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TRIUMF DESIGN NOTE TRI-DN-07-13 May, 2007 Analytic Models for Quadrupole Fringe-Field Eﬀects Shane Koscielniak TRIUMF ABSTRACT We have introduced a method to construct the transfer matrix through a linear quadrupole fringe ﬁeld for the small class of analytic fringes that permit a closed-form double integral. Although this method is approximate, we have introduced a technique to regulate the errors in the equation of motion and determinant such that errors in position and divergence of the trajectory are comparable with or even below those arising from numerical integration. The method has been applied to the particularly simple case of a cosine-squared fall oﬀ and proven to be remarkably accurate. 4004 WESBROOK MALL, VANCOUVER, B.C., CANADA V6T 2A3 1 Introduction Let t be the longitudinal coordinate. Formulations of the motion in quadrupole fringe ﬁelds W (t) have a long history. Lee-Whiting[1], developed form factors (depending on the fringe shape) based on iterative solution of an integral equation, ignoring the Maxwellian terms due to W ≡ ∂W/∂t. In the same spirit of iterative approximation, Matsuda and Wollnik[2] introduced the aberrations from W and W . Here we shall concentrate upon particular fringe shapes that facilitate a high-order approximation that is superior to numerical integration. This property is achieved by insisting that both the error in the equation of motion is zero and the determinant of the transfer matrix is unity at the entry, exit and centre of the fringe ﬁeld. 2 Motion in quadrupole fringe ﬁeld When the pole face is perpendicular to the quadrupole symmetry axis, our ﬁrst order analysis of the quadrupole fringe ﬁeld shows that the forces acting are [Fx , Fy ] = B1 evs [−x, +y]W (z) . (1) Here W models the fringe ﬁeld fall oﬀ. In the case of an exit face, W (0) = 1 and W (L) = 0, where L is the fringe length. When the gradient (Tesla/m) B1 > 0, the quadrupole is horizontally focusing. Let K 2 = eB1 /(γvs m0 ) where e and γvs m0 are the particle charge and momentum, respectively. Let x and y be the particle divergences. The equations of motion are (d/dt)[x , y ] + K 2 W (t)[+x(t), −y(t)] = [0, 0] (2) Here t is synonymous with the longitudinal coordinate z. We shall now ﬁnd an almost exact solution for x, y by successive approximations. 3 1st Approximation ¯ ¯ The fringe may be written W (t) = W + Wac (t) where W is the average value, and Wac is an ¯ alternating part. The ﬁrst step is to replace W (s) by W leading to (d/dt)[x , y ] + k 2 [+x(t), −y(t)] = [0, 0] , (3) where k 2 = K 2 W . The equation has the well-known solution ¯ C(t) S(t) [x(t), x (t)] = T0 [x0 , x0 ] with T0 = . (4) C (t) S (t) Here C, S are the principal functions having the properties: C(0) = 1, S(0) = 0, C (0) = 0, S (0) = 1, CS − SC = 1 . (5) There is an analogous solution fo y, y . 1 4 2nd Approximation We now restore the alternating part of W (s) (d/dt)x + k 2 x(t) = −K 2 Wac (t)x(t) . (6) We shall treat this as if it were an inhomogeneous equation and solvable[3, 4] by the method of Green’s functions. First we note some properties of the Green’s function G(u, v). G(u, v) = S(u)C(v) − C(u)S(v) , G(u, u) = 0 . (7) d d G(u, v) = −S(v)C (u) , +C(v)S (u) G(u, v)|v=u = 1 . (8) du du For our particular horizontal equation, there is the property d2 C = −k 2 C , S = −k 2 S , G(u, v) = −k 2 G(u, v) . (9) du2 The solution is t x(t) = x0 C + x0 S − K 2 G(t, u)Wac (u)x(u)du (10) 0 t x (t) = x0 C + x0 S − K 2 G (t, u)Wac (u)x(u)du (11) 0 t x (t) = −k 2 (x0 C + x0 S) + K 2 k 2 G(t, u)Wac (u)x(u)du − Wac (t)x(t)] (12) 0 t = −K 2 W (t)x(t) + K 2 k 2 G(t, u)Wac (u)x(u)du . 0 This may also be written in a matrix form: [x, x ] = T[x0 , x0 ] with T = T0 + ΔT and t t 0 G(t, u)CWac du 0 G(t, u)SWac du ΔT = −K 2 t t . (13) 0 G (t, u)CWac du 0 G (t, u)SWac du Here we have eplicitly substituted the solution (4) into the right hand of (10, 11). 4.1 Errors Ideally the equation of motion (2) is identically zero. The departure from zero is a measure of how inaccurate is our approximate solution. We substitute (10, 11, 12) into the diﬀerential equation (2) and obtain the error t ε(t) = −K 4 Wac (t) G(t, u)Wac (u)x(u)du . (14) 0 The basic equation of motion is non-dissipative, and is therefore conservative. Thus, despite the varying coeﬃcient W (t), the determinant of the transfer matrix T must remain identically equal to unity, as may be conﬁrmed by pure numerical integration of the equations 2 of motion. We form the determinant of the matrix T = (T0 + ΔT). In order to simplify this determinant, we substitute for G(t, u) and G (t, u) from (7) and (8); giving cancellation of the K 2 terms, leading to t t Det[T] = 1 + K 4 G(t, u)C(u)Wac (u)du G (t, u)S(u)Wac(u)du (15) 0 0 t t − K4 G(t, u)S(u)Wac (u)du G (t, u)C(u)Wac(u)du. 0 0 We substitute again and ﬁnd t t t 2 Det[T] = 1 + K 4 C 2 Wac (u)du S 2 Wac (u)du − K 4 C(u)S(u)Wac (u)du . (16) 0 0 0 Clearly, the determinant deviates from unity. The next step shall be to modify the transfer matrix so as to regulate the error ε and the determinant. 5 3rd Approximation The matrix elements T11 , T12 relate to x(t), while elements T21 , T22 relate to x (t). Now T21 = T11 and T22 = T12 . The act of taking derivatives typically ampliﬁes the eﬀect of errors, and it is to be expected that the relative errors in x (t) are greater (by far) than those in x(t); and this is conﬁrmed by comparison with direct numerical integrations. Consequently, we take the matrix: t C − K2 G(t, u)CWac du S − K 2 0t G(t, u)SWac du 0 T= , (17) F21 (t) F22 (t) where the functions F21 , F22 are to be determined. We substitute [x, x ] = T[x0 , x0 ] into the equation of motion (2) and ﬁnd the error term: t ε = K 2 W (t)x(t) − K 4 W (t) G(t, u)Wac (u)x(u)du + [x0 F21 + x0 F22 ] , (18) 0 where x(t) = x0 C + x0 S. ε must be zero independent of the coeﬃcient x0 , x0 , leading to diﬀerential equations for F21 , F22 , with solution: t t v F21 (t) = F21 (0) − K 2 C W du + K 4 G[v, u]C[u]Wac (u)du W (v)dv (19) 0 0 0 t t v F22 (t) = F22 (0) − K 2 S W du + K 4 G[v, u]S[u]Wac (u)du W (v)dv . (20) 0 0 0 The constants F21 (0), F22 (0) are chosen to make the determinant equal unity at t = 0 and t = L. The determinant is t DetT = [C(t)F22 (t) − S(t)F21 (t)] − K 2 [C(u)F22 (t) − S(u)F21 (t)]G(t, u)Wac (u)du . (21) 0 At t = 0, the determinant is F22 (0) = 1. Hence F21 (0) is chosen to make DetT = 1 at t = L; the symbolic solution is too lengthy to record here. 3 6 Example of cos2(bt) fringe ﬁeld Evidently, the utility of this approach is limited by the need to ﬁnd closed form expressions for the double integrals; and this limits W (t) to simple functions. We shall study the case that W (t) = cos2 (bt) for an exit ﬁeld, with b = π/(2L) and b = k. This is more realistic than a linear decay, but still short of “ideal” because real fringe ﬁelds tend to have an initial rapid √ ¯ fall oﬀ, but a lingering tail. For this case W = 1/2, k = K/ 2 and Wac = (1/2) cos(2bt). 6.1 Horizontal motion For the horizontal motion C(t) = cos(kt) and S(t) = sin(kt)/k. The partial transfer matrix is ΔT = K2 sin bt[k cos bt sin kt − b sin bt cos kt] cos bt[b cos bt sin kt − k sin bt cos kt] 4b(b2 − k2 ) (−2b2 + k2 ) cos kt sin 2bt + bk cos2 bt sin kt (−2b2 + k2 ) sin kt sin 2bt + bk cos2 bt cos kt (22) The error (before introducing F21 , F22 ) is ε = K 4 cos 2bt x0 sin bt(−b cos kt sin bt + k cos bt sin kt) + (x0 /k) cos bt(−k cos kt sin bt + b cos bt sin kt) . 8b(b2 − k2 ) (23) The determinant (before introducing F21 , F22 ) is K4 (k 2 − 5b2 ) cos 4bt cos 2(b − k)t cos 2(b + k)t 1+ + + − . (24) 64(b2 − k 2 ) 2b2 (b2 − k 2 ) 2b2 k(b − k) k(b + k) 6.1.1 Corrected matrix elements The next step is to ﬁnd the matrix coeﬃcients F21 , F22 : 2 2 K2 F21 + K cos bt cos kt + sin bt(−b cos kt sin bt + k cos bt sin kt) = 0 , (25) 4b(b2 − k 2 ) K2 K2 F22 + cos2 bt sin kt + cos bt(−k cos kt sin bt + b cos bt sin kt) = 0 . (26) k 4b(b2 − k 2 ) The integrals can be performed in closed form, but are rather lengthy. 6.2 Vertical motion Analogously, for the vertical plane For the horizontal motion C(t) = cosh(kt) and S(t) = sinh(kt)/k. The driving term for the inhomogeneous equation is +K 2 Wac y(t). d2 /dt2 G(t, u) = +k 2 G(t, u). The top row of the partial transfer matrix is Δ[T11 , T12 ] = K2 2 sin bt[k cos bt sinh kt + b sin bt cosh kt], 2 cos bt[−b cos bt sinh kt + k sin bt cosh kt] . b(b2 + k2 ) (27) The lower row is Δ[T21 , T22 ] = Δ[T11 , T12 ]. 4 The error (before introducing F21 , F22 ) is ε = K 4 cos 2bt −y0 sin bt(b cosh kt sin bt + k cos bt sinh kt) + (y0 /k) cos bt(−k cosh kt sin bt + b cos bt sinh kt) . 8b(b2 + k2 ) (28) The determinant (before introducing F21 , F22 ) is K4 −(k 2 + 5b2 ) (b2 + k 2 ) cos 4bt 2 1+ + + (k cos 2bt cosh 2kt + b sin 2bt sinh 2kt) . 64(b2 + k 2 )2 2b2 2b2 k (29) 6.2.1 Corrected Matrix Elements The next step is to ﬁnd the matrix coeﬃcients F21 , F22 : K2 F21 − K 2 cos2 bt cosh kt + sin bt(b cosh kt sin bt + k cos bt sinh kt) = 0 , (30) 4b(b2 + k 2 ) K2 K2 F22 − cos2 bt sinh kt + cos bt(k cosh kt sin bt − b cos bt sinh kt) = 0 . (31) k 4b(b2 + k 2 ) The integrals can be performed in closed form, but are rather lengthy. 7 Numerical example For the cos2 (bt) fringe ﬁeld we now show a numerical example for the parameters k = π/3, b = 5π/3 and L = 3/10. We consider the particle trajectory with x0 = 0.2 and x0 = 20◦ . 7.1 Horizontal and vertical motion Figures 1,2 show our analytic trajectories superimposed on ones computed by direct numer- ical integration. At this level of resolution, no diﬀerence can be detected by eye; and so we resort to graphing the relative fractional errors (ﬁgures 3,5,7,9) in the approximate analytic trajectories compared with the “exact” values from numerical integration. 0.34 0.375 0.32 0.35 0.3 0.325 0.28 0.3 0.26 0.275 0.24 0.25 0.22 0.225 0.05 0.1 0.15 0.2 0.25 0.3 0.05 0.1 0.15 0.2 0.25 0.3 Figure 1: Trajectory x (red) and x (blue) Figure 2: Trajectory y (red) and y (blue) In a falling fringe ﬁeld, the particle divergences x , y tend toward constant values. 5 7.2 Errors in horizontal motion Here we compare numerical evaluation of our analytic expressions against direct numerical integration of the equations of motion for x, x . 7.2.1 Before correction 1.00004 0.05 0.1 0.15 0.2 0.25 0.3 1.00002 -0.00005 0.05 0.1 0.15 0.2 0.25 0.3 -0.0001 0.99998 -0.00015 0.99996 -0.0002 0.99994 -0.00025 0.99992 -0.0003 0.9999 Figure 3: Relative fractional error in x Figure 4: Determinants via numerical (red) and x (blue) (blue) and Green’s function (red) 7.2.2 After introducing F21 , F22 correction 1.00004 0.05 0.1 0.15 0.2 0.25 0.3 1.00003 -0.00001 1.00002 -0.00002 1.00001 -0.00003 0.05 0.1 0.15 0.2 0.25 0.3 0.99999 -0.00004 Figure 5: Relative fractional error in x Figure 6: Determinants via numerical (red) and x (blue) (blue) and Green’s function (red) From the ﬁgures 3-6 it is clear that there is an order of magnitude reduction in the errors after introducing the F21 , F22 matrix elements. Notice that the ordinate (vertical axis) has been expanded by a factor of 10 between ﬁgures 3 and 5 to better resolve the much reduced error in x . 7.3 Errors in vertical motion Here we compare numerical evaluation of our analytic expressions against direct numerical integration of the equations of motion for y, y . 6 7.3.1 Before correction 0.05 0.1 0.15 0.2 0.25 0.3 0.05 0.1 0.15 0.2 0.25 0.3 0.99998 -0.00005 0.99996 -0.0001 0.99994 -0.00015 0.99992 -0.0002 0.9999 Figure 7: Relative fractional error in y Figure 8: Determinants via numerical (red) and y (blue) (blue) and Green’s function (red) 7.3.2 After introducing F21 , F22 correction 0.05 0.1 0.15 0.2 0.25 0.3 0.05 0.1 0.15 0.2 0.25 0.3 0.999998 -6 -5·10 0.999996 -0.00001 0.999994 0.999992 -0.000015 0.99999 -0.00002 0.999988 -0.000025 0.999986 Figure 9: Relative fractional error in y Figure 10: Determinants via numerical (red) and y (blue) (blue) and Green’s function (red) From the ﬁgures 7-10 it is clear that there is an order of magnitude reduction in the errors after introducing the F21 , F22 matrix elements. Again, notice that the vertical scale has been expanded between ﬁgure 7 and 9. 8 Conclusion We have introduced a method to construct the transfer matrix through a linear quadrupole fringe ﬁeld for the small class of analytic fringes that permit a closed-form double integral. Although this method is approximate, we have introduced a technique to regulate the errors in the equation of motion and determinant such that errors in position and divergence of the trajectory are comparable with or even below those arising from numerical integration. The method has been applied to the particularly simple case of a cosine-squared fall oﬀ and proven to be remarkably accurate. 7 References [1] G.E. Lee-Whiting, Nucl. Instrum. Meth.-A, 76, 305 (1969). [2] H. Matsuda & H. Wollnik, Nucl. Instrum. Meth.-A, 103, 117 (1972). [3] Karl Brown, A First- and Second-Order Matrix Theory for Design of Beam Transport Systems and Charged Particle Spectrometers, SLAC Report-75, June 1982. [4] David Carey: The Optics of Charged Particle Beams, Volume 6 of the Accelerators and Storage Rings series; published by Harwood Academic Publishers, 1987. 8

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