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Central Forces Two-Body System Center of mass R Equal external force on both bodies. F2int m2 Add to get the CM motion ext ext MR F1 F2 Subtract for relative motion int int r r F1 F2 1 2 m1 m2 r = r1 – r2 F2ext r2 int ext m1r1 F1 F1 int ext m2 r2 F2 F2 m1 R F1int r1 F1ext Reduced Mass Internal forces are equal and opposite. int int r r F F ( 1 1 ) F int 1 2 m1 m2 m1 m2 Express in terms of a reduced mass m. int r r ( m1 m2 ) F int F 1 2 m1m2 m • • m less than either m1, m2 m approximately equals the smaller mass when the other is large. m m1m2 m2 for m1 m2 m1 m2 Central Motion Central motion takes place in a plane. • Force, velocity, and radius are coplanar. Orbital angular momentum is constant. J r p r mr dJ r mr r mr 0 dt Use J to avoid confusion with Lagrangian L If the central force is time-independent, the orbit is symmetrical about an apse. • Apse is where velocity is perpendicular to radius Central Force Equations Use spherical coordinates. • Makes r obvious from central force. • Generalized forces Qq = Qf = 0. • Central force need not be from a potential. Kinetic energy expression T 12 m (r 2 r 2q 2 r 2 sin 2 qf 2 ) d T T Qr dt r r d T T 0 dt q q d T T 0 dt f f Coordinate Reduction T doesn’t depend on f directly. Constant angular momentum about the polar axis. • Constrain the motion to a plane • Include the polar axis in the plane Two coordinates r, q. d T T 0 dt f f d T 0 dt f T 2 2 constant m r sin q f f T 12 m (r 2 r 2q 2 ) Angle Equation T doesn’t depend on q directly. Also represents constant angular momentum. • A constant of the motion Change the time derivative to an angle derivative. d T T 0 dt q q d T 0 dt q T 2 m r qJ q constant d dq d J d 2 dt dt dq mr dq Orbit Equation d T T Qr dt r r J d T T Qr 2 mr dq r r J d [ 12 m (r 2 r 2q 2 )] [ 12 m (r 2 r 2q 2 )] Qr 2 mr dq r r J dr J 2 J d J dr J2 mr ( 2 ) 2 ( 2 ) 3 Qr 2 r dq mr r dq mr dq mr 1 d 1 dr 1 mQr ( ) 2 2 2 3 r dq r dq r J Let u = 1/r d 2u mQr u dq 2 J 2u 2 Central Potential Central force can derive from a potential. d T T V Qr dt r r r Rewrite as differential equation with angular momentum. J 2 V mr 3 0 mr r Equivalent Lagrangian 2 J L 12 mr V 2 2mr 2 next