指挥控制与仿真2012，Vol.34Issue(4)：55-60,6.DOI:10.3969/j.issn.1673-3819.2012.04.011
飞机结冰时不变参数识别技术
Time Invariant Parameter Identification of Inflight Aircraft Icing
摘要
Abstract
Aircraft icing is one of the flight accidents usually. As issue has been paid more attention, the aircraft icing research is facing the direction of intelligent identification and control integrated. Then the first problem to be solved is aircraft icing parameter detection technology. The paper introduces the six degrees of freedom of aircraft simulation model and ice parameter model. Then an aircraft icing parameter identification method is introduced, which is based on H-infinity, and also verify its feasibility by simulation results. This method is not subject to the influence of external disturbances.关键词
飞机结冰/结冰检测/参数识别Key words
aircraft icing/ icing detection/ parameter identification分类
航空航天引用本文复制引用
应思斌,葛彤,艾剑良..飞机结冰时不变参数识别技术[J].指挥控制与仿真,2012,34(4):55-60,6.基金项目
中国博士后基金(20100480588) （20100480588）
