• 不 限
  • 期刊论文
  • 硕博论文
  • 会议论文
  • 报 纸
  • 英文论文
  2. 您的位置
  3. 首页
  4. 会议论文
  5. A NEW ASYMPTOTIC PERTURBAITON METHOD FOR NONLINEAR OSCILLATORS

A NEW ASYMPTOTIC PERTURBAITON METHOD FOR NONLINEAR OSCILLATORS

来源 :The Third International Conference on Dynamics,Vibration and | 被引量 : 0次 | 上传用户：xyhanhui
【摘 要】
：
The study of nonlinear oscillations has occupied researchers for quite a long period of time.Various perturbation methods such as multiple scales method.Lindstedt-Poincaré method, harmonic balance met
【作 者】
：
Hu Hailiang Zhang Wei 
【机 构】
：
College of Mechanical Engineering,Beijing University,of Technology,Beijing 100124,China;College of M
【出 处】
：
The Third International Conference on Dynamics,Vibration and
【发表日期】
：
2010年4期
【关键词】
：
Nonlinear oscillators Perturbation method Asymptotic perturbation method 
下载到本地 , 更方便阅读
下载此文 赞助VIP
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
　　The study of nonlinear oscillations has occupied researchers for quite a long period of time.Various perturbation methods such as multiple scales method.Lindstedt-Poincaré method, harmonic balance method and Krylov-Bogoliubov-Mitropolsky (KBM) method have been developed to analysis nonlinear systems[1].ln 1996,A.Maccari[2-4] proposed a reasonably simple analytical method for the study of nonlinear systems.The asymptotic perturbation (AP) method provides a systematic means to obtain increasingly accurate solution by increasing the order of approximation in terms of the small parameter.
其他文献
BIFURCATION ANALYSIS OF NEARLY NONSMOOTH OSCILLATIONS IN INPUT-CONSTRAINED FLIGHT CONTROL SYSTEMS
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
会议
Flight controlnonlinear systemcontrol constraintsbifurcation analysislimit c
DESIGN AND ANALYSIS OF COMBINED NONLINEAR DYNAMIC INVERSION AND H∞-BASED FLIGHT CONTROL LAWS
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
会议
Nonlinear dynamic inversionH∞-based control designrobust performance and stabi
FLAP-LAG STABILITY OF HELICOPTER ROTOR BLADES USING CONTINUATION AND BIFURCATION METHODS
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
会议
Nonlinear periodic systemblade stabilityflap-lag stability helicopterbifurcat
MODELING AND CONTROL OF A MICRO FLAPPING WING ROTORCRAFT
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
会议
Flapping wingmicro rotorcraftelectromagnetic actuatorperiodic control
Modeling of Small Unmanned Aircraft with new configuration for Flight Control System Design
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
会议
flight dynamicsSmall Unmanned Aircraftnew configuration flight control system
RECONFIGURATION OF TETHERED SATELLITE FORMATIONS AT A COLLINEAR LIBRATION POINT
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
会议
Collinear libration point orbitstethered satellite formationsreconfigurationn
THE EFFECTS OF BRACINGS IN ELIMINATION OF VIBRATION LOCALIZATION IN MISTUNED BLADED-DISK ASSEMBLIES
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
会议
vibration localizationbladed-disk assembliesperiodic structuresproperties of
THE IMPACT OF THE ACTUATOR NON-LINEAR FACTORS ON THE FLIGHT DYNAMICS OF THE STATIC UNSTABLE AIRCRAFT
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
会议
Bifurcation analysisDead-zoneFlight control lawFlying wingNonlinear systemS
THE PREDICTION OF PIO SUSCEPTIBILITY OF A LARGE TRANSPORT AIRCRAFT
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
会议
Pilot-Induced Oscillationsflight control systemrate limiting elementscategory
TWO-STATE DYNAMIC GAIN SCHEDULING CONTROL APPLIED TO F16 AIRCRAFT MODEL
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 rec
会议
Nonlinear systemnonlinear controlgain schedulingdynamic gain scheduling