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標(biāo)題: Titlebook: Dynamics of Controlled Mechanical Systems; IUTAM/IFAC Symposium G. Schweitzer,M. Mansour Conference proceedings 1989 Springer-Verlag, Berli [打印本頁(yè)]

作者: 呻吟    時(shí)間: 2025-3-21 18:28
書(shū)目名稱Dynamics of Controlled Mechanical Systems影響因子(影響力)




書(shū)目名稱Dynamics of Controlled Mechanical Systems影響因子(影響力)學(xué)科排名




書(shū)目名稱Dynamics of Controlled Mechanical Systems網(wǎng)絡(luò)公開(kāi)度




書(shū)目名稱Dynamics of Controlled Mechanical Systems網(wǎng)絡(luò)公開(kāi)度學(xué)科排名




書(shū)目名稱Dynamics of Controlled Mechanical Systems被引頻次




書(shū)目名稱Dynamics of Controlled Mechanical Systems被引頻次學(xué)科排名




書(shū)目名稱Dynamics of Controlled Mechanical Systems年度引用




書(shū)目名稱Dynamics of Controlled Mechanical Systems年度引用學(xué)科排名




書(shū)目名稱Dynamics of Controlled Mechanical Systems讀者反饋




書(shū)目名稱Dynamics of Controlled Mechanical Systems讀者反饋學(xué)科排名





作者: menopause    時(shí)間: 2025-3-21 23:42
Historical Perspectives: Concepts,lectronic control devices cannot be modeled with adequate accuracy. Therefore, a combined dynamical simulation using a software model of the mechanical parts and a hardware design of the active elements is an economic strategy. However, the problem of the interfaces between hardware and software has to be solved.
作者: 柔美流暢    時(shí)間: 2025-3-22 01:17
to a finite degree of freedom system with the Galerkin method, and the control is determined by means of the optimal regulator theory. Numerical calculations are carried out for six degree of freedom system, and the effects of the location and length of the actuator are examined.
作者: homocysteine    時(shí)間: 2025-3-22 07:12
the computer responds with lines of text representing equations needed to continue the analysis. Ultimately, the equations of motion appear on the screen, and one additional command then leads to a FORTRAN simulation program.
作者: Invertebrate    時(shí)間: 2025-3-22 12:00
R. Süss,V. Kinzel,J. D. Scribnertual to graphical program representation, the way to compose programs by connecting available modules, and the target system independence. A program inherently specifies the most parallel execution but may also be run sequentially.
作者: ATOPY    時(shí)間: 2025-3-22 14:08
Computer Aided Formulation of Equations of Motionthe computer responds with lines of text representing equations needed to continue the analysis. Ultimately, the equations of motion appear on the screen, and one additional command then leads to a FORTRAN simulation program.
作者: ATOPY    時(shí)間: 2025-3-22 17:24

作者: 一瞥    時(shí)間: 2025-3-22 21:42

作者: 珠寶    時(shí)間: 2025-3-23 03:20
Modeling the Dynamics of a Complete Vehicle with Nonlinear Wheel Suspension Kinematics and Elastic Hoperations. The program is applied for extended simulation runs. It has to serve as a basis for the control design of anti-block-systems (ABS), drive-slide control systems (ASR) and active suspension systems.
作者: 眨眼    時(shí)間: 2025-3-23 05:40
State Equations of Motion for Flexible Bodies in Terms of Quasi-Coordinatesbsequently expressed in terms of quasi-coordinates representing rigid-body motions. Finally, the second-order Lagrange’s equations for hybrid systems are transformed into a set of state equations suitable for control. An illustrative example is presented.
作者: 煞費(fèi)苦心    時(shí)間: 2025-3-23 12:26
Structure of Magnetic Bearing Control System for Compensating Unbalance Forceriations of the controlled object but loses the property for a change of the rotational speed. The structure of a new controller is presented which holds the property even if the rotational speed is perturbed. The controller is obtained by modifying the original controller based upon a formula of Laplace transform.
作者: 遵循的規(guī)范    時(shí)間: 2025-3-23 17:48
Suzannah Harnor,James Pickles,Celine Canon to support the complete design and analysis cycle. The benefits of this concept are discussed and realizations at Dornier are introduced together with examples from recent applications and an outlook on further developments.
作者: Complement    時(shí)間: 2025-3-23 18:42
Wnt Signaling in Cartilage Development,ack gains, and the design is done in the frequency domain using the Loop Transfer Recovery method. The controller is shown to suppress the air resonance instability throughout wide range helicopter loading conditions and forward flight speeds.
作者: Obsessed    時(shí)間: 2025-3-24 02:11

作者: jabber    時(shí)間: 2025-3-24 04:56
A Simple Active Controller to Supress Helicopter Air Resonance in Hover and Forward Flightack gains, and the design is done in the frequency domain using the Loop Transfer Recovery method. The controller is shown to suppress the air resonance instability throughout wide range helicopter loading conditions and forward flight speeds.
作者: lattice    時(shí)間: 2025-3-24 10:16

作者: 解凍    時(shí)間: 2025-3-24 10:58

作者: 褲子    時(shí)間: 2025-3-24 18:39

作者: 可以任性    時(shí)間: 2025-3-24 22:44

作者: 勤勉    時(shí)間: 2025-3-25 01:54

作者: 強(qiáng)制令    時(shí)間: 2025-3-25 05:16

作者: dagger    時(shí)間: 2025-3-25 08:00
Laser Ablation-Deposited CN, Thin Films,le to use too few and too many). Preliminary attempts to solve this new research question are described. It is also shown that there exists optimal . of the actuators. NASA’s SCOLE example demonstrates the concepts.
作者: 步兵    時(shí)間: 2025-3-25 15:26
Conference proceedings 1989te of the art It intends to evalua~ the limits of performance that can be achieved by controlling the dynamics, and it should point to gaps in present research and areas for future research. Mainly, it has brought together leading experts from quite different areas presenting their points of view. T
作者: 燦爛    時(shí)間: 2025-3-25 16:24

作者: transplantation    時(shí)間: 2025-3-25 20:18
Fiber Connected Tug of War war. It is implemented in a miniature system, and checked the validity before the realization of a practical system. The miniature system worked as expected. The practical system is to be demonstrated at Aomori-Hakodate Exposition.
作者: 摻和    時(shí)間: 2025-3-26 01:58
Placing Dynamic Sensors and Actuators on Flexible Space Structuresle to use too few and too many). Preliminary attempts to solve this new research question are described. It is also shown that there exists optimal . of the actuators. NASA’s SCOLE example demonstrates the concepts.
作者: 殺子女者    時(shí)間: 2025-3-26 07:32
Model Verification by Experiments with Finite Effect Sequences (FES)nce of nonlinearities in the plant is studied and their influence on the test is reduced by a modification of the FES. Practical problems arising in the application to a robot arm are discussed and recommendations for further investigations are given.
作者: patriarch    時(shí)間: 2025-3-26 11:05

作者: hazard    時(shí)間: 2025-3-26 12:40

作者: 親密    時(shí)間: 2025-3-26 16:54

作者: 倔強(qiáng)一點(diǎn)    時(shí)間: 2025-3-27 00:12
Simulation, Test and Diagnostics Integrated for a Safety Design of Magnetic Bearing Prototypes complex mechatronic product, consisting of hardware and of software. These basic procedures form a selfcontained software package - the “safety development system” SDS - closely linked to the actual product. As an example we will apply this development system to the design of magnetic bearings.
作者: Countermand    時(shí)間: 2025-3-27 04:58

作者: 無(wú)彈性    時(shí)間: 2025-3-27 05:49
Towards Graphical Programming in Control of Mechanical Systemss, no side-effects, step-wise refinement. Each program part is represented in a data flow view and a control flow view. A Macintosh-style tool supports direct manipulation of the graphical representations, maintains consistency between the two complementary views, and automatically generates code. A
作者: Mendicant    時(shí)間: 2025-3-27 13:00

作者: Flagging    時(shí)間: 2025-3-27 15:34
Active Vibration Control of a Cantilever Beam by a Piezoelectric Ceramic Actuatorments) are induced by a pair of piezoelectric ceramic actuators partially bonded on the upper and lower side of the beam. The problem is first reduced to a finite degree of freedom system with the Galerkin method, and the control is determined by means of the optimal regulator theory. Numerical calc
作者: 河流    時(shí)間: 2025-3-27 19:15

作者: 整頓    時(shí)間: 2025-3-27 23:54
Structure of Magnetic Bearing Control System for Compensating Unbalance Force from their nominal values. The concept of designing the control system is that unbalance forces are estimated by an observer and cancelled by the electromagnetic forces of the bearing. It is shown theoretically that the original controller can suspend the rotor without whirling for the parameter va
作者: FEIGN    時(shí)間: 2025-3-28 04:05

作者: Valves    時(shí)間: 2025-3-28 10:17
A Simple Active Controller to Supress Helicopter Air Resonance in Hover and Forward Flightresented. This model is used to illustrate the effect of unsteady aerodynamics, forward flight, and torsional flexibility on air resonance. Next a nominal configuration, which experiences air resonance in forward flight, is selected. A simple multivariable compensator using conventional swashplate i
作者: 尾隨    時(shí)間: 2025-3-28 12:31

作者: 浪蕩子    時(shí)間: 2025-3-28 15:40
https://doi.org/10.1007/978-3-476-02743-6nce of nonlinearities in the plant is studied and their influence on the test is reduced by a modification of the FES. Practical problems arising in the application to a robot arm are discussed and recommendations for further investigations are given.
作者: 合法    時(shí)間: 2025-3-28 20:13
Roberta De Tullio,Monica Avernated analytically in minimum coordinates. In particular, the nonlinear constraint equations arising from the closed loops can be stated explicitly in recursive form. In addition, significant elasticities of the vehicle are considered..The corresponding simulation program requires a minimum number of
作者: Asparagus    時(shí)間: 2025-3-29 01:37
ch is a task that can be very laborious, especially if the device under consideration has a relatively large number of moving parts. This paper deals with a computer program intended to enable an analyst to formulate equations of motion with minimal labor. The name of the program is AUTOLEV..The pri
作者: 無(wú)能性    時(shí)間: 2025-3-29 03:49

作者: 撤退    時(shí)間: 2025-3-29 10:30

作者: atopic    時(shí)間: 2025-3-29 13:37

作者: Pelago    時(shí)間: 2025-3-29 17:11
R. Süss,V. Kinzel,J. D. Scribners, no side-effects, step-wise refinement. Each program part is represented in a data flow view and a control flow view. A Macintosh-style tool supports direct manipulation of the graphical representations, maintains consistency between the two complementary views, and automatically generates code. A
作者: 碌碌之人    時(shí)間: 2025-3-29 21:10
Suzannah Harnor,James Pickles,Celine Canollites with flexible appendages, docking spacecraft, space robots on orbiting platforms. Computer simulation is one of the chief means to support these goals. Two “traditional” classes of tools are characterized by their capabilities and limitations: nonlinear dynamic simulation software and 3D soli
作者: misshapen    時(shí)間: 2025-3-30 00:52
ments) are induced by a pair of piezoelectric ceramic actuators partially bonded on the upper and lower side of the beam. The problem is first reduced to a finite degree of freedom system with the Galerkin method, and the control is determined by means of the optimal regulator theory. Numerical calc
作者: colloquial    時(shí)間: 2025-3-30 04:38
https://doi.org/10.1007/978-3-658-37912-4 pulls the tug fixed on the center of rope to its side is the winner. The problem of this game is that all teams should be gathered at a same place. Therefore the game between Zurich and Munich was not possible. The objective of this research is to develop the system to make the game possible for te
作者: Psa617    時(shí)間: 2025-3-30 08:59
Max S. Pinheiro,José Roberto Moreira from their nominal values. The concept of designing the control system is that unbalance forces are estimated by an observer and cancelled by the electromagnetic forces of the bearing. It is shown theoretically that the original controller can suspend the rotor without whirling for the parameter va
作者: 安裝    時(shí)間: 2025-3-30 13:16





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