Problem GPS 3.13 If the center of force is located at the origin of an
Transcription
Problem GPS 3.13 If the center of force is located at the origin of an
Goldstein Problem 3-6 Problem GPS 3.13 If the center of force is located at the origin of an x-y coordinate system, then the orbit is a circle that passes through the origin as, for example, drawn below. This circle has radius a, and its origin is at (a, 0). The equation that describes it is (x!a)2 + y2 = a2 . In terms of polar coordinates measured from the center of force, we have x = r cosθ and y = r sinθ . After substituting for x and y in the equation of the circle, we obtain the representation of the orbit in polar coordinates as r = 2a cosθ . Note that a full orbit is traversed as θ varies from !π/2 to π/2 instead of the usual 0 to 2π. Problem Goldstein 3-6 (a) Start with the differential equation of the orbit in terms of the variable u = 1/r, l2 2 u m µ ¶ 1 d2 u 2 + u = −f ( u ) , dθ (1) where l is the angular momentum, m is the mass of the particle, and u = (2a cos θ)−1 . (2) tan θ du = , dθ 2a cos θ (3) · ¸ 2 tan2 θ 1 d2 u 1 + = . 2a cos θ cos θ dθ2 (4) The required derivatives are and After we substitute Eqs.(2) and (4) into (1), we obtain l2 8a2 l2 5 l2 1 1 1 (1 + tan2 θ) = − u2 = − u . f( ) = − u2 u m a cos θ m a cos3 θ m (5) Thus, in terms of r, the force is k , r5 (6) 8a2 l2 . m (7) f(r) = − where the force constant k is k= (b) The potential corresponding to Eq.(6) is V (r) = − k . 4r4 (8) Thus, the total energy of this orbit is E= ·2 k m ·2 (r + r 2 θ ) − 4 . 2 4r (9) With r = 2a cos θ , 1 (10) we find · · r = −2aθ sin θ . (11) After substituting Eqs.(10) and (11) into Eq.(9), we find ·2 E = 2ma2 θ − k , 4r4 (12) but from the conservation of angular momentum we also know that · l = mr2 θ . (13) Thus, Eq.(12) simplifies to E= 1 4r4 µ 8a2 l2 −k m ¶ =0, (14) which is seen to equal zero after substituting for k using Eq.(7). (c) The period of the motion may be found from the conservation of angular momentum, Eq.(13), in the form · l dA r2 θ = = , 2 2m dt (15) where A is the area of the orbit, in this case, πa2 . Integrating Eq.(15) over a full period τ gives τl = πa2 , 2m (16) τ = 2πma2 /l . (17) and solving for τ gives (d) Start with the definitions of x and y in polar coordinates, to obtain · · · · · · x = r cos θ − rθ sin θ , (18) and y = r sin θ + rθ cos θ . · (19) · Then, substitute for r and θ, using Eqs.(11) and (13) to find · x=− l tan θ , ma 2 (20) and · y= l (1 − tan2 θ) . 2ma (21) We can find the speed either from ·2 ·2 v = (x + y )1/2 , (22) or, equivalently from ·2 ·2 · v = (r + r2 θ )1/2 = 2aθ. · (23) · · After substituting for x and y or for θ, we obtain v= l sec2 θ . 2ma (24) At the center of force θ equals either π/2 or −π/2, for which sec θ and tan θ are · · infinite. Thus, it is clear that x, y, and v are also infinite at this point. 3