摘要
本文对飞行器模拟加热装置进行了模型辨识和自适应控制,模型辨识使用ARMAX(n)辨识器,辨识结果和机理分析一致,自适应控制采用STCCAMAC两种算法,控制结果满足性能指标要求。
In this paper, the modek identification and adaptive control of artificial heating facility of aircraft have completed. The ARMAX(n) model identification method has used. The identifi- cation results are exactly the same as the theoretical model. The STC and CAMAC control algo- rithm has used in adaptive control. The control effects satisfy all the regurments of contral system.
关键词
飞行器
模拟加热装置
模型辨识
artificial heating facility of aircraft
algorithm
identification
adaptive control
