层。并根据各个机载任务的地位和使用资源的不同将其分别归属到这三个不同的层次中。最后,根据目前的软/硬件水平,提出了一个与此递阶结构相适应的物理布局方案。
Based on the human intelligent control system, a three-leveled hierarchical control architecture is proposed. At the top of the architecture, a decision-making level is in charge of decision-making works. In the middle, an organization ＆ coordination level will schedule resources, monitor the states of the fighter and switch the control modes, etc. And the bottom is an execution level which holds the concrete drive and measurement; then, according to their function and resources all the tasks involving flight control and mission management are sorted to individual level; at last, in order to validate the three-leveled architecture, a physical configuration is also showed.
出处
《飞行力学》
CSCD
北大核心
2007年第1期43-46,共4页
Flight Dynamics
关键词
飞行控制系统
递阶
决策层
组织协调层
执行层
flight control system
hierachical
decision-making level
organization ＆ coordination level
execution level
