Non-linear Control for Underactuated Mechanical SystemsSpringer Science & Business Media, 2002 - 295 halaman 1 Introduction.- 1.1 Motivation.- 1.2 Outline of the book.- 1.2.1 Energy-based control approaches for several underactuated mechanical systems.- 1.2.2 The hovercraft model, the PVTOL aircraft and the helicopter.- 2 Theoretical preliminaries.- 2.1 Lyapunov stability.- 2.2 Lyapunov direct method.- 2.3 Passivity and dissipativity.- 2.4 Stabilization.- 2.5 Non-holonomic systems.- 2.6 Underactuated systems.- 2.7 Homoclinic orbit.- 3 The cart-pole system.- 3.1 Introduction.- 3.2 Model derivation.- 3.2.1 System model using Newton's second law.- 3.2.2 Euler-Lagrange's equations.- 3.3 Passivity of the inverted pendulum.- 3.4 Controllability of the linearized model.- 3.5 Stabilizing control law.- 3.5.1 The homoclinic orbit.- 3.5.2 Stabilization around the homoclinic orbit.- 3.5.3 Domain of attraction.- 3.3 Stability analysis.- 3.4 Simulation results.- 3.5 Experimental results.- 3.6 Conclusions.- 4 A convey-crane system.- 4.1 Introduction.- 4.2 Model.- 4.3 Passivity of the system.- 4.4 Damping oscillations control law.- 4.5 Asymptotic stability analysis.- 4.6 Simulation results.- 4.7 Concluding remarks.- 5 The pendubot system.- 5.1 Introduction.- 5.2 System dynamics.- 5.2.1 Equations of motion via Euler-Lagrange formulation.- 5.3 Passivity of the pendubot.- 5.4 Linearization of the system.- 5.5 Control law for the top position.- 5.5.1 The homoclinic orbit.- 5.5.2 Stabilization around the homoclinic orbit.- 5.6 Stability analysis.- 5.7 Simulation results.- 5.8 Experimental results.- 5.9 Conclusions.- 6 The Furuta pendulum.- 6.1 Introduction.- 6.2 Modeling of the system.- 6.2.1 Energy of the system.- 6.2.2 Euler-Lagrange dynamic equations.- 6.3.3 Passivity properties of the Furuta pendulum.- 6.3 Controllability of the linearized model.- 6.4 Stabilization algorithm.- 6.5 Stability analysis.- 6.6 Simulation results.- 6.7 Conclusions.- 7 The reaction wheel pendulum.- 7.1 Introduction.- 7.2 The reaction wheel pendulum.- 7.2.1 Equations of motion.- 7.2.2 Passivity properties of the system.- 7.2.3 Linearization of the system.- 7.2.4 Feedback linearization.- 7.3 First energy-based control design.- 7.4 Second energy-based controller.- 7.5 Simulation results.- 7.6 Conclusions.- 7.7 Generalization for Euler-Lagrange systems.- 8 The planar flexible-joint robot.- 8.1 Introduction.- 8.2 The two-link planar robot.- 8.2.1 Equations of motion.- 8.2.2 Linearization of the system.- 8.2.3 Passivity of the system.- 8.3 Control law for the two-link manipulator.- 8.3.1 Equivalent closed-loop interconnection.- 8.4 Stability analysis.- 8.5 Simulation results.- 8.6 The three-link planar robot.- 8.7 Control law for the three-link robot.- 8.8 Stability analysis.- 8.9 Simulation results.- 8.10 Conclusions.- 9 The PPR planar manipulator.- 9.1 Introduction.- 9.2 System dynamics.- 9.2.1 Equations of motion via Euler-Lagrange formulation.- 9.2.2 Passivity properties of the planar PPR manipulator.- 9.3 Energy-based stabilizing control law.- 9.3.1 Equivalent closed-loop interconnection.- 9.4 Convergence and stability analysis.- 9.5 Simulation results.- 9.6 Conclusions.- 10 The ball and beam acting on the ball.- 10.1 Introduction.- 10.2 Dynamical model.- 10.2.1 Mechanical properties.- 10.3 The control law.- 10.3.1 Stability analysis.- 10.4 Simulation results.- 10.5 Conclusions.- 11 The hovercraft model.- 11.1 Introduction.- 11.2 The hovercraft model.- 11.2.1 System model using Newton's second law.- 11.2.2 Euler-Lagrange's equations.- 11.2.3 Controllability of the linearized system.- 11.3 Stabilizing control law for the velocity.- 11.4 Stabilization of the position>.- 11.4.1 First approach.- 11.4.2 Second approach.- 11.4.3 Third approach.- 11.5 Simulation results.- 11.6 Conclusions.- 12 The PVTOL aircraft.- 12.1 Introduction.- 12.2 The PVTOL aircraft model.- 12.3 Input-output linearization of the system.- 12.4 Second stabilization approach.- 12.5 Third stabilization algorithm.- 12.6 Forwarding control law.- 12.6.1 First step: a Lyapunov function for the altitudeangle (y, ... |
Isi
I | 1 |
II | 7 |
IV | 8 |
V | 11 |
VI | 12 |
VII | 14 |
VIII | 15 |
IX | 17 |
LXX | 122 |
LXXI | 123 |
LXXII | 125 |
LXXIV | 129 |
LXXV | 130 |
LXXVI | 132 |
LXXVII | 135 |
LXXIX | 136 |
X | 18 |
XI | 19 |
XII | 21 |
XIII | 23 |
XIV | 24 |
XV | 25 |
XVI | 27 |
XVII | 28 |
XVIII | 29 |
XIX | 32 |
XXI | 37 |
XXII | 38 |
XXIII | 40 |
XXIV | 43 |
XXV | 45 |
XXVI | 46 |
XXVII | 47 |
XXVIII | 48 |
XXIX | 51 |
XXX | 53 |
XXXI | 54 |
XXXII | 55 |
XXXIII | 58 |
XXXIV | 59 |
XXXV | 60 |
XXXVI | 61 |
XXXVII | 64 |
XXXVIII | 67 |
XXXIX | 68 |
XL | 71 |
XLI | 73 |
XLII | 74 |
XLIII | 75 |
XLIV | 76 |
XLV | 78 |
XLVII | 80 |
XLVIII | 83 |
XLIX | 86 |
LI | 89 |
LII | 90 |
LIII | 92 |
LIV | 93 |
LV | 94 |
LVI | 95 |
LVII | 97 |
LVIII | 100 |
LIX | 104 |
LXI | 107 |
LXII | 108 |
LXIII | 110 |
LXIV | 111 |
LXV | 112 |
LXVII | 113 |
LXVIII | 117 |
LXIX | 120 |
LXXX | 138 |
LXXXI | 139 |
LXXXII | 142 |
LXXXIII | 143 |
LXXXIV | 144 |
LXXXV | 146 |
LXXXVI | 147 |
LXXXVIII | 150 |
LXXXIX | 151 |
XC | 155 |
XCI | 157 |
XCIII | 159 |
XCIV | 161 |
XCV | 162 |
XCVI | 163 |
XCVIII | 165 |
XCIX | 166 |
C | 167 |
CI | 171 |
CII | 173 |
CIII | 174 |
CIV | 176 |
CV | 177 |
CVI | 178 |
CVII | 179 |
CVIII | 180 |
CIX | 184 |
CX | 188 |
CXII | 193 |
CXIV | 194 |
CXV | 195 |
CXVI | 203 |
CXVII | 206 |
CXVIII | 207 |
CXIX | 213 |
CXX | 214 |
CXXII | 215 |
CXXIII | 217 |
CXXIV | 218 |
CXXV | 223 |
CXXVIII | 225 |
CXXIX | 235 |
CXXX | 242 |
CXXXI | 252 |
CXXXII | 253 |
CXXXV | 255 |
CXXXVI | 258 |
CXXXVII | 261 |
CXXXVIII | 270 |
CXXXIX | 272 |
CXL | 276 |
CXLI | 279 |
CXLII | 291 |
Edisi yang lain - Lihat semua
Non-linear Control for Underactuated Mechanical Systems Isabelle Fantoni,Rogelio Lozano Pratinjau terbatas - 2012 |
Non-Linear Control for Underactuated Mechanical Systems Isabelle Fantoni,Rogelio Lozano Pratinjau tidak tersedia - 2001 |
Non-linear Control for Underactuated Mechanical Systems Isabelle Fantoni,Rogelio Lozano Pratinjau tidak tersedia - 2012 |
Istilah dan frasa umum
actuated aerodynamic airframe angle angular velocity approach asymptotically stable backstepping ball and beam center of mass Chapter closed-loop system considered control design control inputs control strategy converge to zero coordinates cos˛ defined derivative det(D det(D(q Differentiating equations of motion equilibrium point error dynamics feedback feedback linearization Figure follows Furuta given homoclinic orbit hovercraft IEEE initial conditions inverted pendulum k₁ kinetic energy Lagrangian largest invariant set LaSalle's invariance Lozano Lyapunov function Lyapunov function candidate manipulator model helicopter non-linear non-linear control Nonlinear Control Note obtain parameters passivity properties pendubot perturbation planar positive definite potential energy presented proposed control law PVTOL aircraft q₁ rad/s robot rotation rotor blades Section Simulation results sin˛ small body forces stability analysis stable equilibrium point T₁ tail rotor torque total energy tracking trajectory u₁ underactuated unstable equilibrium V₁ vector θο
