摘要
航空发动机模型参数随外界条件变化很大，在整个飞行包线实现最优控制具有一定的难度。根据预测控制在线寻优的特点将其应用于航空发动机控制，并考虑到发动机的安全限制继而构造了带不等式约束的预测控制器。
<Absract> As aero-engine model parameters change greatly with external conditions, it is difficult to realize the optimum control of the aero-engine within the flight envelope. This paper applies the predictive control which can be used to search for the optimum on line to aero-engine conteos and, taking the aero-engine's safety limits into consideration, designs the predictive controller with inequality restrain.
出处
《中国民航学院学报》
1998年第4期1-4,共4页
Journal of Civil Aviation University of China
关键词
预测控制
不等式约束
航空发动机
控制
predictive control
, inequality restraint
aero-engine control
