基于前视突风探测信息的飞机载荷减缓控制  

Load Alleviation for an Aircraft Based on Forward Looking Gust Information

作　　者：胡志明[1] 赵永辉[1] 

机构地区：[1]南京航空航天大学机械结构力学及控制国家重点实验室,江苏南京210016

出　　处：《航空计算技术》2015年第4期33-37,共5页Aeronautical Computing Technique

基　　金：国家自然科学基金项目资助(11472128);机械结构力学及控制国家重点实验室(南京航空航天大学)自主研究课题资助(0114G01)

摘　　要：突风载荷减缓是改善飞机飞行性能的一项关键技术。基于紊流探测器获得的飞机前方突风速度信息,以翼根剪力、弯矩和翼尖加速度响应为减缓指标,建立了计入控制面偏转角度和偏转速率约束的突风载荷模型预测控制方法,设计了模型预测控制器,进行了闭环系统仿真,并与参考(PID)控制作了对比。仿真结果表明,模型预测控制能够有效抑制突风载荷。Gust load alleviation is an important technique for improving the flight qualities of aircratts. It xs assumed that the preview information on the incoming gust shape in front of the aircraft can be obtained from a Light Detecting And Ranging gust sensor. In order to alleviate the wing root shearing force, bending moment as well as the acceleration response at wing tip, a model predictive controller with control surface deflection angle and deflection rate constraints is designed. The simulation results for the closed loop system are compared with those obtained by the reference controller（PID）. It has been shown that the controller with MPC law can suppress the gust loads effectively.

关 键 词：阵风载荷减缓 前视突风信息 模型预测控制 

分 类 号：V211[航空宇航科学与技术—航空宇航推进理论与工程]