Effective Potential for a Symmetric Rigid Body: Circular Orbits and Stability, Quizzes of Physics

The solution to a quiz question about the effective potential for a symmetric rigid body under the influence of gravity. The document derives expressions for the canonical momenta, energy, and angular velocities, and discusses the conditions for circular orbits and their stability. Useful for students studying classical mechanics, rigid body dynamics, and potential energy.

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Pre 2010

Uploaded on 08/30/2009

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PHY6938-01: The Road to the Comps
Classical Mechanics Quiz
Solution prepared by: Jorge Piekarewicz
September 22, 1999
(a) Given the components of the angular velocity of the rigid body along the body axes,
the Lagrangian for a symmetric rigid body under the influence of gravity becomes:
L=I
2(˙
θ2+˙
φ2sin2θ) + Iz
2(˙
φcos θ+˙
ψ)2M gl cos θ . (1)
(b) Since the Lagrangian is independent of φ,ψ, and t, namely,
∂L
∂φ =L
∂ψ =L
∂t = 0 ,
the canonical momenta conjugate to φand ψ as well as the total energy of the
system are constants of the motion:
pψ=∂L
˙
ψ=Iz(˙
φcos θ+˙
ψ) = IzωzIa , (2)
pφ=∂L
˙
φ=I˙
φsin2θ+Iz(˙
φcos θ+˙
ψ) cos θIb , (3)
E=I
2(˙
θ2+˙
φ2sin2θ) + Iz
2(˙
φcos θ+˙
ψ)2+Mgl cos θ . (4)
(c) To write an expression for ˙
φand ˙
ψin terms of θone can use Eqs. (2) and (3) to obtain:
˙
φ=bacos θ
sin2θ,˙
ψ=Ia
Iz
(bacos θ) cos θ
sin2θ.(5)
(d) The above expressions may now be inserted into the energy equation which becomes
E0E1
2Izω2
z= constant = 1
2I˙
θ2+Veff (θ),(6)
pf3

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PHY6938-01: The Road to the Comps

Classical Mechanics – Quiz

Solution prepared by: Jorge Piekarewicz

September 22, 1999

(a) Given the components of the angular velocity of the rigid body along the body axes,

the Lagrangian for a symmetric rigid body under the influence of gravity becomes:

L =

I

θ

2

φ

2

sin

2

θ) +

I

z

φ cos θ +

ψ)

2

− M gl cos θ. (1)

(b) Since the Lagrangian is independent of φ, ψ, and t, namely,

∂L

∂φ

∂L

∂ψ

∂L

∂t

the canonical momenta conjugate to φ and ψ — as well as the total energy of the

system — are constants of the motion:

p ψ

∂L

ψ

= I

z

φ cos θ +

ψ) = I z

ω z

≡ Ia , (2)

p φ

∂L

φ

= I

φ sin

2

θ + I z

φ cos θ +

ψ) cos θ ≡ Ib , (3)

E =

I

θ

2

φ

2

sin

2

θ) +

I

z

φ cos θ +

ψ)

2

  • M gl cos θ. (4)

(c) To write an expression for

φ and

ψ in terms of θ one can use Eqs. (2) and (3) to obtain:

φ =

b − a cos θ

sin

2 θ

ψ =

Ia

I

z

(b − a cos θ) cos θ

sin

2 θ

(d) The above expressions may now be inserted into the energy equation which becomes

E

≡ E −

I

z

ω

2

z

= constant =

I

θ

2

  • V eff

(θ) , (6)

where we have introduced the “effective” potential through the definition:

Veff (θ) = M gl cos θ +

I

(b − a cos θ)

2

sin

2

θ

(e) For the particular case of a = b we can write the effective potential in terms of x ≡

cos

2 (θ/2) as:

V

eff

(x) = 2M glx +

Ia

2

(

1 − x

x

)

− M gl , (8)

Clearly, the effective potential supports circular orbits, namely, a solution to the equa-

tions of motion of the form θ(t) = θ 0

= constant. This solution is obtained by de-

manding:

V

eff

(x) = 2M gl −

Ia

2

2 x

2

= 0 , or x 0

= cos

2

(θ 0

Ia

2

4 M gl

Note that under these conditions (a = b) a real solution exists only for:

Ia

2

4 M gl

Moreover, by inspecting the effective potential one concludes that the circular orbit

is stable, V

′′

eff

(x 0

) = Ia

2 /x

3

0

0, so that the frequency of small oscillations may be

extracted from the energy equation [ξ ≡ (θ − θ 0 )]:

E

′′

≡ E

− V eff

(θ 0

I

ξ

2

V

′′

eff

(θ 0

2

+... , so that (11)

ω s.o.

V

′′

eff

(θ 0

)/I. (12)