期刊文献+
共找到5,345篇文章
< 1 2 250 >
每页显示 20 50 100
Numerical investigation on the engraving process of a pyrotechnic actuator with an improved two-phase flow model of interior ballistic
1
作者 Yue Li Cong Liu +1 位作者 Cheng Cheng Genghui Jiang 《Defence Technology(防务技术)》 2025年第4期120-132,共13页
By combining with an improved model on engraving process,a two-phase flow interior ballistic model has been proposed to accurately predict the flow and energy conversion behaviors of pyrotechnic actuators.Using comput... By combining with an improved model on engraving process,a two-phase flow interior ballistic model has been proposed to accurately predict the flow and energy conversion behaviors of pyrotechnic actuators.Using computational fluid dynamics(CFD),the two-phase flow and piston engraving characteristics of a pyrotechnic actuator are investigated.Initially,the current model was utilized to examine the intricate,multi-dimensional flow,and energy conversion characteristics of the propellant grains and combustion gas within the pyrotechnic actuator chamber.It was discovered that the combustion gas on the wall's constant transition from potential to kinetic energy,along with the combined effect of the propellant motion,are what create the pressure oscillation within the chamber.Additionally,a numerical analysis was conducted to determine the impact of various parameters on the pressure oscillation and piston motion,including pyrotechnic charge,pyrotechnic particle size,and chamber structural dimension.The findings show that decreasing the pyrotechnic charge will lower the terminal velocity,while increasing and decreasing the pyrotechnic particle size will reduce the pressure oscillation in the chamber.The pyrotechnic particle size has minimal bearing on the terminal velocity.The results of this investigation offer a trustworthy forecasting instrument for comprehending and creating pyrotechnic actuator designs. 展开更多
关键词 Pyrotechnic actuator Engraving process Two-phase flow Pressure oscillation
在线阅读 下载PDF
Hysteresis modeling and compensation of piezo actuator with sparse regression
2
作者 JIN Yu WANG Xucheng +3 位作者 XU Yunlang YU Jianbo LU Qiaodan YANG Xiaofeng 《Journal of Systems Engineering and Electronics》 2025年第1期48-61,共14页
Piezo actuators are widely used in ultra-precision fields because of their high response and nano-scale step length.However,their hysteresis characteristics seriously affect the accuracy and stability of piezo actuato... Piezo actuators are widely used in ultra-precision fields because of their high response and nano-scale step length.However,their hysteresis characteristics seriously affect the accuracy and stability of piezo actuators.Existing methods for fitting hysteresis loops include operator class,differential equation class,and machine learning class.The modeling cost of operator class and differential equation class methods is high,the model complexity is high,and the process of machine learning,such as neural network calculation,is opaque.The physical model framework cannot be directly extracted.Therefore,the sparse identification of nonlinear dynamics(SINDy)algorithm is proposed to fit hysteresis loops.Furthermore,the SINDy algorithm is improved.While the SINDy algorithm builds an orthogonal candidate database for modeling,the sparse regression model is simplified,and the Relay operator is introduced for piecewise fitting to solve the distortion problem of the SINDy algorithm fitting singularities.The Relay-SINDy algorithm proposed in this paper is applied to fitting hysteresis loops.Good performance is obtained with the experimental results of open and closed loops.Compared with the existing methods,the modeling cost and model complexity are reduced,and the modeling accuracy of the hysteresis loop is improved. 展开更多
关键词 sparse identification of nonlinear dynamics(SINDy) hysteresis loop relay operator sparse regression piezo actuator
在线阅读 下载PDF
Adaptive fault-tolerant control based on boundary estimation for space robot under joint actuator faults and uncertain parameters 被引量:5
3
作者 Rong-Hua Lei Li Chen 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2019年第6期964-971,共8页
Since the joint actuator of the space robot executes the control instructions frequently in the harsh space environment,it is prone to the partial loss of control effectiveness(PLCE)fault.An adaptive fault-tolerant co... Since the joint actuator of the space robot executes the control instructions frequently in the harsh space environment,it is prone to the partial loss of control effectiveness(PLCE)fault.An adaptive fault-tolerant control algorithm is designed for a space robot system with the uncertain parameters and the PLCE actuator faults.The mathematical model of the system is established based on the Lagrange method,and the PLCE actuator fault is described as an effectiveness factor.The lower bound of the effectiveness factors and the upper bound of the uncertain parameters are estimated by an adaptive strategy,and the estimated value is fed back to the control algorithm.Compared with the traditional fault-tolerant algorithms,the proposed algorithm does not need to predetermine the lower bound of the effectiveness factor,hence it is more in line with the actual engineering application.It is proved that the algorithm can guarantee the stability of the closed-loop system based on the Lyapunov function method.The numerical simulation results show that the proposed algorithm can not only compensate for the uncertain parameters,but also can tolerate the PLCE actuator faults effectively,which verifies the effectiveness and superiority of the control scheme. 展开更多
关键词 Space robot actuator faults Uncertain parameters Effectiveness factor Fault-tolerant control
在线阅读 下载PDF
Design of wearable hand rehabilitation glove with soft hoop-reinforced pneumatic actuator 被引量:16
4
作者 SUN Zhong-sheng GUO Zhong-hua TANG Wei 《Journal of Central South University》 SCIE EI CAS CSCD 2019年第1期106-119,共14页
Traditional hand rehabilitation gloves usually use electrical motor as actuator with disadvantages of heaviness,bulkiness and less compliance.Recently,the soft pneumatic actuator is demonstrated to be more suitable fo... Traditional hand rehabilitation gloves usually use electrical motor as actuator with disadvantages of heaviness,bulkiness and less compliance.Recently,the soft pneumatic actuator is demonstrated to be more suitable for hand rehabilitation compared to motor because of its inherent compliance,flexibility and safety.In order to design a wearable glove in request of hand rehabilitation,a soft hoop-reinforced pneumatic actuator is presented.By analyzing the influence of its section shape and geometrical parameters on bending performance,the preferred structure of actuator is achieved based on finite element method.An improved hoop-reinforced actuator is designed after the fabrication and initial measurement,and its mathematical model is built in order to quickly obtain the bending angle response when pressurized.A series of experiment about bending performance are implemented to validate the agreement between the finite element,mathematical and experimental results,and the performance improvement of hoop-reinforced actuator.In addition,the designed hand rehabilitation glove is tested by measuring its output force and actual wearing experience.The output force can reach 2.5 to 3 N when the pressure is 200 kPa.The research results indicate that the designed glove with hoop-reinforced actuator can meet the requirements of hand rehabilitation and has prospective application in hand rehabilitation. 展开更多
关键词 PNEUMATIC soft actuator hoop-reinforced hand rehabilitation
在线阅读 下载PDF
Reference tracking control for flexible air-breathing hypersonic vehicle with actuator delay and uncertainty 被引量:3
5
作者 Hongyi Li Yiming Cheng Yulin Si Huijun Gao 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2011年第1期141-145,共5页
This paper considers the problem of reference tracking control for the flexible air-breathing hypersonic flight vehicle with actuator delay and uncertainty.By constructing the Lyapunov functional including the lower a... This paper considers the problem of reference tracking control for the flexible air-breathing hypersonic flight vehicle with actuator delay and uncertainty.By constructing the Lyapunov functional including the lower and upper bounds of the time-varying delay,the non-fragile controller is designed such that the resulting closed-loop system is asymptotically stable and satisfies a prescribed performance cost index.The simulation results are given to show the effectiveness of the proposed control method,which is validated by excellent output reference altitude and velocity tracking performance. 展开更多
关键词 actuator delay flexible air-breathing hypersonic flight vehicle(FAHFV) non-fragile control output tracking control.
在线阅读 下载PDF
Robust reliable H_∞ control for discrete-time Markov jump linear systems with actuator failures 被引量:2
6
作者 Chen Jiaorong Liu Fei 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2008年第5期965-973,共9页
The robust reliable H∞ control problem for discrete-time Markovian jump systems with actuator failures is studied. A more practical model of actuator failures than outage is considered. Based on the state feedback me... The robust reliable H∞ control problem for discrete-time Markovian jump systems with actuator failures is studied. A more practical model of actuator failures than outage is considered. Based on the state feedback method, the resulting closed-loop systems are reliable in that they remain robust stochastically stable and satisfy a certain level of H∞ disturbance attenuation not only when all actuators are operational, but also in case of some actuator failures, The solvability condition of controllers can be equivalent to a feasibility problem of coupled linear matrix inequalities (LMIs). A numerical example is also given to illustrate the design procedures and their effectiveness. 展开更多
关键词 discrete-time Markov jump systems actuator failure reliable control robust H∞-control time-delay.
在线阅读 下载PDF
Disturbance observer based position tracking of electro-hydraulic actuator 被引量:4
7
作者 国凯 魏建华 田启岩 《Journal of Central South University》 SCIE EI CAS CSCD 2015年第6期2158-2165,共8页
A nonlinear controller based on an extended second-order disturbance observer is presented to track desired position for an electro-hydraulic single-rod actuator in the presence of both external disturbances and param... A nonlinear controller based on an extended second-order disturbance observer is presented to track desired position for an electro-hydraulic single-rod actuator in the presence of both external disturbances and parameter uncertainties. The proposed extended second-order disturbance observer deals with not only the external perturbations, but also parameter uncertainties which are commonly regarded as lumped disturbances in previous researches. Besides, the outer position tracking loop is designed with cylinder load pressure as output; and the inner pressure control loop provides the hydraulic actuator the characteristic of a force generator. The stability of the closed-loop system is provided based on Lyapunov theory. The performance of the controller is verified through simulations and experiments. The results demonstrate that the proposed nonlinear position tracking controller, together with the extended second-order disturbance observer, gives an excellent tracking performance in the presence of parameter uncertainties and external disturbance. 展开更多
关键词 electro-hydraulic system single-rod actuator disturbance observer external disturbance parameter uncertainty
在线阅读 下载PDF
Observer-based backstepping longitudinal control for carrier-based UAV with actuator faults 被引量:9
8
作者 Fengying Zheng Ziyang Zhen Huajun Gong 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2017年第2期322-337,共16页
The paper presents the longitudinal control for the carrier-based unmanned aerial vehicle (UAV) system with unmeasured states, actuator faults, control input constraints, and external disturbances. By combining output... The paper presents the longitudinal control for the carrier-based unmanned aerial vehicle (UAV) system with unmeasured states, actuator faults, control input constraints, and external disturbances. By combining output state observer, adaptive fuzzy control, and constraint backstepping technology, a robust fault tolerant control approach is proposed. An output state observer with fuzzy logic systems is developed to estimate unmeasured states, and command filters rather than differentiations of virtual control law are used to solve the computational complexity problem in traditional backstepping. Additionally, a robust term is introduced to offset the fuzzy adaptive estimation error and external disturbance, and an appropriate fault controller structure with matching conditions obtained from fault compensation is proposed. Based on the Lyapunov theory, the designed control program is illustrated to guarantee that all the closed-loop signals of the given system are bounded, and the output errors converge to a small neighborhood of zero. A carrier-based UAV nonlinear longitudinal model is employed to testify the feasibility and validity of the control scheme. The simulation results show that all the controllers can perform at a satisfactory level of reference tracking despite the existence of unknown aerodynamic parameters and actuator faults. © 2017 Beijing Institute of Aerospace Information. 展开更多
关键词 actuators Aircraft control BACKSTEPPING Control system analysis Control theory Controllers Error compensation Fault tolerance Flight control systems Fuzzy control Fuzzy filters Fuzzy logic State estimation Three term control systems Unmanned aerial vehicles (UAV)
在线阅读 下载PDF
Simultaneous anti-windup synthesis for linear systems subject to actuator saturation 被引量:1
9
作者 Maopeng Ran Qing Wang +1 位作者 Chaoyang Dong Maolin Ni 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2015年第1期119-126,共8页
A synthesis method for global stability and performance of input constrained linear systems, which uses a linear outputfeedback controller and a static anti-windup compensator is investigated. Different from the tradi... A synthesis method for global stability and performance of input constrained linear systems, which uses a linear outputfeedback controller and a static anti-windup compensator is investigated. Different from the traditional two-step anti-windup design procedure, the proposed method synthesizes all controller parameters simultaneously. Sufficient conditions for global stability and minimizing the induced L2 gain are formulated and solved as a linear matrix inequalities(LMIs) optimization problem, which also provides an opportunity to search for a better performance tradeoff between the linear controller and the anti-windup compensator.The well-posedness of the close-loop system is also guaranteed.Simulation results show the effectiveness of the proposed method. 展开更多
关键词 actuator saturation ANTI-WINDUP simultaneous synthesis L2 synthesis linear matrix inequalities(LMIs)
在线阅读 下载PDF
A parameter estimation based adaptive actuator failure compensation control scheme 被引量:1
10
作者 Gang Tao Ruiyun Qi Chang Tan 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2011年第1期1-11,共11页
An adaptive actuator failure compensation control scheme is developed using an indirect adaptive control method,by calculating the controller parameters from adaptive estimates of system parameters and actuator failur... An adaptive actuator failure compensation control scheme is developed using an indirect adaptive control method,by calculating the controller parameters from adaptive estimates of system parameters and actuator failure parameters.A key technical issue is how to deal with the actuator failure uncertainties such as failure pattern,time and values.A complete parametrization covering all possible failures is used to solve this issue for adaptive parameter estimation.A simultaneous mapping from the estimated system/failure parameters to the controller parameters is employed to make the control system capable of ensuring the desired system performance under failures,which is verified by simulation results. 展开更多
关键词 actuator failure compensation adaptive control failure pattern and values parameter estimation stability and tracking uncertainty parametrization.
在线阅读 下载PDF
Optimization of actuator/sensor position of multi-body system with quick startup and brake 被引量:3
11
作者 唐华平 唐春喜 殷陈锋 《Journal of Central South University of Technology》 EI 2007年第6期803-807,共5页
A new method was put forward to optimize the position of actuator/sensor of multi-body system with quick startup and brake. Dynamical equation was established for the system with intelligent structure of piezoelectric... A new method was put forward to optimize the position of actuator/sensor of multi-body system with quick startup and brake. Dynamical equation was established for the system with intelligent structure of piezoelectric actuators. According to the property of the modes varying with time, the performance index function was developed based on the optimal configuration principle of energy maximal dissipation, and the relevant optimal model was obtained. According to its characteristic, a float-encoding genetic algorithm, which is efficient, simple and excellent for solving the global-optimal solution of this problem, was adopted. Taking the plane manipulator as an example, the result of numerical calculation shows that, after the actuator/sensor position being optimized, the vibration amplitude of the multi-body system is reduced by 35% compared with that without optimization. 展开更多
关键词 actuator/sensor multi-body system active control OPTIMIZATION genetic algorithm
在线阅读 下载PDF
Multi-objectives nonlinear structure optimization for actuator in trajectory correction fuze subject to high impact loadings 被引量:4
12
作者 Jiang-hai Hui Min Gao +3 位作者 Ming Li Ming-rui Li Hui-hui Zou Gang Zhou 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2021年第4期1338-1351,共14页
This paper presents an actuator used for the trajectory correction fuze,which is subject to high impact loadings during launch.A simulation method is carried out to obtain the peak-peak stress value of each component,... This paper presents an actuator used for the trajectory correction fuze,which is subject to high impact loadings during launch.A simulation method is carried out to obtain the peak-peak stress value of each component,from which the ball bearings are possible failures according to the results.Subsequently,three schemes against impact loadings,full-element deep groove ball bearing and integrated raceway,needle roller thrust bearing assembly,and gaskets are utilized for redesigning the actuator to effectively reduce the bearings’stress.However,multi-objectives optimization still needs to be conducted for the gaskets to decrease the stress value further to the yield stress.Four gasket’s structure parameters and three bearings’peak-peak stress are served as the four optimization variables and three objectives,respectively.Optimized Latin hypercube design is used for generating sample points,and Kriging model selected according to estimation result can establish the relationship between the variables and objectives,representing the simulation which is time-consuming.Accordingly,two optimization algorithms work out the Pareto solutions,from which the best solutions are selected,and verified by the simulation to determine the gaskets optimized structure parameters.It can be concluded that the simulation and optimization method based on these components is effective and efficient. 展开更多
关键词 actuator Trajectory correction fuze Impact loadings Optimized Latin hypercube design Kriging model Optimization algorithm
在线阅读 下载PDF
Dynamic friction modelling and parameter identification for electromagnetic valve actuator 被引量:6
13
作者 SHAO Da XU Si-chuan DU Ai-min 《Journal of Central South University》 SCIE EI CAS CSCD 2018年第12期3004-3020,共17页
A new modified LuGre friction model is presented for electromagnetic valve actuator system.The modification to the traditional LuGre friction model is made by adding an acceleration-dependent part and a nonlinear cont... A new modified LuGre friction model is presented for electromagnetic valve actuator system.The modification to the traditional LuGre friction model is made by adding an acceleration-dependent part and a nonlinear continuous switch function.The proposed new friction model solves the implementation problems with the traditional LuGre model at high speeds.An improved artificial fish swarm algorithm(IAFSA)method which combines the chaotic search and Gauss mutation operator into traditional artificial fish swarm algorithm is used to identify the parameters in the proposed modified LuGre friction model.The steady state response experiments and dynamic friction experiments are implemented to validate the effectiveness of IAFSA algorithm.The comparisons between the measured dynamic friction forces and the ones simulated with the established mathematic friction model at different frequencies and magnitudes demonstrate that the proposed modified LuGre friction model can give accurate simulation about the dynamic friction characteristics existing in the electromagnetic valve actuator system.The presented modelling and parameter identification methods are applicable for many other high-speed mechanical systems with friction. 展开更多
关键词 LuGre friction model artificial fish swarm algorithm Gauss mutation chaotic search parameter identification electromagnetic valve actuator
在线阅读 下载PDF
Distributed fault diagnosis observer for multi-agent system against actuator and sensor faults 被引量:3
14
作者 YE Zhengyu JIANG Bin +2 位作者 CHENG Yuehua YU Ziquan YANG Yang 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2023年第3期766-774,共9页
Component failures can cause multi-agent system(MAS)performance degradation and even disasters,which provokes the demand of the fault diagnosis method.A distributed sliding mode observer-based fault diagnosis method f... Component failures can cause multi-agent system(MAS)performance degradation and even disasters,which provokes the demand of the fault diagnosis method.A distributed sliding mode observer-based fault diagnosis method for MAS is developed in presence of actuator and sensor faults.Firstly,the actuator and sensor faults are extended to the system state,and the system is transformed into a descriptor system form.Then,a sliding mode-based distributed unknown input observer is proposed to estimate the extended state.Furthermore,adaptive laws are introduced to adjust the observer parameters.Finally,the effectiveness of the proposed method is demonstrated with numerical simulations. 展开更多
关键词 multi-agent system(MAS) sensor fault actuator fault unknown input observer sliding mode fault diagnosis
在线阅读 下载PDF
Ionic polymer metal composites actuators with enhanced driving performance by incorporating graphene quantum dots 被引量:1
15
作者 YIN Guo-xiao HE Qing-song +2 位作者 YU Min WU Yu-wei XU Xian-rui 《Journal of Central South University》 SCIE EI CAS CSCD 2022年第5期1412-1422,共11页
In order to further improve the driving performance of ionic polymer metal composites(IPMCs),Nafion/graphene quantum dots(GQDs)hybrid membranes incorporating GQDs with various contents of 0,0.1 wt.%,0.5 wt.%,1.0 wt.%,... In order to further improve the driving performance of ionic polymer metal composites(IPMCs),Nafion/graphene quantum dots(GQDs)hybrid membranes incorporating GQDs with various contents of 0,0.1 wt.%,0.5 wt.%,1.0 wt.%,2.0 wt.%and 4.0 wt.%were fabricated by solution casting,and then IPMCs were manufactured by electroless plating.The water contents and elastic moduli of the hybrid membranes were tested.The morphology characteristics of the hybrid membranes and the IPMCs were observed,and the current,AC impedance,blocking force and displacement of the IPMCs were measured.The results show that the elastic modulus of the hybrid membranes decreases,the water content increases,and the actuation performance of the IPMCs improves significantly after the addition of GQDs.IPMC with 1.0 wt.%GQDs exhibits the best driving property.Compared with the IPMC without GQDs,the working current,ion conductivity,blocking force,and tip displacement increase by 94.67%,311.11%,53.66%,and 66.07%,respectively.These results lay a solid foundation for the preparation of IPMCs with high performance,and further broaden their applications in biomedical devices and bionic robots. 展开更多
关键词 graphene quantum dots hybrid membrane ionic polymer metal composites actuation performance
在线阅读 下载PDF
Multiple Model-based Adaptive Reconfiguration Control for Actuator Fault 被引量:9
16
作者 GUO Yu-Ying JIANG Bin 《自动化学报》 EI CSCD 北大核心 2009年第11期1452-1458,共7页
关键词 执行器 二阶动态 仿真结果 计算方法
在线阅读 下载PDF
Finite-time control of formation system for multiple flight vehicles subject to actuator saturation 被引量:1
17
作者 ZHAO Enjiao ZHONG Zenan ZHENG Xin 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2020年第5期1019-1030,共12页
This paper investigates the problem of formation tracking control for multiple flight vehicle(MFV) system considering actuator saturation constraints. First, the formation tracking control model is established. Then, ... This paper investigates the problem of formation tracking control for multiple flight vehicle(MFV) system considering actuator saturation constraints. First, the formation tracking control model is established. Then, the problem of formation control of the MFV system is converted to the convergence of a dynamical system, which is obtained by using the differential geometry theory.A class of saturation functions is introduced, and on this basis a second-order finite-time formation control protocol is developed.With the help of the homogeneous theory and Lasalle's invariance principle, it is theoretically proved that the designed formation protocol could complete the formation task in finite time, and the control inputs are shown to remain within their available actuating limits. Finally, simulations are performed to verify the effectiveness of the scheme. 展开更多
关键词 formation control multiple flight vehicle(MFV) FINITE-TIME actuator saturation
在线阅读 下载PDF
Consensus of multi-vehicle cooperative attack with stochastic multi-hop time-varying delay and actuator fault 被引量:2
18
作者 CAI Guangbin ZHAO Yushan +1 位作者 ZHAO Yang HU Changhua 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2021年第1期228-242,共15页
A consensus-distributed fault-tolerant(CDFT)control law is proposed for a class of leader-following multi-vehicle cooperative attack(MVCA)systems in this paper.In particular,the switching communication topologies,stoc... A consensus-distributed fault-tolerant(CDFT)control law is proposed for a class of leader-following multi-vehicle cooperative attack(MVCA)systems in this paper.In particular,the switching communication topologies,stochastic multi-hop timevarying delays,and actuator faults are considered,which may lead to system performance degradation or on certain occasions even cause system instability.Firstly,the estimator of actuator faults for the following vehicle is designed to identify the actuator faults under a fixed topology.Then the CDFT control protocol and trajectory following error are derived by the relevant content of Lyapunov stability theory,the graph theory,and the matrix theory.The CDFT control protocol is proposed in the same manner,where a more realistic scenario is considered,in which the maximum trajectory following error and information on the switching topologies during the cooperative attack are available.Finally,numerical simulation are carried out to indicate that the proposed distributed fault-tolerant(DFT)control law is effective. 展开更多
关键词 leader-following multi-vehicle cooperative attack(MVCA) switching topology fault-tolerant control stochastic multi-hop time-varying delay stochastic actuator fault
在线阅读 下载PDF
Structure design and characteristics analysis of a cylindrical giant magnetostrictive actuator for ball screw preload 被引量:1
19
作者 JU Xiao-jun LIN Ming-xing +2 位作者 FAN Wen-tao BU Qing-qiang WU Xiao-jian 《Journal of Central South University》 SCIE EI CAS CSCD 2018年第7期1799-1812,共14页
In order to achieve automatic adjustment of the double-nut ball screw preload, a magnetostrictive ball screw preload system is proposed. A new cylindrical giant magnetostrictive actuator (CGMA), which is the core co... In order to achieve automatic adjustment of the double-nut ball screw preload, a magnetostrictive ball screw preload system is proposed. A new cylindrical giant magnetostrictive actuator (CGMA), which is the core component of the preload system, is developed using giant magnetostrictive material (GMM) with a hole. The pretightening force of the CGMA is determined by testing. And the magnetic circuit analysis method is introduced to calculate magnetic field intensity of the actuator with a ball screw shaft. To suppress the thermal effects on the magnetostrictive outputs, an oil cooling method which can directly cool the heat source is adopted. A CGMA test platform is established and the static and dynamic output characteristics are respectively studied. The experimental results indicate that the CGMA has good linearity and no double-frequency effect under the bias magnetic field and the output accuracy of the CGMA is significantly improved with cooling measures. Although the output decreased with screw shaft through the actuator, the performance of CGMA meets the design requirements for ball screw preload with output displacement more than 26 μm and force up to 6200 N. The development of a CGMA will provide a new approach for automatic adjustment of double-nut ball screw preload. 展开更多
关键词 ball screw preload cylindrical giant magnetostrictive actuator (CGMA) structure design output characteristics
在线阅读 下载PDF
Actuator characterization of a man-portable precision maneuver concept 被引量:1
20
作者 Ilmars CELMINS Frank E.FRESCONI Bryant P.NELSON 《Defence Technology(防务技术)》 SCIE EI CAS 2014年第2期141-148,共8页
The US Army Research Laboratory is conducting research to explore technologies that may be suitable for maneuvering man-portable munitions.Current research is focused on the use of rotary actuators with spin-stabilize... The US Army Research Laboratory is conducting research to explore technologies that may be suitable for maneuvering man-portable munitions.Current research is focused on the use of rotary actuators with spin-stabilized munitions.A rotary actuator holds the potential of providing a low-power solution for guidance of a spinning projectile.This is in contrast to a linear(reciprocating) actuator which would need to constantly change direction,resulting in large accelerations which in turn would require large forces,thereby driving up the actuator power.A rotational actuator would be operating at a fairly constant rotation rate once it is up to speed,resulting in much lower power requirements.Actuator experiments conducted over a variety of conditions validate the dynamic models of the actuator and supply the data necessary for model parameter estimation.Actuator performance metrics of spin rate response,friction,and power requirements were derived from the data.This study indicates that this class of maneuver concepts can be driven with these actuators.These results enable actuator design and multidisciplinary simulation of refined maneuver concepts for a specific application. 展开更多
关键词 执行器 旋转速度 特性 男子 模型参数估计 致动器 低功率 驱动器
在线阅读 下载PDF
上一页 1 2 250 下一页 到第
使用帮助 返回顶部