PHY6426/Fall 2007: CLASSICAL MECHANICS HOMEWORK ASSIGNMENT #6 due by 9:35 a.m. Mon 10/8 Instructor: D. L. Maslov maslov@phys.ufl.edu 392-0513 Rm. 2114 Please help your instructor by doing your work neatly. 1. A sphere rolls without slipping along a horizontal surface. Using Eulerian angles and nonholonomic rolling constraint, show that the center of the sphere is moving along a straight line while the angular velocity remains constant in time. (Hint: use the projections of the angular velocity on the axes of the fixed system; see Goldstein, Derivation 14, p. 182.) Solution: Ω1,2,3 are the projections of the angular velocity on the axes of the fixed system. a) Let’s first solve the problem in a simple way, without using the non-holonomic constraints. Frictional force f acts in the plane. Equations of motion mẍ1 = f1 mẍ2 = f2 . This force also produces a torque about the c.o.m. of the sphere. The corresponding equations describing the dynamics of the angular momentum are N1 = f2 R = I Ω̇1 N2 = −f1 R = I Ω̇2 , N3 = 0. where I is the moment of inertia. Rolling constraint ẋ1 = RΩ2 → ẍ1 = RΩ̇2 ẋ2 = −RΩ1 → ẍ2 = −RΩ̇1 . Substituting expressions for ẍ1 into the equation of motion and using the equations for torque, we find that we have two results for f1 f1 = mẍ1 = mRΩ̇2 I f1 = − Ω̇2 → R I Ω̇2 = 0. mR + R As the coefficient in front of Ω̇2 is strictly positive, the last equations can be satisfied only if Ω̇2 = 0. Similarly, one shows that Ω̇1 = 0. Then, it follows that ẍ1 = ẍ2 = 0. The ratio of velocity components is obtained by dividing the first constraint equation by the second one Ω2 ẋ1 =− . ẋ2 Ω1 2 Thus, we see that the sphere rolls along a straight line whose tangent is determined by the ratio of the angular velocities tan θ = ẋ2 Ω1 =− . ẋ1 Ω2 2) In order to apply the technique of non-holonomic constraints, we write the constraint equation as α Fα = A α j q̇j = 0 and add Aα j = ∂Fα /∂ q̇α multiplied by the Lagrange factors µα to the right-hand side of the Euler equation ∂L d ∂L − = µ α Aα j. dt ∂ q̇j ∂qj The Lagrangian is 3 1 X 2 1 2 Ω , L = m (ṙ) + I 2 2 i=1 i where r is the position of the c.o.m. and Ωi are defined with respect to a stationary system (XY Z). Projecting the angular velocities on the axes of XY Z, we find Ω1 = θ̇ cos φ + ψ̇ sin θ sin φ Ω2 = θ̇ sin φ − ψ̇ sin θ cos φ Ω3 = φ̇ + ψ̇ cos θ. Substituting these expressions into Ω21 + Ω22 + Ω23 , we find Ω21 + Ω22 + Ω23 = θ̇2 + φ̇2 + ψ̇ 2 + 2φ̇ψ̇ cos θ. As before, the rolling constraint reads ẋ1 = Ω2 R ẋ2 = −Ω1 R or, using equations for Ω1 and Ω2 , ẋ1 =0 R ẋ2 = 0. = θ̇ cos φ + ψ̇ sin θ sin φ + R f1 = θ̇ sin φ − ψ̇ sin θ cos φ − f2 Equations of motion ∂L ∂F1 ∂F2 d ∂L − = µ1 + µ2 , dt ∂ q̇j ∂qj ∂ q̇j ∂ q̇j where j labels x1 , x2 , φ, ψ, and θ. Performing differentiations, we find mẍ1 = −µ1 /R mẍ2 d I φ̇ + ψ̇ cos θ dt d ψ̇ + φ̇ cos θ I dt I θ̈ + I φ̇ψ̇ sin θ = µ2 /R d = I Ω̇3 = 0 dt = sin θ (−µ1 cos φ + µ2 sin φ) = µ1 sin φ + µ2 cos φ 3 Note that Ω3 =const. Multiply the last equation by sin φ/ sin θ and the one before the last one by cos φ, and add them up. This gives a relation for µ2 sin φ cos θ sin φ + φ̈ − φ̈θ̈ sin φ . µ2 = I θ̈ cos φ + φ̇ψ̇ sin θ cos φ + ψ̈ sin θ sin θ Noticing that φ̈ + ψ̈ cos θ − ψ̇ θ̇ sin θ = 0, the expression for µ2 is reduced to i d h θ̇ cos φ + ψ̇ sin θ sin φ dt I d = I Ω1 = − ẍ2 dt R µ2 = I Thus, ẍ2 = −RΩ̇1 . On the other hand, mẍ2 = I µ2 = − ẍ2 . R R It follows then that ẍ2 = 0 Ω̇1 = 0. Similarly, ẍ1 = 0 Ω̇2 = 0. The conclusions are made in the same way as in the “simple” solution. 2. Goldstein, Problem 5.7 Choose the the principal axes so that I1 < I2 < I3 . Focus on the axis x1 first. The angular velocity is almost aligned with this axis, so that we can write ω = ω1 x̂1 + ε2 x̂2 + ε3 x̂3 , where projections ε2 and ε3 are small. The Euler equations for a torque-free motion I1 ω̇1 = ω2 ω3 (I2 − I3 ) I2 ω̇2 = ω1 ω3 (I3 − I1 ) I3 ω̇3 = ω1 ω2 (I1 − I2 ) become I1 ω̇1 = ε2 ε3 (I2 − I3 ) I2 ε̇2 = ω1 ε3 (I3 − I1 ) I3 ε̇3 = ω1 ε2 (I1 − I2 ) . To lowest order in ε2 and ε3 , the RHS of the first equation is equal to zero, which means that ω1 =const. Differentiating the second equation and using the third one gives ε̈2 = −Ω21 ε2 , 4 where Ω21 = ω12 (I3 − I1 ) (I2 − I1 ) I2 I3 Likewise, ε̈3 = −Ω21 ε3 The motion is stable if Ω21 > 0 which is the case because of the ordering of I’s. Thus rotation about the x1 axis is stable. Components of ω, transverse to this axis, rotate with the frequency s (I3 − I1 ) (I2 − I1 ) Ω1 = ω 1 . I2 I3 Results for other axes can be simply obtained by a cyclic permutation of indices 1, 2, 3. This gives Ω22 = ω22 (I1 − I2 ) (I3 − I2 ) . I1 I3 Ω22 < 0 because I1 < I2 , and thus rotation about the x2 axis is unstable. Finally, Ω23 = ω32 (I2 − I3 ) (I1 − I3 ) >0 I1 I3 and rotation about x3 is stable. 3. Goldtsein, Problem 4.23 Choose the frame as shown in the figure: the xy plane is tangent to the Earth surface, the z axis is along the radius. The pivoting point of the pendulum is on the z axis. Consider first the motion of the pendulum for stationary Earth. The pendulum swings in the plane normal to the xy plane. The motion in this plane is described by ẍ + ω02 x = 0 ÿ + ω0 y = 0, p where ω0 = g/l and l is the length of the pendulum. Earth’s rotation add extra terms to the RHS of these equations. For slow rotation, one can neglect the centrifugal force (proportional to Ω 2 ) and keep only the Coriolis force. Then the equations change to ẍ + ω02 x = 2 (v × Ω)x = 2ẏΩz ÿ + ω0 y = 2 (v × Ω)y = −2ẋΩz , where Ωz = Ω cos θ. Multiplying the second equation by i adding up the two equations, we obtain ζ̈ + 2iΩz ζ̇ + ω02 ζ = 0, where ζ = x + iy. A solution of the form ζ ∝ eiωt gives an equation for ω ω 2 + 2Ωz ω − ω02 = 0 or ω1,2 = −Ωz ± As Ωz ω0 , one can expand the last result as q ω02 + Ω2z . ω1,2 = −Ωz ± ω0 . 5 Ω z x θ y Hence the general solution for ζ is ζ = e−iΩz t Aeiω0 t + Be−iω0 t . For Ωz = 0, ζ = x0 (t) + iy0 (t), where x0 (t) and y0 (t) are trajectories for Ωz = 0. Therefore, ζ = x + iy = e−iΩz t (x0 + iy0 ) . Separating real and imaginary parts, we find x = x0 cos Ωz t + y0 sin Ωz t y = −x0 sin Ωz t + y0 cos Ωz t. The plane of the pendulum rotates about the z axis with angular frequency Ωz .