• 제목/요약/키워드: Nonstationary Random Excitation

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An equivalent linearization method for nonlinear systems under nonstationary random excitations using orthogonal functions

  • Younespour, Amir;Cheng, Shaohong;Ghaffarzadeh, Hosein
    • Structural Engineering and Mechanics
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    • 제66권1호
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    • pp.139-149
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    • 2018
  • Many practical engineering problems are associated with nonlinear systems subjected to nonstationary random excitations. Equivalent linearization methods are commonly used to seek for approximate solutions to this kind of problems. Compared to various approaches developed in the frequency and mixed time-frequency domains, though directly solving the system equation of motion in the time domain would improve computation efficiency, only limited studies are available. Considering the fact that the orthogonal functions have been widely used to effectively improve the accuracy of the approximated responses and reduce the computational cost in various engineering applications, an orthogonal-function-based equivalent linearization method in the time domain has been proposed in the current paper for nonlinear systems subjected to nonstationary random excitations. In the numerical examples, the proposed approach is applied to a SDOF system with a set-up spring and a SDOF Duffing oscillator subjected to stationary and nonstationary excitations. In addition, its applicability to nonlinear MDOF systems is examined by a 3DOF Duffing system subjected to nonstationary excitation. Results show that the proposed method can accurately predict the nonlinear system response and the formulation of the proposed approach allows it to be capable of handling any general type of nonstationary random excitations, such as the seismic load.

WAVELET ANALYSIS OF VEHICLE NONSTATIONARY VIBRATION UNDER CORRELATED FOUR-WHEEL RANDOM EXCITATION

  • Wang, Y.S.;Lee, C.M.;Zhang, L.J.
    • International Journal of Automotive Technology
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    • 제5권4호
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    • pp.257-268
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    • 2004
  • The wavelet analysis method is introduced in this paper to study the nonstationary vibration of vehicles. A new road model, a so-called time domain correlated four-wheel road roughness, which considers the coherence relationships between the four wheels of a vehicle, has been newly developed. Based on a vehicle model with eight degrees of freedom, the analysis of nonstationary random vibration responses was carried out in a time domain on a computer. Verification of the simulation results show that the proposed road model is more accurate than previous ones and that the simulated responses are credible enough when compared with some references. Furthermore, by taking wavelet analysis on simulated signals, some substantial rules of vehicle nonstationary vibration, such as the relationship between each vibration level, and how the vibration energy flows on a time-frequency map, beyond those from conventional spectral analysis, were revealed, and these will be of much benefit to vehicle design.

A STUDY ON NONSTATIONARY RANDOM VIBRATION OF A VEHICLE IN TIME AND FREQUENCY DOMAINS

  • Zhang, L.J.;Lee, C.M.;Wang, Y.S.
    • International Journal of Automotive Technology
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    • 제3권3호
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    • pp.101-109
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    • 2002
  • A time domain method for solving nonstationary random vibration caused by vehicle acceleration is first proposed in which a time changing model is established for representing nonstationary excitation of a rough road. Furthermore a novel frequency domain method called the transient power spectral density with spatial frequency (TPSD) is presented to obtain a response of vehicle system in frequency domain. This method has been proved to be valid by comparing numerical results with the exact solution.

Nonstationary Random Process를 이용한 인공지진파 발생 -설계응답스펙트럼에 의한 파워스펙트럼의 조정- (Generation of Artificial Earthquake Ground Motions using Nonstationary Random Process-Modification of Power Spectrum Compatible with Design Response Spectrum-)

  • 김승훈
    • 한국지진공학회:학술대회논문집
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    • 한국지진공학회 1999년도 춘계 학술발표회 논문집 Proceedings of EESK Conference-Spring
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    • pp.61-68
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    • 1999
  • In the nonlinear dynamic structural analysis the given ground excitation as an input should be well defined. Because of the lack of recorded accelerograms in Korea it is required to generate an artificial earthquake by a stochastic model of ground excitation with various dynamic properties rather than recorded accelerograms. It is well known that earthquake motions are generally non-stationary with time-varying intensity and frequency content. Many researchers have proposed non-stationary random process models. Yeh and Wen (1990) proposed a non-stationary modulation function and a power spectral density function to describe such non-stationary characteristics. Satio and Wen(1994) proposed a non-stationary stochastic process model to generate earthquake ground motions which are compatible with design reponse spectrum at sites in Japan. this paper shows the process to modify power spectrum compatible with target design response spectrum for generating of nonstationary artificial earthquake ground motions. Target reponse spectrum is chosen by ATC14 to calibrate the response spectrum according to a give recurrence period.

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비정상 랜덤 가진력을 받는 항공기 착륙장치의 응답해석 기법연구 (On the Approximate Solution of Aircraft Landing Gear under Nonstationary Random Excitations)

  • 황재혁;유병성;공병식
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1997년도 추계학술대회논문집; 한국과학기술회관; 6 Nov. 1997
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    • pp.345-351
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    • 1997
  • The motion of an aircraft landing gear over rough runway at variable speed is nonstationary. hi this paper, a method for the computation of nonstationary response variance is presented which uses a state space form for the combination of landing gear and runway excitation. The dynamic characteristics of the landing gear under nonstationazy random excitations has also been analyzed using the proposed method. The formulation is for linear systems of arbitrary order and allows any deterministic velocity history.

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비정상 랜덤 가진력을 받는 항공기 착륙장치의 동특성 해석 (Dynamic Analysis of Aircraft Landing Gear under Nonstationary Random Excitations)

  • 황재혁;유병성;박명호
    • 소음진동
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    • 제8권2호
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    • pp.251-259
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    • 1998
  • The motion of an aircraft landing gear over rough runway at variable speed is nonstationary. In this paper, a method for the computation of nonstationary response variance is presented which uses a state space form for the combination of landing gear and runway excitation. The dynamic characteristics of the landing gear under nonstationary random excitations has also been analyzed using the proposed method. The formulation is for linear systems of arbitrary order and allows any deterministic velocity history. It has been found by a series of simulation that correlation parameter, damping coefficients of landing gear and tire, and velocity profiles play a prominent role on the dynamic characteristics.

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On the Approximate Solution of Aircraft Landing Gear Under Nonstationary Random Excitations

  • Hwang, Jai-Hyuk;Kim, Jung-Soo
    • Journal of Mechanical Science and Technology
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    • 제14권9호
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    • pp.968-977
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    • 2000
  • The motion of an aircraft landing gear over a rough runway can be modeled by a nonclassically damped system subject to nonstationary random excitations. In this paper, the approximate analysis methods based on either the real or complex normal modes for the computation of nonstationary response covariances are proposed. It has been found by simulation involving a realistic example that, for the nonclassically damped random vibrational systems, the approximate solution method based on the complex normal mode is superior to other approaches with respect to the accuracy and computation time.

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비정상 랜덤 가진력을 받는 항공기 착륙장치의 동특성 해석 (Dynamic Analysis of Aircraft Landing Gear under Nonstationary Random Excitations)

  • 황재혁;유병성;박명호
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1997년도 춘계학술대회논문집; 경주코오롱호텔; 22-23 May 1997
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    • pp.60-68
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    • 1997
  • The motion of an aircraft landing gear over rough runway at variable speed is nonstationary. In this paper a method for the computation of nonstationary response variance is presented which uses a state space form for the combination of landing gear and runway excitation. The dynamic characteristics of the landing gear under nonstationary random excitations has also been analyzed using the proposed method. The formulation is for linear systems of arbitrary order and allows any deterministic velocity history. It has been found by a series of simulation that correlation parameter, damping coefficients of landing gear and tire, and velocity profiles plays a prominent role on the dynamic characteristics.

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유체-구조물 상호작용을 고려한 면진구조물의 추계학적 응답해석 (Stochastic Analysis of Base-Isolated Pool Structure Considering Fluid-Structure Interaction Effects)

  • 고현무;김재관;박관순;하동호
    • 대한토목학회논문집
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    • 제14권3호
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    • pp.463-472
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    • 1994
  • Random 지반운동에 대한 면진수조구조물 응답의 추계학적 해석방법을 연구하였다. 유연한 벽체와 내부유체간의 유체구조물 상호작용은 유체운동의 유한요소 모델링에 의하여 얻어지는 부가질량행렬 형태로 고려되었다. 정상(定常)(Stationary)지반운동으로는 수정된 Clough-Penzien Spectral Model이 사용되었으며, 비정상(非定常)(Nonstationary)지반운동으로는 상기모델에 포락함수를 적용한 모델을 사용하였다. 운동을 지배하는 Lyapunov Covariance Matrix 미분방정식의 해를 구하여 두 종류 면진시스템의 정상응답 및 비정상응답을 해석하였다.

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비정상과정의 강한 지진에 대한 해양 가이드 타워의 동력학적 응답해석 (Nonstationary Response Analysis of Offshore Guyed Tower for Strong Earthquakes)

  • 류정선
    • 전산구조공학
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    • 제5권3호
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    • pp.127-137
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    • 1992
  • 해양 가이드 타워를 대상으로 하여 지진하중에 대한 심해용 구조물의 비정상 거동해법에 대하여 연구하였다. 지반운동의 비정상 특성을 정상과정 성분에 시간포락함수가 곱해진 형태로 모형화하였으며, 구조물의 비정상 거동은 시간종속 분산함수로 구하였다. 지진의 시간포락함수와 정상과정 성분의 자기상관함수를 지수함수로 수식화하여 나타냄으로써, 구조물 거동의 시간종속 분산값을 해석적인 방법으로 구할 수 있는 기법을 개발하였다. 시간에 따른 거동의 분산값을 기본자료로 하여 지진의 발생기간 동안 예상되는 최대거동을 구하였으며, 이 값을 구조물 거동을 정상과정으로 가정하여 산정한 결과와 비교 분석하였다.

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