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Upper-Bound Limit Analysis of the Multi-Layer Slope Stability and Failure Mode Based on Generalized Horizontal Slice Method
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作者 Huawei Zhang Changdong Li +5 位作者 Wenqiang Chen Ni Xie Guihua Wang Wenmin Yao Xihui Jiang Jingjing Long 《Journal of Earth Science》 SCIE CAS CSCD 2024年第3期929-940,共12页
Multi-layer slopes are widely found in clay residue receiving fields.A generalized horizontal slice method(GHSM)for assessing the stability of multi-layer slopes that considers the energy dissipation between adjacent ... Multi-layer slopes are widely found in clay residue receiving fields.A generalized horizontal slice method(GHSM)for assessing the stability of multi-layer slopes that considers the energy dissipation between adjacent horizontal slices is presented.In view of the upper-bound limit analysis theory,the energy equation is derived and the ultimate failure mode is generated by comparing the sliding surface passing through the slope toe(mode A)with that below(mode B).In addition,the influence of the number of slices on the stability coefficients in the GHSM is studied and the stable value is obtained.Compared to the original method(Chen’s method),the GHSM can acquire more precise results,which takes into account the energy dissipation in the inner sliding soil mass.Moreover,the GHSM,limit equilibrium method(LEM)and numerical simulation method(NSM)are applied to analyze the stability of a multi-layer slope with different slope angles and the results of the safety factor and failure mode are very close in each case.The ultimate failure modes are shown to be mode B when the slope angle is not more than 28°.It illustrates that the determination of the ultimate sliding surface requires comparison of multiple failure modes,not only mode A. 展开更多
关键词 stability and failure mode slope stability generalized horizontal slice method upperbound limit analysis energy dissipation geotechnical engineering.
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A New Grasping Mode Based on a Sucked-type Underactuated Hand 被引量:5
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作者 Pei-Chen Wu Nan Lin +3 位作者 Ting Lei Qian Cheng Jin-Ze Wu Xiao-Ping Chen 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2018年第6期25-33,共9页
Robot hands have been developing during the last few decades. There are many mechanical structures and analyti?cal methods for di erent hands. But many tough problems still limit robot hands to apply in homelike envir... Robot hands have been developing during the last few decades. There are many mechanical structures and analyti?cal methods for di erent hands. But many tough problems still limit robot hands to apply in homelike environment. The ability of grasping objects covering a large range of sizes and various shapes is fundamental for a home service robot to serve people better. In this paper, a new grasping mode based on a novel sucked?type underactuated(STU) hand is proposed. By combining the flexibility of soft material and the e ect of suction cups, the STU hand can grasp objects with a wide range of sizes, shapes and materials. Moreover, the new grasping mode is suitable for some situations where the force closure is failure. In this paper, we deduce the e ective range of sizes of objects which our hand using the new grasping mode can grasp. Thanks to the new grasping mode, the ratio of grasping size between the biggest object and the smallest is beyond 40, which makes it possible for our robot hand to grasp diverse objects in our daily life. For example, the STU hand can grasp a soccer(220 mm diameter, 420 g) and a fountain pen(9 mm diameter, 9 g). What’s more, we use the rigid body equilibrium conditions to analysis the force condition. Experiment evaluates the high load capacity, stability of the new grasping mode and displays the versatility of the STU hand. The STU hand has a wide range of applications especially in unstructured environment. 展开更多
关键词 Grasping mode Underactuated hand Sucked?type stability of new mode Grasping diverse objects
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Dynamic flight stability of a bumblebee in forward flight 被引量:8
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作者 Yan Xiong Mao Sun 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2008年第1期25-36,共12页
The longitudinal dynamic flight stability of a bumblebee in forward flight is studied. The method of computational fluid dynamics is used to compute the aerodynamic derivatives and the techniques of eigenvalue and eig... The longitudinal dynamic flight stability of a bumblebee in forward flight is studied. The method of computational fluid dynamics is used to compute the aerodynamic derivatives and the techniques of eigenvalue and eigenvector analysis are employed for solving the equations of motion. The primary findings are as the following. The forward flight of the bumblebee is not dynamically stable due to the existence of one (or two) unstable or approximately neutrally stable natural modes of motion. At hovering to medium flight speed [flight speed Ue = (0-3.5)m s^-1; advance ratio J = 0-0.44], the flight is weakly unstable or approximately neutrally stable; at high speed (Ue = 4.5 m s^-1; J = 0.57), the flight becomes strongly unstable (initial disturbance double its value in only 3.5 wingbeats). 展开更多
关键词 Bumblebee Dynamic stability Forward flight Navier-Stokes simulation Natural modes of motion
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Dynamic Stability Analysis of Linear Time-varying Systems via an Extended Modal Identification Approach 被引量:2
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作者 Zhisai MA Li LIU +3 位作者 Sida ZHOU Frank NAETS Ward HEYLEN Wim DESMET 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2017年第2期459-471,共13页
The problem of linear time-varying(LTV) system modal analysis is considered based on time-dependent state space representations, as classical modal analysis of linear time-invariant systems and current LTV system mo... The problem of linear time-varying(LTV) system modal analysis is considered based on time-dependent state space representations, as classical modal analysis of linear time-invariant systems and current LTV system modal analysis under the "frozen-time" assumption are not able to determine the dynamic stability of LTV systems. Time-dependent state space representations of LTV systems are first introduced, and the corresponding modal analysis theories are subsequently presented via a stabilitypreserving state transformation. The time-varying modes of LTV systems are extended in terms of uniqueness, and are further interpreted to determine the system's stability. An extended modal identification is proposed to estimate the time-varying modes, consisting of the estimation of the state transition matrix via a subspace-based method and the extraction of the time-varying modes by the QR decomposition. The proposed approach is numerically validated by three numerical cases, and is experimentally validated by a coupled moving-mass simply supported beam exper- imental case. The proposed approach is capable of accurately estimating the time-varying modes, and provides anew way to determine the dynamic stability of LTV systems by using the estimated time-varying modes. 展开更多
关键词 Linear time·varying systems · Extended modal identification · Dynamic stability analysis · Time·varying modes
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Analysis of Effects of the Arc Voltage on Arc Discharges in a Cathode Ion Source of Neutral Beam Injector
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作者 陈俞钱 胡纯栋 谢亚红 《Plasma Science and Technology》 SCIE EI CAS CSCD 2016年第4期453-456,共4页
A hot cathode bucket ion source is used for the EAST(experimental advanced superconducting tokamak)neutral beam injector.The thermal electrons emitted from the surface of the cathode are extracted and accelerated by... A hot cathode bucket ion source is used for the EAST(experimental advanced superconducting tokamak)neutral beam injector.The thermal electrons emitted from the surface of the cathode are extracted and accelerated by the electric field formed by the arc voltage,which is applied between the arc chamber of the ion source and the cathode.This paper analyzes the effects of arc voltage on the arc discharge in a hot cathode high current ion source. 展开更多
关键词 high current ion source arc discharge thermal emission limited mode stability
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IMPROVED COVARIANCE DRIVEN BLIND SUBSPACE IDENTIFICATION METHOD
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作者 ZHANG Zhiyi FAN Jiangling HUA Hongxing 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2006年第4期548-553,共6页
An improved covariance driven subspace identification method is presented to identify the weakly excited modes. In this method, the traditional Hankel matrix is replaced by a reformed one to enhance the identifiabilit... An improved covariance driven subspace identification method is presented to identify the weakly excited modes. In this method, the traditional Hankel matrix is replaced by a reformed one to enhance the identifiability of weak characteristics. The robustness of eigenparameter estimation to noise contamination is reinforced by the improved Hankel matrix, in combination with component energy index (CEI) which indicates the vibration intensity of signal components, an alternative stabilization diagram is adopted to effectively separate spurious and physical modes. Simulation of a vibration system of multiple-degree-of-freedom and experiment of a frame structure subject to wind excitation are presented to demonstrate the improvement of the proposed blind method. The performance of this blind method is assessed in terms of its capability in extracting the weak modes as well as the accuracy of estimated parameters. The results have shown that the proposed blind method gives a better estimation of the weak modes from response signals of small signal to noise ratio (SNR)and gives a reliable separation of spurious and physical estimates. 展开更多
关键词 Subspace identification method Weak modes Hankel matrix Component energy index (CEI) Stabilization diagram
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Scaling effects on combustion modes in a single-side expansion kerosene-fueled scramjet combustor 被引量:3
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作者 Fan LI Mingbo SUN +4 位作者 Jiajian ZHU Zun CAI Hongbo WANG Yanxiang ZHANG Yongchao SUN 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2021年第5期684-690,共7页
The combustion modes in two different scramjet combustors with the mass flow rates of 1.8 kg/s and 3.6 kg/s are experimentally investigated to explore the scaling effects on supersonic combustion with a Mach number 2.... The combustion modes in two different scramjet combustors with the mass flow rates of 1.8 kg/s and 3.6 kg/s are experimentally investigated to explore the scaling effects on supersonic combustion with a Mach number 2.0 inflow.It is found that the scramjet combustor with a larger scale can broaden the flame rich blowout limit.As the Equivalence Ratio(ER)increases,the combustion in the small-scale combustor maintains in the cavity-stabilized mode,and the flamebase moves downstream along the cavity shear layer;however,the combustion in the large-scale combustor gradually transfers from the cavity-stabilized mode to the jet-wake-stabilized mode.The differences in the cavity residence time,the ignition delay time and the Damkohler number caused by different scales of the scramjet combustor are likely to account for the scaling effects on the combustion modes. 展开更多
关键词 Cavity COMBUSTION Combustion stabilized mode Scaling effect SCRAMJET SUPERSONIC
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A 0.6 V 10 bit 1 MS/s monotonic switching SAR ADC with common mode stabilizer in 0.13 μm CMOS
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作者 吕伟 罗多纳 +4 位作者 梅逢城 杨家琪 姚立斌 贺林 林福江 《Journal of Semiconductors》 EI CAS CSCD 2014年第5期98-104,共7页
This paper presents a 0.6 V 10 bit successive approximation register (SAR) ADC design dedicated to the wireless sensor network application. It adopts a monotonic switching scheme in the DAC to save chip area and pow... This paper presents a 0.6 V 10 bit successive approximation register (SAR) ADC design dedicated to the wireless sensor network application. It adopts a monotonic switching scheme in the DAC to save chip area and power consumption. The main drawback of the monotonic switching scheme is its large common mode shift and the associated comparator offset variation. Due to the limited headroom at the 0.6 V supply voltage, the conventional constant current biasing technique cannot be applied to the dynamic comparator. In this design, a common mode stabilizer is introduced to address this issue in low-voltage design. The effectiveness of this method is verified through both simulation and measurement results. Fabricated with 1P8M 0.13 μm CMOS technology, the proposed SAR ADC consumes 6.3 μW at 1 MS/s from a 0.6 V supply, and achieves 51.25 dB SNDR at the Nyquist frequency and FOM of 21 fJ/conversion-step. The core area is only 120 × 300 μm^2. 展开更多
关键词 SAR ADC monotonic switching common mode stabilizer comparator offset
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Design and studies on the traveling wave transverse RF deflecting structure 被引量:1
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作者 张敬如 侯汨 +2 位作者 戴建枰 裴士伦 裴国玺 《Chinese Physics C》 SCIE CAS CSCD 北大核心 2008年第3期232-235,共4页
With the development of free electron laser (FEL) and the international linear collider (ILC), the electron bunch length is getting smaller and smaller, The traveling-wave transverse RF deflecting structure is an ... With the development of free electron laser (FEL) and the international linear collider (ILC), the electron bunch length is getting smaller and smaller, The traveling-wave transverse RF deflecting structure is an important part of the RF deflecting method for bunch length measurement and phase space diagnostics. The operation mode in RF deflector is the "TM11-like" mode. Since the TM11-like mode in this structure has a pair of degenerate dipole modes, two additional holes are provided on either side of each iris to stabilize the mode. The simulation and optimization have been done. A prototype has been fabricated and tested. The cold test results have been compared with the simulations of the first three modes. 展开更多
关键词 TM11-like mode RF deflector mode stabilizer vertical polarized wave parallel polarized wave
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Approach and landing guidance design for reusable launch vehicle using multiple sliding surfaces technique 被引量:1
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作者 Xiangdong LIU Fengdi ZHANG +1 位作者 Zhen LI Yao ZHAO 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2017年第4期1582-1591,共10页
An autonomous approach and landing(A&L) guidance law is presented in this paper for landing an unpowered reusable launch vehicle(RLV) at the designated runway touchdown. Considering the full nonlinear point-mass ... An autonomous approach and landing(A&L) guidance law is presented in this paper for landing an unpowered reusable launch vehicle(RLV) at the designated runway touchdown. Considering the full nonlinear point-mass dynamics, a guidance scheme is developed in threedimensional space. In order to guarantee a successful A&L movement, the multiple sliding surfaces guidance(MSSG) technique is applied to derive the closed-loop guidance law, which stems from higher order sliding mode control theory and has advantage in the finite time reaching property.The global stability of the proposed guidance approach is proved by the Lyapunov-based method.The designed guidance law can generate new trajectories on-line without any specific requirement on off-line analysis except for the information on the boundary conditions of the A&L phase and instantaneous states of the RLV. Therefore, the designed guidance law is flexible enough to target different touchdown points on the runway and is capable of dealing with large initial condition errors resulted from the previous flight phase. Finally, simulation results show the effectiveness of the proposed guidance law in different scenarios. 展开更多
关键词 Finite time control Landing guidance Lyapunov stability Reusable launch vehicle Sliding mode control
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