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lec15_ODE2

# lec15_ODE2 -         LeapFrog and Verlet method for...

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Unformatted text preview:         LeapFrog and Verlet method for ODEs Example: Simple Pendulum ODE of vectors Example: Projectile motion with air drag       HW#6 due today Get HW#6 off website Reading for Differential Equations in Appendix B.     Consider general ODE with initial condition: We are interested in a solution from t=0 to t=T in n time steps: du = f (u(t)) and u(0) = u0 dt T ∆t = n     Notation for solution at time step k: Using foward difference, ODE becomes Finally solution for time k+1 is uk+1 − uk = f (uk ) ∆t uk+1 = uk + ∆tf (uk ) uk ≡ u(tk )     Need value of u at k=0 time step to get this started (initial condition).   In many systems, the rate at which a quantity changes depends linearly on the value of that quantity. du (chemical reactions, nuclear fission, = −bu dt heat transfer,…) Initial condition (t=0):   u(0) = A   Solution is an exponential: u(t) = Ae −bt     Euler is based on forward difference approximation with error of order τ 2 . Big problem is it is NOT energy conserving. Using center difference method, we get the leap-frog method:       Error is of order τ 3 , and it IS energy conserving. However it is not self starting (need k=-1 step at start). One solution is to take an initial Euler step, then go with LeapFrog after the first step is computed. Why “leap-frog”? Let’s apply to a standard mechanics problem… uk+1 = uk−1 + 2τ f (uk )   By Newton’s laws and basic mechanics force (F), acceleration (a) velocity (v), position (r): F = ma   dv = a(r(t)) dt dr = v (t) dt Apply Leap-Frog method to solve for position and velocity at time step k based on previous values: vk+1 = vk−1 + 2τ a(rk ) rk+2 = rk + 2τ vk+1   Note how v and r values leap-frog each other.   Here we use the central difference formulas for BOTH the first derivative (v) AND second derivative (r). 2 dr dr = a(r) 2 dt dt = v (t) rk+1 − rk−1   So scheme becomes: v k= 2τ rk+1 = 2rk − rk−1 + τ 2 ak     Error for v is of order τ 2 and error for r is of order Calculation of v is not required to compute r. τ 4     Physics – velocity becomes angular velocity and position becomes angular position. Equations of motion are: dφ =ω dt dω g = α(φ) = − sin φ dt l   Or numerically using Verlet (just interested in position) φk+1 = 2φk − φk−1 + τ αk 2 Euler Verlet     Often in science the quantities we are interested in are vectors which require a magnitude and direction. Typically we express a vector by it’s individual components: ￿ = (vx , vy , vz ) v   Computationally, our 1D problems now become 3 1-D problems. We just perform the calculations on each of the components individually.     dvx 1 = Fdx (vx ) dt m dvy 1 = Fdy (vy ) − g dt m Restrict to 2-D, so only need x and y components of r and v. Force of gravity is only in y direction, drag force is always opposite to velocity (x and y components constantly change). drx = vx dt dry = vy dt 1 ￿ Fd = − Cd ρA|￿ |￿ vv 2 ...
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