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標(biāo)題: Titlebook: Non-linear Control for Underactuated Mechanical Systems; Isabelle Fantoni,Rogelio Lozano Book 2002 Springer-Verlag London 2002 Control.Con [打印本頁(yè)]

作者: charity    時(shí)間: 2025-3-21 18:13
書目名稱Non-linear Control for Underactuated Mechanical Systems影響因子(影響力)




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書目名稱Non-linear Control for Underactuated Mechanical Systems年度引用學(xué)科排名




書目名稱Non-linear Control for Underactuated Mechanical Systems讀者反饋




書目名稱Non-linear Control for Underactuated Mechanical Systems讀者反饋學(xué)科排名





作者: LVAD360    時(shí)間: 2025-3-21 20:34
Introduction,. The development of robots having an autonomous and complex behavior such as the adaptation to environment changes and uncertainties, planification and execution strategies without human intervention and the learning ability to improve performances is one of the ultimate goals in research of roboti
作者: Relinquish    時(shí)間: 2025-3-22 01:11
Theoretical preliminaries,important theorems based on Lyapunov theory. We will give some notions and basic concepts of passivity. Then, we will recall a necessary condition for the existence of a continuously stabilizing control law for non-linear systems, often referred to as Brockett’s necessary condition. The definitions
作者: Substitution    時(shí)間: 2025-3-22 05:15
The Furuta pendulum,nstructions. As we have seen in Chapter 3, the structure of the conventional inverted pendulum is the rail-cart type, which consists of a cart running on a rail and a pendulum attached to the cart. The inverted pendulum of this type has the movement limitation of its cart as a restriction of the con
作者: 口訣    時(shí)間: 2025-3-22 10:04

作者: Fallibility    時(shí)間: 2025-3-22 16:42

作者: 雄偉    時(shí)間: 2025-3-22 19:45

作者: Trochlea    時(shí)間: 2025-3-23 01:08

作者: BATE    時(shí)間: 2025-3-23 05:22
The PVTOL aircraft,f an aircraft, taking into account aeroelastic effects, flexibility of the wings, internal dynamics of the engine and the multitude of changing variables, are quite complex and somewhat unmanageable for the purposes of control. It is also particularly interesting to consider a simplified aircraft, w
作者: Bricklayer    時(shí)間: 2025-3-23 08:33
Helicopter on a platform,ral model (7-DOF) to be used on the autonomous forward flight of helicopters. We present the basic idea of the 7-DOF modelling. However, in this chapter, we focus on the particular case of a reduced order model (3-DOF) representing the scale model helicopter mounted on an experimental platform. We n
作者: 有偏見    時(shí)間: 2025-3-23 11:11

作者: subordinate    時(shí)間: 2025-3-23 17:26

作者: 使出神    時(shí)間: 2025-3-23 19:02
Isabelle Fantoni,Rogelio LozanoWill help the reader to gain experience in the modelling of mechanical systems and familiarise with new control methods for non-linear systems.Deals with the application of modern control theory to so
作者: Nuance    時(shí)間: 2025-3-23 22:32
978-1-4471-1086-6Springer-Verlag London 2002
作者: 大約冬季    時(shí)間: 2025-3-24 04:30

作者: TRUST    時(shí)間: 2025-3-24 06:57

作者: 希望    時(shí)間: 2025-3-24 13:05
The cart-pole system,The inverted pendulum is one of the most popular laboratory experiments used for illustrating non-linear control techniques. This system is motivated by applications such as the control of rockets and the antiseismic control of buildings.
作者: OREX    時(shí)間: 2025-3-24 18:16
A convey-crane system,Based on the results of control of the inverted pendulum on a cart presented in Chapter 3, we propose a control law of a convey-crane, which transports a load suspended from a cart minimizing the oscillations of the load. The technique has also been presented in [18].
作者: 小畫像    時(shí)間: 2025-3-24 22:59
The pendubot system,The two-link underactuated robotic mechanism called the pendubot is used for research in non-linear control and for education in various concepts like non-linear dynamics, robotics and control system design.
作者: Decimate    時(shí)間: 2025-3-25 01:48

作者: 事與愿違    時(shí)間: 2025-3-25 07:11
Communications and Control Engineeringhttp://image.papertrans.cn/n/image/667116.jpg
作者: licence    時(shí)間: 2025-3-25 07:29
https://doi.org/10.1007/978-1-4471-0177-2Control; Control Engineering; Control Theory; Energy-based Control; Lyapunov Theory; Mechanical Systems; N
作者: contradict    時(shí)間: 2025-3-25 12:03
The planar flexible-joint robot,since the pendulum and the pendubot move in a vertical plane. On the other hand, a pendulum or a pendubot moving in a horizontal plane has no potential energy. No gravitational forces are applied on the system.
作者: prostatitis    時(shí)間: 2025-3-25 19:45

作者: 業(yè)余愛好者    時(shí)間: 2025-3-25 20:05

作者: 門窗的側(cè)柱    時(shí)間: 2025-3-26 04:12

作者: UTTER    時(shí)間: 2025-3-26 07:56
The ball and beam acting on the ball,1 is motivated by the control of small rotational oscillations of platforms and vehicle suspensions. For simplicity, we assume that the center of the beam is connected to the pivot using a rotational spring and we neglect friction.
作者: 卜聞    時(shí)間: 2025-3-26 12:15
Helicopter on a platform,er, we focus on the particular case of a reduced order model (3-DOF) representing the scale model helicopter mounted on an experimental platform. We note that both cases represent underactuated systems (υ € . for the 7-DOF model and υ € . for the 3-DOF model studied in this chapter).
作者: faucet    時(shí)間: 2025-3-26 13:37

作者: Gossamer    時(shí)間: 2025-3-26 19:52

作者: Intuitive    時(shí)間: 2025-3-26 22:36

作者: 精密    時(shí)間: 2025-3-27 04:29
The PVTOL aircraft,hich has a minimum number of states and inputs but retains the main features that must be considered when designing control laws for a real aircraft. Therefore, as considered by Hauser et al. [35], we focus our study on the planar vertical take-off and landing (PVTOL) aircraft, which is a highly manoeuvrable jet aircraft.
作者: inchoate    時(shí)間: 2025-3-27 09:09

作者: aneurysm    時(shí)間: 2025-3-27 13:31
Non-linear Control for Underactuated Mechanical Systems
作者: Tartar    時(shí)間: 2025-3-27 15:25

作者: 碌碌之人    時(shí)間: 2025-3-27 18:11
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