TWO-STATE DYNAMIC GAIN SCHEDULING CONTROL APPLIED TO F16 AIRCRAFT MODEL

来源 :The Third International Conference on Dynamics,Vibration and | 被引量 : 0次 | 上传用户:newAya
下载到本地 , 更方便阅读
声明 : 本文档内容版权归属内容提供方 , 如果您对本文有版权争议 , 可与客服联系进行内容授权或下架
论文部分内容阅读
  Gain scheduling (GS) controllers follow the process of subdividing a nonlinear control problem into a series of linear ones, the design of controllers to suit each linear design condition and then reconstruction of the resultant set of gains into a single continuous controller1.Survey papers [2, 3] outline the substantial work in GS research, which has proved to be a popular approach for nonlinear control in a variety of application areas especially flight control.
其他文献
This paper presents evaluation procedures, concepts, and results from a limited test to evaluate the ability of the Open-Loop Onset Point (OLOP) criterion to predict Pilot-Induced-Oscillations (PIO) i
Numerical bifurcation analysis using continuation methods has emerged as a valuable component in the analysis of mathematical models described by differential equations.The application of bifurcation
There is a significant interest in developing flight control laws which need minimum gain scheduling across the whole flight envelope while providing required robust performance and stability properti
The stability of a helicopter rotor blade is a complex problem, involving aerodynamic, structural.material and geometric nonlinearities.Different mathematical techniques have been used in the past to
Micro aerial vehicles (MAVs) have drawn a great deal of interest in the past decade due to the advances in micro technology.Most research groups working on MAVs today based their designs on fixed, rot
In the past few ten years so m any kinds of "vertical takeoffand land (VTOL) " aircraft came out.With new configuration, they have the advantages of both helicopters and airplanes.The flight envelope
The idea of using space tethers for tethered satellite formations has received a great deal of attention in recent years with some existing research on concepts and applications [1].The advantage of u
A turbo disk can be regarded as a periodic system if all of the blades are assembled periodically.In some turbo disks, like steam turbines, the blades are assembled into periodic groups of blades and
The nonlinearity of the controller is becoming a matter of concern for more and more researchers in the engineering field [1].In this paper, the bifurcation analysis method is used to evaluate the eff
Flight control system design for large, fly-by-wire aircraft is aimed at providing optimal handling qualities for all mission tasks that the aircraft has to fulfill.Pilot-Induced Oscillations (PIO) ar