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Do the Jovian Bow Shock and Magnetopause Surfaces in the Joy et al. [2002] Model Predict Measured Boundary Normals Correctly? S. P. Joy 1,2 , W. S. Kurth 3 , M. G. Kivelson 1,2 , R. J. Walker 1,2 1) Institute of Geophysics and Planetary Physics – University of California at Los Angeles 2) Dept. of Earth and Space Science – University of California at Los Angeles 3) Dept. of Physics and Astronomy – University of Iowa Joy et al. [2002] provided probabalistic descriptions of the jovian bow shock and magnetopause locations by mapping spacecraft observations to the sub-solar point along model surfaces derived from the MHD simulation of Ogino et al. [1998]. The resulting statistics are strongly affected by the surface models used in the mapping process. Here we analyze the quality of the surface models used in that mapping by comparing the normal directions of the observed boundary crossings to the normal directions predicted by the model surfaces. We have identified 116 magnetopause and 132 bow shock crossings in the Galileo data from orbits 0-34 using both the plasma wave (PWS) and magnetometer (MAG) data sets. We have determined the boundary normal directions for both these newly identified crossings as well as the previously published crossings of Galileo, Ulysses, Voyager and Pioneer. When possible, boundary normals were determined from the MAG data by the minimum variance technique of Sonnerup and Cahill [1967]. Some boundary crossings could not be analyzed because of data gaps or inadequate sampling resolution. The analyzed boundary crossings (130 magnetopause, 156 bow shock) are well distributed in local time (~03:00 - 19:00) and are mostly near equatorial. Initial results indicate that the shape models used by Joy et al. [2002] are reasonable. We will examine the small non-zero mean difference between the observed and model boundary surfaces to determine whether the discrepancy is statistically significant. The large variance of the observed normal directions about the mean may imply that the normal directions fluctuate because of surface waves on the boundaries or that steady state models do not apply in the presence of changing solar wind conditions. Abstract Shape models for the bow shock and magnetopause (Figure 1) were determined by using Ogino-Walker MHD simulation [Ogino et al., 1998] results from runs at different values of the solar wind dynamic pressure (P D ). MHD simulation thermal pressure with B=0 and P=0.090 nPa. Traces show the magnetopause (dashed) and bow shock surfaces (solid). Figure 1 This shape model is a second order polynomial of the form: z 2 = A(P D ) + B(P D )x + C(P D )x 2 + D(P D )y + E(P D )y 2 + F(P D )xy This plot shows the boundary surface cross-sections at Z=0 (a,d), Y=0 (b,e) and X=0 (c,f) at low, average, and high pressure (Figure 4 from Joy et al., [2002]). Note the high degree of symmetry in the model families in both the dawn-dusk and equatorial planes. Figure 2 X Y -200 -100 0 100 200 -200 -150 -100 -50 0 50 100 150 200 The Joy et al. [2002] boundary models use the fraction of time all observing spacecraft were inside or outside the boundary (magnetopause or bow shock) to determine the most probable boundary location. In both cases, the data are mapped to the sub-solar line to give a standoff distance. If this mapping is incorrect, the probability distributions might be very different. Figure 3 shows how data are mapped from the observation point along the spacecraft trajectories to bins along the sub-solar line. Figure 3 Figure 3 demonstrates how the shape model impacts the statistics determined along the sub-solar line. The pink model maps the red data points to the sub-solar line and the blue model maps the blue points (there is some overlap). The pink model is less flared than the blue model. It maps points on the flanks closer to the planet to the same location that the blue model maps more distant points. Near the nose the mapping is less dependent on the shape model. Boundary Normal Directions Model: The Joy et al. [2002] models can be fit to any location within a large region of space (there are inner and outer solution limits) by simply varying the pressure used to select the model coefficients. For each crossing, the model was fit through the observing spacecraft location and a model normal direction was computed. Observed: Boundary crossing times were either jointly identified in the Galileo MAG and PWS data or were taken from the literature (Pioneer 10/11 – Intriligator and Wolfe, [1976]; Voyager 1/2 - Lepping et al., [1981]; Ulysses – Bame et al., [1992];). The magnetometer data for each event was then analyzed by using the minimum variance technique of Sonnerup and Cahill [1967] to determine the boundary normal directions. The data used in this analysis were the highest time resolution available from the Planetary Data System for each of the various spacecraft (Pioneer 4/3 sec, Voyager 1.92 sec, Ulysses 1 min, Galileo >= 24 sec). Minimum variance solutions are highly sensitive to the exact subset of data selected for analysis. For each event, data were selected such that the minimum amount of data was input to allow the field to transition from undisturbed upstream to undisturbed downstream states. In addition, the data in the minimum variance direction were required to be steady and the ratio of the eigenvalues of the solution was required to be large enough to indicate a well defined minimum variance direction ( λ 2 / λ 3 > 2.5). The normal directions for the magnetopause crossings were required to have small (<= 0.5 nT) normal components. Figure 4 shows an example of the data in the minimum variance coordinate system and the data that were used to determine the MV solution. Figure 5 shows the observed and model bow shock and magnetopause normal directions in the X-Y and Y-Z planes of the JSE coordinate system. For the bow shock, good crossings are defined as having λ 2 / λ 3 > 2.5 (well defined normal direction) and separations in time of at least 1 hour (remove waves and other dynamical structures). For magnetopause crossings to be considered good, in addition to meeting the criteria above, the average field in the normal direction during the interval selected for the MV analysis must be <= 0.5 nT. Figure 4 Galileo MAG (orbit 33) - Minimum Variance Coordinates B L [nT] -16.00 -8.00 0.00 8.00 B M [nT] -12.00 -4.00 4.00 12.00 B N [nT] -12.00 -4.00 4.00 12.00 |B| [nT] DOY: 305 2002-Nov-1 Nov-01 15:00 Nov-01 16:00 Nov-01 17:00 Nov-01 18:00 Nov-01 19:00 0.00 8.00 16.00 24.00 R 50.80 50.42 50.04 49.65 49.27 48.88 loctim 15.07 15.08 15.09 15.09 15.10 15.10 Galileo MAG (orbit 33) - JSE Coordinates B X [nT] -16.00 -8.00 0.00 8.00 B Y [nT] -12.00 -4.00 4.00 12.00 B Z [nT] -12.00 -4.00 4.00 |B| [nT] DOY: 305 2002-Nov-1 Nov-01 15:00 Nov-01 16:00 Nov-01 17:00 Nov-01 18:00 Nov-01 19:00 0.00 8.00 16.00 24.00 R 50.80 50.42 50.04 49.65 49.27 48.88 loctim 15.07 15.08 15.09 15.09 15.10 15.10 Magnetopause crossing in JSE coordinates (left) and minimum variance coordinates (right). The shaded area between the vertical bars shows the time interval used in the analysis. Normal Direction Statistics Table 1 The differences between the model and observed normal directions (model – observed) were computed and analyzed statistically (Table 1). In general, the average angular deviation from the model (cone angle) is much smaller than the standard deviations (BS μ = 3.5 o , σ = 30 o ; MP μ = -7.5 o , σ = 38 o ; cone angles are given the same sign as the difference in the y-components ). However, many of the observed boundary normals are not well defined. We have further analyzed the good boundary crossing events to see if there are any statistically significant local time variations. For both the magnetopause and bow shock surfaces, the mean angular differences of the normals, projected into the JSE X-Y plane are consistent with the model shapes being less flared than the observed crossings. However, given the large standard deviations and the small number of samples, these results by themselves do not provide statistical justification for abandoning the MHD derived shape models. Both model shapes also show very good agreement with the observations near noon local time. Table 1 shows the basic statistics associated with the differences between the model and observed normal directions. The x, y, and z’s are the differences between the unit vector components. The cone angle is the 3-D angle between the two normal directions. The X-Y, X-Z, and Y-Z angles are the projections of the cone angle into each of these planes in the JSE coordinate system. Projections are only considered good when the observed normal is more than 45 o from the normal of the projection plane. Summary and Conclusions 1. In general the model bow shock and magnetopause shapes derived from the Ogino-Walker simulation do a good job of predicting the average observed normal directions. 2. The agreement between observations and model is best on the dayside, particularly near noon. 3. The observations of both the bow shock and the magnetopause normal directions suggest that the model shape could be improved if the flaring angle was 5-10 o larger. 4. The average magnetopause cone angle on the dawn side is much larger than on the dusk side. This result is not yet understood but may be related to the fact that the dawn-side observations are further from the equator than most of the dusk side passes. 5. The observed magnetopause normal directions have a larger scatter on the night-side than on the day-side. The scatter is consistent with dynamic processes including waves being present on the boundary flanks. References Joy, S. P., M. G. Kivelson, R. J. Walker, K. K. Khurana, C. T. Russell, and T. Ogino, Probabilistic models of the Jovian magnetopause and bow shock locations, J. Geophys Res., 107, No. A10, 2002. Ogino, T., R.J. Walker, and M.G. Kivelson, A global magnetohydrodynamic simulation of the jovian magnetosphere, J. Geophys. Res., 103, 225, 1998. Sonnerup, B. U. O., and L/. J. Cahill, Magnetopause structure and attitude from Explorer 12 observations, J. Geophys. Res., 72, 171, 1967. Intriligator, D. S., and J. H. Wolfe, Results from the plasma analyzer experiment on Pioneers 10 and 11, in Jupiter, edited by T. Geherls, pp 848-869, Univ. of Arizona Press, Tuscon, 1976. Lepping, R. P., M. G. Silverstein, and N. F. Ness, Magnetic field measurements at Jupter by Voyagers 1 and 2: Daily plots of 48 second averages, NASA Tech., 83, 864, 1981. Bame, S.J. B.L. Barraclough, W.C. Feldman, G.R. Gisler, J.T. Gosling, D.J. McComas, J.L. Philips, M.F. Thomsen, B.E. Goldstein, and M. Neugebauer, Jupiter’s magnetosphere: Plasma description from the Ulysses flyby, Science, 257, 1539, 1992. Huddleston, D.E., C.T. Russell, M.G. Kivelson, K.K. Khurana, and L. Bennett, Location and shape of the jovian magnetopause and bow shock, J. Geophys. Res., 103, No. E9, 20075, 1998. The Joy et al. Boundary Shape Model Figure 5 Magnetopause All Crossings Good Crossings Model and Observed Model and Observed -300 -200 -100 0 100 200 300 -100 -50 0 50 100 unit vector Y Z -300 -200 -100 0 100 200 300 -100 -50 0 50 100 unit vector Y Z Bow Shock All Crossings Good Crossings Model and Observed Model and Observed -300 -200 -100 0 100 200 -200 -100 0 100 200 unit vector X Y Y -300 -200 -100 0 100 200 -200 -100 0 100 200 unit vector X -200 -100 0 100 200 -200 -100 0 100 200 unit vector X Y -200 -100 0 100 200 -200 -100 0 100 200 unit vector X Y -200 -100 0 100 200 -100 -50 0 50 100 unit vector Y Z -200 -100 0 100 200 -100 -50 0 50 100 unit vector Y Z X -200 -100 0 100 -200 -100 0 100 200 a Bow Shock Y X -200 -100 0 100 0 100 200 300 400 b Z Y -200 -100 0 100 200 0 100 200 300 400 c Z Y -200 -100 0 100 200 0 100 200 300 400 f Z X -200 -100 0 100 0 100 200 300 400 e Z X -200 -100 0 100 -200 -100 0 100 200 d Magnetopause Y Dawn-Dusk Equatorial Noon-Midnight Bow Shock x y z Cone Angle X-Y Angle X-Z Angle Y-Z Angle Full Average 0.07 0.05 0.00 3.48 2.61 -1.68 6.17 StdDev 0.26 0.27 0.33 30.08 23.20 36.83 44.08 N-Samples 156 156 156 156 156 156 156 Good Data Average 0.03 0.07 0.00 4.43 2.52 -3.44 -7.12 StdDev 0.24 0.25 0.30 27.27 19.36 16.13 17.24 N-Samples 107 107 107 107 96 34 22 Dawn (03:00 - 09:00 LT) 0.04 -0.13 -0.07 -19.40 -7.99 -0.65 -2.21 StdDev 0.34 0.19 0.30 23.28 15.03 29.47 15.64 N-Samples 15 15 15 15 13 3 5 Noon (09:00-15:00 LT) 0.11 0.06 0.03 5.43 4.02 -9.39 6.70 StdDev 0.07 0.12 0.13 11.01 7.31 4.58 0.54 N-Samples 17 17 17 17 14 10 1 Dusk (15:00-21:00 LT ) 0.02 0.11 0.00 8.98 4.19 -1.00 -9.52 StdDev 0.16 0.16 0.19 17.22 12.41 5.04 6.30 N-Samples 75 75 75 75 69 21 16 Magnetopause x y z Cone Angle X-Y Angle X-Z Angle Y-Z Angle Full Average 0.11 -0.03 0.01 -7.55 -4.65 0.70 -3.68 StdDev 0.46 0.34 0.24 37.50 55.09 30.58 31.43 N-Samples 130 130 130 130 130 130 130 Good Data Average 0.08 -0.02 0.01 -3.83 3.68 5.14 -4.38 StdDev 0.34 0.26 0.18 28.37 13.74 12.33 7.60 N-Samples 82 82 82 82 58 37 24 Dawn (03:00 - 09:00 LT) 0.20 -0.40 0.06 -45.43 -13.26 21.35 -17.36 StdDev 0.26 0.18 0.13 20.27 6.59 10.46 6.71 N-Samples 19 19 19 19 9 9 6 Noon (09:00-15:00 LT) 0.04 0.06 0.00 3.14 4.63 -0.87 -0.80 StdDev 0.08 0.14 0.08 10.71 8.34 5.01 0.70 N-Samples 29 29 29 29 25 19 3 Dusk (15:00-21:00 LT ) 0.05 0.13 0.00 13.48 9.05 1.61 0.10 StdDev 0.21 0.11 0.09 15.09 8.60 4.17 3.52 N-Samples 60 60 60 60 50 35 41

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  • Do the Jovian Bow Shock and Magnetopause Surfaces in the Joy et al. [2002] Model Predict Measured Boundary Normals Correctly?S. P. Joy1,2, W. S. Kurth3, M. G. Kivelson1,2, R. J. Walker1,2

    1) Institute of Geophysics and Planetary Physics – University of California at Los Angeles2) Dept. of Earth and Space Science – University of California at Los Angeles

    3) Dept. of Physics and Astronomy – University of Iowa

    Joy et al. [2002] provided probabalistic descriptions of the jovian bow shock andmagnetopause locations by mapping spacecraft observations to the sub-solar point along model surfaces derived from the MHD simulation of Ogino et al. [1998]. The resulting statistics are strongly affected by the surface models used in the mapping process. Here we analyze the quality of the surface models used in that mapping by comparing the normal directions of the observed boundary crossings to the normal directions predicted by the model surfaces. We have identified 116 magnetopause and 132 bow shock crossings in the Galileo data from orbits 0-34 using both the plasma wave (PWS) and magnetometer (MAG) data sets. We have determined the boundary normal directions for both these newly identified crossings as well as the previously published crossings of Galileo, Ulysses, Voyager and Pioneer. When possible, boundary normals were determined from the MAG data by the minimum variance technique of Sonnerup and Cahill [1967]. Some boundary crossings could not be analyzed because of data gaps or inadequate sampling resolution. The analyzed boundary crossings (130 magnetopause, 156 bow shock) are well distributed in local time (~03:00 - 19:00) and are mostly near equatorial. Initial results indicate that the shape models used by Joy et al. [2002] are reasonable. We will examine the small non-zero mean difference between the observed and model boundary surfaces to determine whether the discrepancy is statistically significant. The large variance of the observed normal directions about the mean may imply that the normal directions fluctuate because of surface waves on the boundaries or that steady state models do not apply in the presence of changing solar wind conditions.

    Abstract

    Shape models for the bow shock and magnetopause (Figure 1) were determined by using Ogino-Walker MHD simulation [Ogino et al., 1998] results from runs at different values of the solar wind dynamic pressure (PD).

    MHD simulation thermal pressure with B=0 and P=0.090 nPa. Traces show the magnetopause (dashed) and bow shock surfaces (solid).

    Figure 1

    This shape model is a second order polynomial of the form:

    z2 = A(PD) + B(PD)x + C(PD)x2 + D(PD)y + E(PD)y2 + F(PD)xy

    This plot shows the boundary surface cross-sections at Z=0 (a,d), Y=0 (b,e) and X=0 (c,f) at low, average, and high pressure (Figure 4 from Joy et al., [2002]). Note the high degree of symmetry in the model families in both the dawn-dusk and equatorial planes.

    Figure 2

    X

    Y

    -200 -100 0 100 200

    -200

    -150

    -100

    -50

    0

    50

    100

    150

    200

    The Joy et al. [2002] boundary models use the fraction of time all observing spacecraft were inside or outside the boundary (magnetopause or bow shock) to determine the most probable boundary location. In both cases, the data are mapped to the sub-solar line to give a standoff distance. If this mapping is incorrect, the probability distributions might be very different. Figure 3 shows how data are mapped from the observation point along the spacecraft trajectories to bins along the sub-solar line.

    Figure 3

    Figure 3 demonstrates how the shape model impacts the statistics determined along the sub-solar line. The pink model maps the red data points to the sub-solar line and the blue model maps the blue points (there is some overlap). The pink model is less flared than the blue model. It maps points on the flanks closer to the planet to the same location that the blue model maps more distant points. Near the nose the mapping is less dependent on the shape model.

    Boundary Normal Directions Model:The Joy et al. [2002] models can be fit to any location within a large region of space (there are inner and outer solution limits) by simply varying the pressure used to select the model coefficients. For each crossing, the model was fit through the observing spacecraft location and a model normal direction was computed.

    Observed:Boundary crossing times were either jointly identified in the Galileo MAG and PWS data or were taken from the literature (Pioneer 10/11 – Intriligator and Wolfe, [1976]; Voyager 1/2 - Lepping et al., [1981]; Ulysses – Bame et al., [1992];). The magnetometer data for each event was then analyzed by using the minimum variance technique of Sonnerup and Cahill [1967] to determine the boundary normal directions.The data used in this analysis were the highest time resolution available from the Planetary Data System for each of the various spacecraft (Pioneer 4/3 sec, Voyager 1.92 sec, Ulysses 1 min, Galileo >= 24 sec).

    Minimum variance solutions are highly sensitive to the exact subset of data selected for analysis. For each event, data were selected such that the minimum amount of data was input to allow the field to transition from undisturbed upstream to undisturbed downstream states. In addition, the data in the minimum variance direction were required to be steady and the ratio of the eigenvalues of the solution was required to be large enough to indicate a well defined minimum variance direction ( λ2/ λ3 > 2.5). The normal directions for the magnetopause crossings were required to have small ( 2.5 (well defined normal direction) and separations in time of at least 1 hour (remove waves and other dynamical structures). For magnetopause crossings to be considered good, in addition to meeting the criteria above, the average field in the normal direction during the interval selected for the MV analysis must be