摘要
介绍了推力矢量控制的由来和意义，着重叙述了推力矢量控制，特别是推力矢量飞机在大迎角、过失速状态下目前主要的非线性鲁棒解耦控制律的设计方法。如非线性逆动态方法、ＮＬＱＲ（非线性二次最优调节器）、自适应方法、变结构方法以及最近出现的基于人工神经元网络的方法。指出了这些方法在推力矢量控制飞机应用中各自的特色以及目前存在的问题。并指出了今后主要的工作方向。
The paper introduces the thrustvectoring ideas and its importance to modern fighter,and also investigates a few of nonlinear robust decoupling approaches for thrustvectoring controlled fighters,especially in the state of poststall and highalpha.These approaches are nonlinear inverse dynamics method,NLQR(nonlinear least quadratic regulator),adaptive control,variable structure control,and artifical neural network method respectively.The paper points out different features of these methods in the application of thrustvectoring control,and also shows the existing problems of these methods.The future work outline is given in the conclusion remarks.
出处
《飞行力学》
CSCD
北大核心
1997年第3期42-47,共6页
Flight Dynamics
