Titlebook: Non-linear Control for Underactuated Mechanical Systems; Isabelle Fantoni,Rogelio Lozano Book 2002 Springer-Verlag London 2002 Control.Con

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书目名称Non-linear Control for Underactuated Mechanical Systems影响因子(影响力)




书目名称Non-linear Control for Underactuated Mechanical Systems影响因子(影响力)学科排名




书目名称Non-linear Control for Underactuated Mechanical Systems网络公开度




书目名称Non-linear Control for Underactuated Mechanical Systems网络公开度学科排名




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书目名称Non-linear Control for Underactuated Mechanical Systems被引频次学科排名




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LVAD360

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

Relinquish

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

Substitution

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

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Fallibility

雄伟

Trochlea

BATE

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

Bricklayer

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