Appendix W. Dynamic Models. W.2 4 Complex Mechanical Systems. Translational and Rotational Systems W.2.1

Similar documents
2002 Prentice Hall, Inc. Gene F. Franklin, J. David Powell, Abbas Emami-Naeini Feedback Control of Dynamic Systems, 4e

ECEN 420 LINEAR CONTROL SYSTEMS. Lecture 6 Mathematical Representation of Physical Systems II 1/67

Robotics I. Test November 29, 2013

Real-Time Implementation of a LQR-Based Controller for the Stabilization of a Double Inverted Pendulum

TOPIC E: OSCILLATIONS EXAMPLES SPRING Q1. Find general solutions for the following differential equations:

The basic principle to be used in mechanical systems to derive a mathematical model is Newton s law,

Moments and Torques. M = F d

Kinematics, Dynamics, and Vibrations FE Review Session. Dr. David Herrin March 27, 2012

End-of-Chapter Exercises

Tutorial 1 - Drive fundamentals and DC motor characteristics

Chapter 8 Rotational Motion and Dynamics Reading Notes

State Space Representation

PLANAR KINETICS OF A RIGID BODY FORCE AND ACCELERATION

N mg N Mg N Figure : Forces acting on particle m and inclined plane M. (b) The equations of motion are obtained by applying the momentum principles to

A-level Physics (7407/7408)

Examples of Applications of Potential Functions in Problem Solving (Web Appendix to the Paper)

Mechatronics. MANE 4490 Fall 2002 Assignment # 1

Plane Motion of Rigid Bodies: Forces and Accelerations

Rotational Equilibrium

= o + t = ot + ½ t 2 = o + 2

In-Class Problems 30-32: Moment of Inertia, Torque, and Pendulum: Solutions

AP Physics QUIZ Chapters 10

Chapter 14 Oscillations. Copyright 2009 Pearson Education, Inc.

Rotation. PHYS 101 Previous Exam Problems CHAPTER

DC Motor Position: System Modeling

A FORCE BALANCE TECHNIQUE FOR MEASUREMENT OF YOUNG'S MODULUS. 1 Introduction

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad

Rigid bodies - general theory

1. [30] Y&F a) Assuming a small angle displacement θ max < 0.1 rad, the period is very nearly

Your Name: PHYSICS 101 MIDTERM. Please circle your section 1 9 am Galbiati 2 10 am Kwon 3 11 am McDonald 4 12:30 pm McDonald 5 12:30 pm Kwon

Texas A & M University Department of Mechanical Engineering MEEN 364 Dynamic Systems and Controls Dr. Alexander G. Parlos

Problem Solving Session 11 Three Dimensional Rotation and Gyroscopes Solutions

Torque and Rotation Lecture 7

Chapter 4. Motion in Two Dimensions

Name (please print): UW ID# score last first

DYNAMICS MOMENT OF INERTIA

7.6 Journal Bearings

(a) On the dots below that represent the students, draw and label free-body diagrams showing the forces on Student A and on Student B.

Rotational Kinematics

θ + mgl θ = 0 or θ + ω 2 θ = 0 (2) ω 2 = I θ = mgl sinθ (1) + Ml 2 I = I CM mgl Kater s Pendulum The Compound Pendulum

CEE 271: Applied Mechanics II, Dynamics Lecture 9: Ch.13, Sec.4-5

Extra Circular Motion Questions

Chapter 14 Periodic Motion

9 Kinetics of 3D rigid bodies - rotating frames

(Refer Slide Time: 00:01:30 min)

Definition. is a measure of how much a force acting on an object causes that object to rotate, symbol is, (Greek letter tau)

AP Q1 Practice Questions Kinematics, Forces and Circular Motion

Chapter 10 Practice Test

is acting on a body of mass m = 3.0 kg and changes its velocity from an initial

Rotational Mechanics Part III Dynamics. Pre AP Physics

Physics Mechanics. Lecture 32 Oscillations II

Welcome back to Physics 211

Review: control, feedback, etc. Today s topic: state-space models of systems; linearization

Lecture Outline Chapter 10. Physics, 4 th Edition James S. Walker. Copyright 2010 Pearson Education, Inc.

Engineering Mechanics Prof. U. S. Dixit Department of Mechanical Engineering Indian Institute of Technology, Guwahati Introduction to vibration

A j = 0.1 cm 2 10 cm 10 cm 10 cm. W j Wj. W j W j. W j. 10 cm 10 cm 10 cm. r i

Chapter 4. Motion in Two Dimensions. Professor Wa el Salah

EE Homework 3 Due Date: 03 / 30 / Spring 2015

The University of Melbourne Engineering Mechanics

1. Replace the given system of forces acting on a body as shown in figure 1 by a single force and couple acting at the point A.

Chapter 5 Newton s Laws of Motion

Example: DC Motor Speed Modeling

Euler-Lagrange's equations in several variables

Mechatronics Modeling and Analysis of Dynamic Systems Case-Study Exercise

Dynamic Modeling of Rotary Double Inverted Pendulum Using Classical Mechanics

MEM04: Rotary Inverted Pendulum

11. (7 points: Choose up to 3 answers) What is the tension,!, in the string? a.! = 0.10 N b.! = 0.21 N c.! = 0.29 N d.! = N e.! = 0.

Two Dimensional Rotational Kinematics Challenge Problem Solutions

Physics 1A. Lecture 10B

(ii) no horizontal force acting (1) (hence) no (horizontal) acceleration (1) [or correct application of Newton s First law] 3

Physics 8 Friday, November 4, 2011

Measuring the Universal Gravitational Constant, G

ME 375 Final Examination Thursday, May 7, 2015 SOLUTION

Force, Mass, and Acceleration

Physics 12. Unit 5 Circular Motion and Gravitation Part 1

Study Guide. Physics 3104A. Science. Force, Motion and Energy. Adult Basic Education. Prerequisite: Physics 2104B or Physics 2204.

AP Physics Electromagnetic Wrap Up

MECH 3140 Final Project

2.003 Engineering Dynamics Problem Set 4 (Solutions)

A TLM model of a heavy gantry crane system

Rolling, Torque, Angular Momentum

CEE 271: Applied Mechanics II, Dynamics Lecture 24: Ch.17, Sec.1-3

Final Examination Thursday May Please initial the statement below to show that you have read it

Design and Comparison of Different Controllers to Stabilize a Rotary Inverted Pendulum

Modelling of Ball and Plate System Based on First Principle Model and Optimal Control

General Physics (PHYC 252) Exam 4

Exam 3 Practice Solutions

Lab Partner(s) TA Initials (on completion) EXPERIMENT 7: ANGULAR KINEMATICS AND TORQUE

Physics 41 HW Set 1 Chapter 15 Serway 8 th ( 7 th )

Robotics I. Figure 1: Initial placement of a rigid thin rod of length L in an absolute reference frame.

PLANAR KINETIC EQUATIONS OF MOTION: TRANSLATION

Chapter 9 TORQUE & Rotational Kinematics

Physics 101: Lecture 15 Torque, F=ma for rotation, and Equilibrium

Chapter 9 [ Edit ] Ladybugs on a Rotating Disk. v = ωr, where r is the distance between the object and the axis of rotation. Chapter 9. Part A.

Equilibrium of a Rigid Body. Engineering Mechanics: Statics

Projectile Motion. directions simultaneously. deal with is called projectile motion. ! An object may move in both the x and y

Rotational Kinetic Energy

Lezione 9 30 March. Scribes: Arianna Marangon, Matteo Vitturi, Riccardo Prota

EXPERIMENT 7: ANGULAR KINEMATICS AND TORQUE (V_3)

Rotation review packet. Name:

Transcription:

Appendix W Dynamic Models W.2 4 Complex Mechanical Systems W.2.1 Translational and Rotational Systems In some cases, mechanical systems contain both translational and rotational portions. The procedure is the same as that described in Section 2.1: sketch the free-body diagrams, de ne coordinates and positive directions, determine all forces and moments acting, and apply Eqs. (2.1) and/or (2.14). Example W.1 Rotational and Translational Motion: Hanging Crane Write the equations of motion for the hanging crane pictured in Fig. W.1 and shown schematically in Fig. W.2. Linearize the equations about = 0, which would typically be valid for the hanging crane. Also linearize the equations for =, which represents the situation for the inverted pendulum shown in Fig. W.3. SOLUTION A schematic diagram of the hanging crane is shown in Fig. W.2 while the free-body diagrams are shown in Fig. W.4. In the case of the pendulum, the forces are shown with bold lines, while the components of the inertial acceleration of its center of mass are shown with dashed lines. Because the pivot point of the pendulum is not xed with respect to an inertial reference, the rotation of the pendulum and the motion of its mass center must be considered. The inertial acceleration needs to be determined because the vector a in Eq. (2.1) is given with respect to an inertial reference. The inertial acceleration of the pendulum s mass center is the vector sum of the three dashed arrows shown in Fig. W.4(b). The derivation of the components of an object s acceleration is called kinematics and is usually studied as a prelude to the application of Newton s laws. The results of a kinematic study are shown in Fig. W.4(b). The component of acceleration along the pendulum is l _ 2 and is called the centripetal acceleration. It is present for any object whose velocity is changing direction. The x-component of acceleration is a consequence of the pendulum pivot point accelerating at the trolley s acceleration and will always have the same direction and magnitude as those of the trolley s. The l component is a result of angular acceleration of the pendulum and is always perpendicular to the pendulum. These results can be con rmed by expressing the center of mass of the pendulum as a vector from an inertial reference and then di erentiating that vector twice to obtain an inertial acceleration. Figure W.4(c) shows ^i and ^j axes which are inertially xed and a vector r describing the position of the pendulum center of mass. The vector can be expressed as r = x^i + l(^i sin ^j cos ): The rst derivative of r is _r = _x^i + l (^i _ cos + ^j sin ): Likewise, the second derivative of r is r = x^i + l (^i cos + ^j sin ) l _ 2 (^i sin ^j cos ): 1

2 APPENDIX W. DYNAMIC MODELS Figure W.1: Crane with a hanging load (Photo courtesy of Harnischfeger Corporation, Milwaukee, Wisconsin) Figure W.2: Schematic of the crane with hanging load

W.2. 4 COMPLEX MECHANICAL SYSTEMS 3 Figure W.3: Inverted pendulum Figure W.4: Hanging crane: (a) free-body diagram of the trolley; (b) free-body diagram of the pendulum; (c) position vector of the pendulum

4 APPENDIX W. DYNAMIC MODELS Note that the equation for r con rms the acceleration components shown in Fig.W.4(b). The l _ 2 term is aligned along the pendulum pointing toward the axis of rotation and the l term is aligned perpendicular to the pendulum pointing in the direction of a positive rotation. Having all the forces and accelerations for the two bodies, we now proceed to apply Eq. (2.1). In the case of the trolley, Fig.W.4(a), we see that it is constrained by the tracks to move only in the x-direction; therefore, application of Eq. (2.1) in this direction yields m t x + b _x = u N; (W.1) where N is an unknown reaction force applied by the pendulum. Conceptually, Eq. (2.1) can be applied to the pendulum of Fig. W.4(b) in the vertical and horizontal directions, and Eq. (2.14) can be applied for rotational motion to yield three equations in the three unknowns: N, P, and. These three equations can then be manipulated to eliminate the reaction forces N and P so that a single equation results describing the motion of the pendulum that is, a single equation in. For example, application of Eq. (2.1) for pendulum motion in the x-direction yields N = m p x + m p l cos m p l _ 2 sin : (W.2) However, considerable algebra will be avoided if Eq. (2.1) is applied perpendicular to the pendulum to yield P sin + N cos m p g sin = m p l + m p x cos : (W.3) Application of Eq. (2.14) for the rotational pendulum motion, for which the moments are summed about the center of mass, yields P l sin Nl cos = I ; (W.4) where I is the moment of inertia about the pendulum s mass center. The reaction forces N and P can now be eliminated by combining Eqs. (W.3) and (W.4). This yields the equation (I + m p l 2 ) + m p gl sin = m p lx cos : (W.5) It is identical to a pendulum equation of motion, except that it contains a forcing function that is proportional to the trolley s acceleration. An equation describing the trolley motion was found in Eq. (W.1), but it contains the unknown reaction force N. By combining Eqs. (W.2) and (W.1), N can be eliminated to yield (m t + m p )x + b _x + m p l cos m p l _ 2 sin = u: (W.6) Equations (W.5) and (W.6) are the nonlinear di erential equations that describe the motion of the crane with its hanging load. For an accurate calculation of the motion of the system, these nonlinear equations need to be solved. To linearize the equations for small motions about = 0, let cos = 1, sin =, and _ 2 = 0; thus the equations are approximated by (I + m p l 2 ) + m p gl = m p lx; (m t + m p )x + b _x + m p l = u: (W.7) Neglecting the friction term b leads to the transfer function from the control input u to hanging crane angle : (s) U(s) = m p l ((I + m p l 2 )(m t + m p ) m 2 pl 2 )s 2 + m p gl(m t + m p ) : (W.8) Inverted pendulum equations For the inverted pendulum in Fig. W.3, where =, assume = + 0, where 0 represents motion from the vertical upward direction. In this case, cos = 1, sin = 0 in Eqs. (W.5) and (W.6), and Eqs. (W.7) become 1

W.2. 4 COMPLEX MECHANICAL SYSTEMS 5 (I + m p l 2 ) 0 m p gl 0 = m p lx; (m t + m p )x + b _x m p l 0 = u: (W.9) As noted in Example 2.2, a stable system will always have the same signs on each variable, which is the case for the stable hanging crane modeled by Eqs. (W.7). However, the signs on and in the top Eq. (W.9) are opposite, thus indicating instability, which is the characteristic of the inverted pendulum. The transfer function, again without friction, is 0 (s) U(s) = m p l ((I + m p l 2 ) m 2 pl 2 )s 2 m p gl(m t + m p ) : (W.10) W.2.2 Problems for Complex Mechanical Systems 1. Assume the driving force on the hanging crane of Fig. W.2 is provided by a motor mounted on the cab with one of the support wheels connected directly to the motor s armature shaft. The motor constants are K e and K t, and the circuit driving the motor has a resistance R a and negligible inductance. The wheel has a radius r. Write the equations of motion relating the applied motor voltage to the cab position and load angle. Solution: The dynamics of the hanging crane are given by Eqs. (W.5) and (W.6), I + m p l 2 + mp gl sin = m p lx cos (m t + m p ) x + b _x + m p l cos m p l _ 2 sin = u where x is the position of the cab, is the angle of the load, and u is the applied force that will be produced by the motor. Our task here is to nd the force applied by the motor. Normally, the rotational dynamics of a motor is J 1 m + b 1 _ m = T m = K t i a where the current is found from the motor circuit, which reduces to R a i a = V a K e _ m for the case where the inductance is negligible. However, since the motor is geared directly to the cab, m and x are related kinematically by x = r m and we can neglect any extra inertia or damping from the motor itself compared to the inertia and damping of the large cab. Therefore we can rewrite the two motor equations in terms of the force applied by the motor on the cab u = T m =r = K t i a =r i a = (V a K e _ m )=R a where _ m = _x=r 1 The inverted pendulum is often described with the angle of the pendulum being positive for clockwise motion. If de ned that way, then reverse the sign on all terms in Eqs. (W.9) in 0 or 0.

6 APPENDIX W. DYNAMIC MODELS These equations, along with I + m p l 2 + mp gl sin = m p lx cos (m t + m p ) x + b _x + m p l cos m p l _ 2 sin = u constitute the required relations. 2. Assume the driving force on the hanging crane of Fig. W.2 is provided by a motor mounted on the cab with one of the support wheels connected directly to the motor s armature shaft. The motor constants are K e and K t, and the circuit driving the motor has a resistance R a and negligible inductance. The wheel has a radius r. Write the equations of motion relating the applied motor voltage to the cab position and load angle.