摘要
针对歼击机自修复控制系统的综合仿真，推导了具有较大稳定域的自适应ＲＫ公式，研制了歼击机自修复控制系统一体化仿真环境，该环境支持歼击机动力学方程的线性化、故障诊断、自修复控制律设计等众多仿真实验任务。在此基础上，应用一种模型参考自修复方法对某型歼击机进行了仿真研究。
A new adaptive algorithm which has a wider stability region was derived and the siumulation environment which is used for the fighter self repaired control systems simulation was designed. This environment can support various simulation experiments which include linearization method, failure diagnosis and reconstruction control law design. A model reference self repairing control method was used to carry out the simulation of fighter self repaired control systems
出处
《航空学报》
EI
CAS
CSCD
北大核心
1999年第2期122-126,共5页
Acta Aeronautica et Astronautica Sinica
基金
博士后基金
航空基金
