Propagation properties of foreshock cavitons: Cluster observations Wang Mengmeng, Yao Shutao, 史 全岐, zhang hui, Tian Anmin, Degeling Alexander, Zhang Shuai, Guo Ruilong, Sun Weijie, Liu Ji, Bai Shichen, Shen Xiaochen, Zhu Xiaoqiong, Fu Suiyan and Pu Zuyin Citation: SCIENCE CHINA Technological Sciences ; doi: 10.1007/s11431-018-9450-3 View online: http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 Published by the Science China Press Articles you may be interested in Statistical research on the motion properties of the magnetotail current sheet: Cluster observations SCIENCE CHINA Technological Sciences 53, 1732 (2010); Propagation of interplanetary shock excited ultra low frequency (ULF) waves in magnetosphere-ionosphere-atmosphere —Multi-spacecraft “Cluster” and ground-based magnetometer observations SCIENCE CHINA Technological Sciences 53, 2528 (2010); Statistical survey on the magnetic field in magnetotail current sheets: Cluster observations Chinese Science Bulletin 55, 2542 (2010); Low-frequency fluctuations in the magnetosheath: Double Star TC-1 and Cluster observations Science in China Series E-Technological Sciences 51, 1626 (2008); Structures of magnetic null points in reconnection diffusion region: Cluster observations Chinese Science Bulletin 53, 1880 (2008); Fo ed SCIENCE CHINA Technological Sciences rR pt Propagation properties of foreshock cavitons: Cluster observations Journal: Science China Technological Sciences Manuscript ID SCTS-2018-0487.R3 ev Manuscript Type: Original Article iew Ac ce Date Submitted by the 23-Nov-2018 Author: ly On Complete List of Authors: Wang, Mengmeng; Shandong University; Chinese Academy of Sciences, National Space Science Center Yao, Shutao; Shandong University at Weihai 史, 全岐; Shandong University, School of Space Science and Physics zhang, hui; Geophysical Institute, University of Alaska Fairbanks Tian, Anmin; School of Space Science and Physics, Shandong University at Weihai Degeling, Alexander Zhang, Shuai; Shandong University at Weihai Guo, Ruilong; Chinese Academy of Sciences, Institute of Geology and Geophysics Sun, Weijie; University of Michigan, Department of Climate and Space Sciences and Engineering Liu, Ji; Chinese Academy of Sciences Bai, Shichen; Shandong University at Weihai Shen, Xiaochen Zhu, Xiaoqiong Fu, Suiyan; Peking University, School of Earth and Space Science Pu, Zuyin; Peking University, School of Earth and Space Science foreshock transient phenomena, cavitons, nonlinear evolution of ULF Keywords: waves, propagation and evolution properties of structures, multipoint spacecraft methods Speciality: Space Sciences Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english ed Fo iew Ac ce ev rR ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences pt Page 1 of 41 Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences Propagation properties of foreshock cavitons: Cluster 2 observations 3 WANG MengMeng1,2, YAO ShuTao1, SHI QuanQi1*, ZHANG Hui3, TIAN AnMin1, 4 DEGELING Alexander William1, ZHANG Shuai1, GUO RuiLong4, SUN WeiJie5, 5 LIU Ji2, BAI ShiChen1, SHEN XiaoChen1, ZHU XiaoQiong1, FU SuiYan6, PU 6 ZuYin6 7 1School 8 2National 9 3Geophysical 10 11 12 4Institute 5Department Space Science Center, Chinese Academy of Sciences, Beijing, 100190, China Institute, University of Alaska Fairbanks, Fairbanks, Alaska, 99775, USA of Geology and Geophysics, Chinese Academy of Sciences, Beijing, 100029, China of Space Physics and Applied Technology, Peking University, Beijing, 100871, China *Corresponding author (email: sqq@sdu.edu.cn) Abstract rR 14 of Space Science and Physics, Shandong University, Weihai, 264209, China of Climate and Space Sciences and Engineering, University of Michigan, Ann Arbor, 48113, USA 6Institute 13 pt ed 1 Fo 15 Foreshock cavitons are transient phenomena observed in the terrestrial foreshock region. 16 They are characterized by a simultaneous depression of magnetic field magnitude and plasma 17 density, which are bounded with enhancements of these two parameters and surrounded by 18 ultra low frequency (ULF) waves. Previous studies focused on the interplanetary magnetic 19 field (IMF) conditions, solar wind (SW) conditions, and the growth of the foreshock waves 20 related to the generation of foreshock cavitons. Previously, a multipoint spacecraft analysis 21 method using Cluster data was applied to analyze only two foreshock cavitons, and this 22 method did not consider uncertainties. In this study, multipoint spacecraft analysis methods, 23 including the timing method, the Minimum Directional Difference (MDD) method, and the 24 Spatiotemporal Difference (STD) method are applied to determine the velocity in both 25 spacecraft and solar wind frames. The propagation properties show good agreement with 26 previous results from simulations and observations that most cavitons move sunward in the 27 solar wind frame, with the velocities larger than the Alfvén speed. The propagation properties 28 of foreshock cavitons support the formation mechanism of cavitons in previous simulations, 29 which suggested that cavitons are formed due to the nonlinear evolution of compressive ULF 30 waves. We find that there is clear decreasing trend between the size of cavitons and their 31 velocity in the solar wind frame. In addition, the timing method considering errors has been 32 applied to study the evolution properties by comparing the velocities with errors of the 33 leading and trailing edges, and we identify three stable cavitons and one contracting caviton, 34 which has not been studied before. Most cavitons should remain stable when they travel 35 toward the Earth’s bow shock. The relationship between the size of foreshock cavitons and 36 their distance from the bow shock is also discussed. iew Ac ce ev ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 2 of 41 Page 3 of 41 37 Key words foreshock transient phenomena, cavitons, nonlinear evolution of ULF waves, 38 propagation and evolution properties of structures, multipoint spacecraft methods 39 1 Introduction 40 When the supermagnetosonic magnetized solar wind encounters the Earth’s magnetosphere, 41 the bow shock forms. The nature of the bow shock depends on the angle Bn between the 42 interplanetary magnetic field (IMF) and the shock normal [1]. The shock is either 43 quasi-parallel 44 upstream of the quasi-parallel shock and the “shock foot” of the quasi-perpendicular shock [2] 45 [3] [4], is populated with particles backstreaming from the bow shock, ULF waves [5][6] 46 [7][8], hot flow anomalies (HFAs) [9], spontaneous hot flow anomalies (SHFAs) [10] [11], 47 and foreshock cavities [12] [13]. These transients can modify the solar wind before they 48 encounter the bow shock. pt ed ( Bn 45 ) or quasi-perpendicular ( Bn 45 ) . The foreshock, located Fo 49 Global hybrid simulations performed by Omidi [14] and Blanco-Cano et al. [15] [16] 50 suggested that a new category of transient structure called foreshock caviton exist in the 51 foreshock region. Foreshock cavitons are transient phenomena as common as HFAs and 52 SHFAs in the foreshock region, which saturate at a width of several RE , with a depressed core 53 plasma density and magnetic field strength bounded by a rim of enhanced plasma density and iew Ac ce ev rR 54 magnetic field strength [14] [15] [16]. Cavitons are not associated with IMF discontinuities, 55 and there is no plasma heating or flow deflection inside the structures, which is in contrast to 56 HFAs. Omidi et al. [14] referred to cavitons as ‘foreshock cavities’ in their simulation of 57 formation of foreshock cavitons. However, foreshock cavitons are always embedded in a sea 58 of ULF waves, which is in contrast to other isolated cavities with no ULF waves nearby. 59 Diffuse ions are found inside and outside foreshock cavitons, while diffuse ions are only 60 found inside foreshock cavities. Schwartz et al. [13] suggested foreshock cavities are formed 61 by thermal expansion because of the magnetic field in cavities connected to the bow shock, 62 which contrasts with notion that the wave interactions generate foreshock cavitons. Hence, 63 Blanco-Cano et al. [15] [16] used the term, foreshock cavitons, to describe these new 64 structures. ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences 65 The interaction of ULF waves in the foreshock contributes to the formation of foreshock 66 cavitons. Under the condition of radial IMF, the foreshock region is permeated by parallel 67 propagating sinusoidal fluctuations with right- or left-hand circular polarization, and fast, 68 linearly polarized, oblique (FLO) waves. The nonlinear evolution of these two types of 69 ultra-low frequency (ULF) waves generates foreshock cavitons [14] [15][16]. Global hybrid 70 simulations performed by Blanco-Cano et al. [16] showed that foreshock cavitons could exist 71 under a wide range of IMF [17] [18] orientations depending on the Mach number. They found 72 that major features of foreshock cavitons do not vary with the IMF orientation. Statistical Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences 73 studies of foreshock cavitons [20] [21] have shown that foreshock cavitons are observed for a 74 wide range of IMF orientation and SW conditions. The time duration of cavitons is 65s and 75 the size is 4.6 RE on average. Inside cavitons, the variations of plasma density and magnetic 76 field magnitude are highly correlated. The foreshock-bow shock system is a significant region for the solar wind-magnetosphere 78 coupling process. There are a plethora of multi-scale plasma physics processes and 79 phenomena in foreshock, making it an important and excellent laboratory to study plasma 80 physics. The generation and evolution of foreshock cavitons are an intrinsic process of the 81 foreshock-bow shock system and play a considerable role in reformation of the system. 82 Hybrid simulations suggest that the interaction between foreshock cavitons and the bow 83 shock generate another transient phenomenon, namely, SHFAs [10][11]. Several cavitons 84 even generate complicated and large structures if they arrive at the bow shock at the same 85 time. They play an important role in the deformation of the bow shock and can lead to ripples 86 on the surface of bow shock. Cavitons may lead to disturbances in the magnetosheath and 87 surface waves on the magnetopause [10] [11] [22] [23] [24]. Considering the magnetospheric 88 response [25], foreshock cavitons are no less important than foreshock transients such as 89 HFAs with large dynamic pressure pulses [26] [27]. Given that cavitons exhibit similar 90 sudden dynamic pressure decreases, cavitons may generate ULF waves in the magnetosphere 91 [28] [29] [30] [31] [32] and drive magnetospheric vortices [33]. Foreshock cavitons may 92 evolve into SHFAs, which can make the plasma more inhomogeneous and contribute to the 93 formation of magnetosheath jets [34] and magnetosheath filamentary structures (MFS) [35]. 94 Successive expansion and contraction of the magnetosphere caused by SHFAs are significant, 95 which may excite ULF waves in the inner magnetosphere [36] [37] [38] [39] [40] [41]. pt ed 77 iew Ac ce ev rR Fo ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 96 As foreshock cavitons form, they are convected by the solar wind towards the bow shock. 97 Blanco-Cano et al. [16] found that cavitons propagate sunward in the solar wind frame, as 98 weakly compressive waves. In their simulations, the velocity of the example caviton in the 99 solar wind frame is 98 km/s, which equals 1.9 VA [16]. Kajdič et al. [19] analyzed two 100 foreshock cavitons observed by the multi-spacecraft Cluster mission. The two cavitons 101 propagate sunward in the solar wind frame at a speed of 188 km/s and 120 km/s. However, 102 only the timing method without calculating errors has been applied to calculate the velocities 103 of these two cavitons [19]. Although theories and simulations provide the formation 104 conditions and the evolution of foreshock cavitons, no observations of the evolution of 105 foreshock cavitons have been reported. 106 In this paper, we perform a study of the propagation properties of a series of foreshock 107 cavitons using several multipoint spacecraft analysis methods, including the timing method 108 [42], the Minimum Directional Derivative (MDD) method [43] and the Spatiotemporal Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 4 of 41 Page 5 of 41 109 Difference (STD) method [44]. Four cavitons with both velocities of leading edge and trailing 110 edge considering errors are classified into three stable structures and one contracting structure. 111 We also examine the possible relationship between the size of foreshock cavitons and the 112 distance from cavitons to the bow shock. 113 2 Data and Methods 114 2.1 Data and Event Selection Cluster mission consists of four identical spacecraft (C1, C2, C3, C4). We obtain the 116 magnetic field data with 0.2s resolution from the Fluxgate Magnetometer (FGM) [45] [46] 117 [47] onboard all four spacecraft, and we obtain the ion data with 4s resolution from the Hot 118 Ion Analyzer (HIA) of the Cluster Ion Spectrometer (CIS) [48] on C1. We obtain the solar 119 wind and IMF data with 1-min resolution from the OMNI database, which indicate 120 parameters near the nose of the Earth’s bow shock. pt ed 115 Fo 121 All foreshock caviton events analyzed here are taken from [20], which presented 92 122 foreshock cavitons selected using C1 data from 2001 to 2006. Firstly, foreshock cavitons 123 observed by all four Cluster spacecraft are selected. Then, we select the cavitons with clear 124 leading and trailing boundaries and with the similar profiles observed by four spacecraft. 125 Following these criteria, twelve foreshock cavitons are selected and their propagation 126 properties are investigated. Further criteria, including the shape parameters of the tetrahedral 127 spacecraft configuration can improve the precision of the timing analysis, MDD analysis, and 128 STD analysis. 129 2.2 Timing method iew Ac ce ev rR 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences The timing method has been widely applied to determine the velocity and normal direction 131 of shocks, magnetic holes, magnetic peaks, and HFAs [42] [49] [50] [51] [52] [53]. To 132 calculate the velocities and normal of the boundaries of foreshock cavitons, we apply a 133 similar method by analyzing magnetic field data detected by four Cluster spacecraft [54] [55]. 134 By solving the following equation, ly On 130 135 r ur r U (t i t j ) (ri rj )gn , 136 the unit normal direction n and velocity magnitude U of the foreshock caviton leading 137 and trailing boundaries are obtained. Here, t ti t j is the time lag between two spacecraft 138 observing the same boundary, and r ij r i r j is their corresponding difference in position 139 vectors. As Cluster mission consists of four spacecraft, three differences in position vectors, 140 r r r r12 , r13 , r14 and three time lags, t12 t1 t2 , t13 t1 t3 , t t1 t4 are determined. 141 Furthermore, we estimate the uncertainty of velocity magnitude and normal direction 142 according to [54]. An empirical relative error of time lag is t 0.1t . the relative 143 uncertainty of the distance between satellites is 0.01, the time lag uncertainty contributes (1) r r r r Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences 144 more to the error of results and is considered dominant. A pair of satellites can give an 145 interval [t t , t t ] . The interval is divided into 11 equidistant points. In total 113 146 calculations of velocity and normal are given due to three time intervals determined by four 147 satellites. The mean velocity and normal are given and the standard deviations estimate the 148 uncertainty. 2.3 The MDD method 150 The Minimum Directional Derivative (MDD) method is a dimensionality determination 151 technique with the help of multipoint measurements described by Shi et al. [43]. The 152 eigenvalues and eigenvectors of 153 principal directions of the structure (where T denotes the transposition). Three directions 154 corresponding to the maximum, intermediate and minimum variations of magnetic field are 155 determined straightforwardly by the MDD method, which can help us investigate the time 156 variation of a structure’s characteristic direction. It is proved that the MDD method is feasible 157 for the determination of the normal direction of 1-D structures including magnetic holes [50] 158 [51] [56], and magnetic peaks [52]. pt ed 149 ur ur L ( B)( B)T indicate the dimensionality and the 159 2.4 160 The Spatiotemporal Difference (STD) method [44] can be applied to calculate the velocity 161 of quasi-stationary structures in any dimensionality using multipoint magnetic field 162 measurements. Further, we can resolve time-variations of the velocity from the STD results. 163 By estimating the time variation of the magnetic field and the magnetic gradient tensor B , 164 the velocity of the structure in the spacecraft frame, V str , is obtained from the equation of 166 ur ur ly On 165 iew Ac ce ev The STD method rR Fo 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 6 of 41 ur ur B ur V str g B 0 . t 3 Propagation and evolution properties of foreshock cavitons 167 3.1 168 3.1.1 169 Timing method is applied to calculate the velocity of foreshock cavitons in the spacecraft 170 and the solar wind frames. Here, the GSE coordinate system is used. We obtain the velocity 171 of foreshock cavitons in the solar wind frame from 172 Propagation properties Timing analysis r r V U v sw gn . (2) 173 Here U is the velocity of caviton in the spacecraft frame obtained from the timing analysis, 174 as before. U is along the normal direction, n . The average value of the solar wind velocity 175 measured by CIS-HIA over a 10 minute interval including the cavitons is used to eliminate 176 fluctuations. In accordance with [48], an uncertainty in the solar wind velocity v sw of 10% 177 in magnitude and +/-5° in direction are considered. We carried out four timing calculations r r Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 7 of 41 178 and considered all four calculations to generate our results, including velocities, normal 179 directions and uncertainty estimates, represented as error bars in Figure 4. If the error bar 180 crosses zero, the caviton is probably stationary with respect to the solar wind. Examples of 181 timing analysis are shown in Figure 1. Figure 1(a-d) show the results for the leading boundary, 182 and figure 1(e-h) show the results for the trailing boundary. The mean speed of the leading 183 boundary in the spacecraft frame is 98.6 km/s and the uncertainty is 4.1 km/s as shown in 184 Figure 1b. The average velocity of leading boundary in the solar wind frame is r 219.2 32.9km / s along n L (0.97,0.14,0.17) with uncertainty of 1.8 . Figures 186 1e-1h show the detailed velocity of the trailing boundary with VT 212.7 33.7 km / s 187 and nT ( 0.93,0.18,0.33) . Magnetic field data with different resolutions were employed 188 to check the reliability of the results. The results agree with those using data with 0.2 s 189 cadence. The velocity with error not including zero shows that the caviton is moving in the 190 solar wind plasma. r pt ed 185 rR Fo 191 3.1.2 MDD and STD analysis 192 Here, we apply the MDD and STD methods to calculate the dimensionality and velocity 193 vector and compare the results with those from the timing method. The analysis results of the 194 same case shown in Figure 1 are shown in Figure 2. As the MDD method suggested, the iew Ac ce ev 195 relative size of the three eigenvalues indicate the dimensionality information of the structure. 196 If 1 ? 2 , 3 , we can regard the structures as quasi-1D, and 1 is the eigenvalue of the 197 maximum variant direction of the magnetic field. The maximum variant direction n1 198 represents the normal of the boundary of foreshock caviton. The ratio of the average 199 and 2 in the limited period indicated by orange shadow is 8.7 for the leading boundary. For 200 the trailing boundary, the ratio in the limited period indicated by the blue shadow is 19.6. 201 Therefore, we regard this caviton as quasi-1D structure. ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences r 1 202 The propagation velocity of the leading boundary in the solar wind frame is -219.3 km/s 203 along n L (0.88, 0.29,0.37) and for trailing boundary, the velocity is -222.0 km/s 204 along nT (0.96, 0.27,0.02) . Here, L denotes the leading boundary and T denotes the 205 trailing boundary. These results fall within the velocity error from timing method as shown in 206 Figure 4(a). r r 207 3.1.3 Statistical results 208 The propagation velocity along the normal of the foreshock cavitons are given by equation 209 (2). The velocity vector of the cavitons in the spacecraft frame is equal to U multiplied by n , 210 while the velocity vector of the cavitons in the solar wind frame is equal to V multiplied by r Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences r n . Velocity magnitudes and directions of the twelve foreshock cavitons calculated by timing, 212 MDD and STD methods are plotted in GSE-XY and GSE-XZ planes. Velocity vectors in both 213 the spacecraft frame and the solar wind frame are plotted in Figure 3. In the spacecraft frame, 214 foreshock cavitons are moving towards the Earth. Eleven cavitons are propagating sunwards 215 in the solar wind frame, which is consistent with previous observations [19] and the 216 predictions of simulations [16]. Another caviton observed on Mar 26, 2005 has a velocity in 217 the solar wind frame that is close to zero, for which the error bar crosses zero. pt ed 211 218 Sizes of foreshock cavitons are calculated using both the timing velocities and STD 219 velocities in the spacecraft frame. As foreshock cavitons propagate in the solar wind frame, 220 we estimate the spatial extents of the cavitons by multiplying their speed in the spacecraft 221 frame by their durations, rather than multiplying their durations by the solar wind velocity 222 [20]. Since foreshock cavitons remain stable when they travel towards the bow shock, the 223 velocities of one boundary are used to calculate the extents of cavitons. Fo 224 Figure 4 (a) shows a plot of the estimated size in RE of foreshock cavitons against their 225 propagation velocity in the solar wind frame. This figure shows the trend that smaller 226 foreshock cavitons have significantly higher velocity than larger ones in the solar wind frame. 227 Since the normal of one edge of foreshock cavitons is obtained from the timing method and 228 MDD & STD method, we calculate the angle between the normal direction and the ambient 229 magnetic field vector. This indicates the direction of propagation for a 1-D structure [43] [44]. 230 The results are shown in Figure 4 (b). The average magnetic field value over a 10 minute 231 interval excluding the cavitons is used. We can see that the foreshock cavitons are 232 propagating along the parallel or anti-parallel direction. These results are obtained using two 233 independent techniques (timing and MDD and STD analysis as described above), with both 234 techniques revealing the same trend. iew Ac ce ev rR Evolution of foreshock cavitons ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 235 3.2 236 Here we show a stable caviton structure observed on 16 February 2002 by comparing the 237 velocities with errors of the leading edge and the trailing edge. The detailed process is as 238 follows. The timing analysis shows that the leading edge travels at a speed of about 239 r 219.2 32.9km / s along the direction n L (0.93,0.14,0.17) in the solar wind, while 240 the trailing edge moves at a speed of about 212.7 33.7 km/ s along the direction 241 r n T (0.93,0.18,0.33) in the solar wind frame. Here, L denotes the leading boundary 242 and T denotes the trailing boundary as before. We calculate the difference of velocities 243 between the leading boundary and trailing boundary by projecting the trailing boundary 244 velocity to the normal of the leading boundary and subtracting the leading boundary velocity 245 magnitude: Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 8 of 41 Page 9 of 41 246 V | VT cos nr L , nr T VL | 247 where nr L , nr L 248 V 9.3km / s L T 32.9 33.7 66.6km / s , we conclude that the leading edge 249 and the trailing edge of the caviton move at velocities that are indistinguishable given the 250 error estimates of the measurements. Consequently, the caviton can be regarded as a stable 251 structure as suggested in Xiao et al [53]. (3) the angle between the normal of the leading edge and trailing edge. As Only four out of twelve cavitons have usable timing velocities considering errors of both 253 the leading boundary and trailing boundary, and we investigate the evolution properties of 254 these four cavitons. Three cavitons are stable, and only one shows property of contraction. 255 Our results indicate that cavitons remain stable when they are convected toward the bow 256 shock. pt ed 252 Fo 257 4 Summary and Discussions 258 By using the timing method, MDD and STD method, we analyze the propagation and 259 evolution properties of twelve foreshock cavitons. We find that all cavitons move earthward 260 in the spacecraft frame and the normal of the edge of cavitons are nearly parallel or 261 anti-parallel to the ambient magnetic field. The velocities of cavitons in the solar wind frame 262 are also calculated. Eleven cavitons of all cavitons move sunward in the solar wind frame. 263 These results are consistent with previous ones from simulations and observations. We also 264 find that the caviton observed on March 26, 2005 has features consistent with those of a 265 mature caviton structure. 266 and their propagation velocity in the solar wind frame. As for the evolution properties, the 267 results suggest that most foreshock cavitons remain stable when they propagate towards the 268 bow shock. We find that there is no clear correlation between the size of foreshock cavitons 269 and their distance from the bow shock. iew Ac ce ev rR We find a clear decreasing trend between foreshock caviton size ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences 270 In the simulation of [16], one caviton moves upstream in the solar wind frame at a speed 271 of 1.9 times of the Alfven speed. By Cluster observations, Kajdič et al. [19] found that two 272 cavitons move at 188 km/s and 120 km/s towards the sun in the solar wind frame. We have 273 also found that foreshock cavitons have a variety of propagation velocities, which is 274 consistent with simulation [16]. The nature of ULF waves and the nonlinear evolution of the 275 waves contribute to the propagation properties of cavitons. Weakly compressive waves 276 propagate upstream in the reference frame of background plasma, which is similar to the 277 propagation direction of cavitons. The normal of the edge of cavitons are nearly parallel or 278 anti-parallel to the ambient magnetic field, which suggests that parallel propagating weakly 279 compressive waves are necessary for the generation of foreshock cavitons. Consequently, the 280 propagation properties imply that foreshock cavitons form due to the nonlinear evolution of 281 circularly polarized, parallel propagating ULF waves and compressive, linearly polarized, Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences 282 oblique ULF waves. We find that in all but one case, foreshock cavitons propagate sunward, 283 and their speed can be shown to be larger than the Alfvén speed. Previous results from 284 simulations and observations have found sunward propagating foreshock cavitons with speeds 285 greater than the Alfvén speed. We appear to have found one counter-example. For the caviton observed on Mar 26, 2005, the uncertainty in its velocity in the solar wind 287 frame is greater than its magnitude – in other words it has an error bar across zero. In this case 288 we consider that it is likely that the caviton is stationary with respect to the solar wind, 289 however the size of the uncertainty in velocity for this event is significant; on the order of the 290 Alfven speed. Compared to other cavitons in our study, this event is observed within a higher 291 speed solar wind (larger than 600 km/s) and lower plasma density (less than 3 cm-3) 292 environment. This caviton does not show a double peak internal structure [19]. There are few 293 small fluctuations or high-frequency waves in the interior, and the profile of magnetic field 294 magnitude is similar to that of plasma density. Blanco-Cano et al. finds that the width of 295 cavitons should increase slightly during their evolution [16], and that towards the end of their 296 evolution, the profiles of magnetic field magnitude and density should become similar. 297 Therefore, this caviton appears to be a mature structure with fewer wave features compared to 298 the newly generated cavitons, possibly because these fluctuations have dissipated over time in 299 this case. pt ed 286 iew Ac ce ev rR Fo 300 The correlation between the size of foreshock cavitons and their velocity in the solar wind 301 frame shows that the bigger scale the foreshock caviton has, the slower it moves in the solar 302 wind flow. There is clear decreasing trend between the size of foreshock cavitons and their 303 velocity in the solar wind frame. It is reasonable to expect that, although the structures were 304 found to be 1-D based on the scale-size of the Cluster satellite configuration, they may be at 305 least 2-D on a larger scale. If we assume that they have roughly the same shape, then size 306 measurements we have obtained are a proxy for their scale size. A structure of a given size 307 propagating with respect to the solar wind will be subject to an effective drag force that 308 increases with the structure’s size (which can be calculated by integrating the total pressure 309 forces around the structure). This may make the larger cavitons more easily be slowed down 310 in the solar wind plasma frame, explaining our observations. ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 311 We studied the propagation properties of foreshock cavitons, which are similar to the 312 propagation properties of solitary waves reported in [50] [59]. Both cavitons and solitary 313 waves are fast-mode structures/waves, and they propagate in the background plasma frame. 314 However, the size of foreshock cavitons exceeds tens to several hundred ion gyroradii and 315 there is no correlation between the propagation velocity in solar wind and the velocity of fast 316 magnetosonic waves. Therefore, foreshock cavitons do not correspond to these kinds of 317 solitary waves. 318 Page 10 of 41 Among the four foreshock cavitons in our study, three cavitons are stable and one is Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 11 of 41 contracting, indicating these are mature or near mature structures. The mature foreshock 320 cavitons are structures with a high correlation between the decrements in density and 321 magnetic field magnitude [20]. Due to the enhancement of the pressure of suprathermal ions, 322 the total pressure inside and outside foreshock cavitons is very similar, [16] [19] and the 323 cavitons can maintain equilibrium. However, when the cavitons are steepening and evolving, 324 their sizes evaluated from the density profile become larger as the structures will expand. 325 These cavitons cannot be selected using rigorous criteria [20] and we are still unable to 326 diagnose their evolution from generation to maturity using spacecraft data. pt ed 319 327 We find that there is no clear correlation between the size of foreshock cavitons and their 328 distance from the bow shock, which may be due to the origin of foreshock cavitons and their 329 evolution properties. The bow shock model presented in [54] [55] [56] under the 330 corresponding IMF and solar wind conditions is used to calculate the distance from the 331 cavitons to the bow shock. Hybrid simulations have shown that foreshock cavitons can appear 332 in a broad area of the ion foreshock [16] and be carried by the solar wind toward the bow 333 shock. The foreshock region is populated by the weakly compressive waves generated by 334 field-aligned ions [63]. Fast, linearly polarized, oblique waves will grow significantly on the 335 condition that the backstreaming ions are cold. The density striations in the perpendicular 336 direction caused by waves are essential for the formation of foreshock cavitons. The nonlinear 337 interaction of the two kinds of waves generates foreshock cavitons. The process does not need 338 a trigger and can be generated self-consistently around the bow shock, which is an intrinsic 339 process in foreshock region. Foreshock cavitons will not disappear on the way to the bow 340 shock. The evolution properties in our study show that cavitons will not expand or contract, 341 instead, caviton width will change only slightly when they are carried toward the bow shock. 342 The width of cavitons depends on their initial size. Therefore, the relationship between the 343 size of cavitons and their distance from the bow shock is not clear. On the other hand, even if 344 foreshock cavitons will expand or contract during their travel toward the bow shock, we 345 cannot obtain the correlation between the size of foreshock cavitons and their distance from 346 the bow shock, as cavitons can be observed on their way to the bow shock and their evolution 347 stages are different from one-another. iew Ac ce ev rR Fo ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences 348 As hybrid simulations performed by Omidi et al. [10] suggested that SHFAs form due to 349 the interaction between foreshock cavitons and the bow shock, more work is required to 350 understand the relation between foreshock cavitons and SHFAs. Using high-resolution plasma 351 data from the Magnetospheric Multiscale (MMS) mission, the particles properties inside 352 foreshock cavitons can be analyzed. 353 Acknowledgments We acknowledge the Cluster Team for providing data. All Cluster data is 354 obtained from the Cluster Science Archive (http://www.cosmos.esa.int/web/csa/). We also 355 acknowledge NASA's Space Physics Data Facility (SPDF) for providing OMNI data Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences 356 (https://omniweb.gsfc.nasa.gov/). This work was supported by the National Natural Science 357 Foundation of China (grants 41574157, 41628402, and 41774153), and Hui Zhang is 358 partially supported by NSF AGS-1352669. We are grateful to the International Space Science 359 Institute-Beijing for supporting the international team “Dayside Transient Phenomena and 360 Their Impact on the Magnetosphere-Ionosphere”. The project was also supported by the 361 specialized research fund for State Key Laboratories. 362 Reference 364 365 366 367 368 370 Space Sci Rev, 2005, 118: 155–160 2. J P Eastwood, E A Lucek, C Mazelle, et al. The foreshock. Space Science Reviews, 2005,118: 41–94 3. Hao Y F, Lu Q M, Gao X L, et al. Ion dynamics at a rippled quasi-parallel shock: 2D hybrid simulations, Astrophys J, 2016, 823, 7-18 4. Hao Y F, Gao X L, Lu Q M, et al. Reformation of rippled quasi-parallel shocks:2-D rR 369 1. Balogh A, Schwartz S J, Bale S D, et al. 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Zhang H, Khurana K K, Kivelson M G, et al. Three-dimensional lunar wake 521 reconstructed from ARTEMIS data. J. Geophys. Res. Space Physics, 2014, 119: 522 5220–5243 523 524 iew Ac ce 520 63. Sun W J, Fu S Y, Parks G K, et al. Field-aligned currents associated with dipolarization fronts. Geophys. Res. Lett., (2013),40: 4503-4508 ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 16 of 41 Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english iew Ac ce ev rR Fo 525 ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences pt ed Page 17 of 41 526 Figure 1 Timing analysis results for one typical foreshock caviton. The left four panels (a-d) are for the 527 leading boundary, and the right four panels (e-h) are for the trailing boundary. Four different magnetic 528 field magnitudes marked by the four colored horizontal lines in Figures 1(a) are used to determine the 529 time when the spacecraft crossed the caviton, corresponding to the different histograms of the same 530 color in Figures 1b-1d. The magnetic field observed by the Cluster spacecraft (Figure 1a). And the 531 black, red, green, and blue curve denotes Cluster 1, 2, 3, 4, respectively. Histograms of the velocities of 532 the boundary in the spacecraft frame (Figure 1b). Histograms of the velocities in the solar wind frame 533 (Figure 1c). Histograms of angles between any two normal vectors of leading boundary (Figure 1d). 534 And the ultimate results of velocity, normal and their uncertainty considering four calculations are 535 written in bold in every subgraph. Figures 1e-1h are results for the trailing boundary of this caviton, 536 and the formats are the same as in Figures 1a-1d. Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences pt ed 538 ev rR Fo 539 Figure 2 MDD and STD analysis result: (a) magnetic field magnitude in GSE coordinates. (b) 541 eigenvalues 542 velocity along the maximum direction. The red shadowed area indicates the leading edge, while the 543 blue shadowed area is the trailing edge. iew Ac ce 540 1 , 2 , and 3 . (c) normal along the maximum derivative direction of magnetic field. (d) ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 18 of 41 Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 19 of 41 545 pt ed 546 rR Fo 547 ev Figure 3 Distribution of foreshock cavitons in GSE XY and XZ plane, with velocity vector in 549 the spacecraft frame (a and b) and in the solar wind frame (c and d). GSE coordinate system Ac ce 548 is used. The azure arrows denote the timing results, and the pink arrows denote the MDD and 551 STD results. A bow shock model presented by Chao et al. [60] is used, under typical solar wi 552 nd conditions ( Bz 0.35nT , D p 2.48nT , M ms 6.96,and 2.08) . The green curve 553 denotes the nominal bow shock. The caviton observed on Mar 26, 2005 is marked by 554 a black solid dot. iew 550 ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences 558 pt ed 556 557 Fo 559 Figure 4 (a) The size of foreshock cavitons versus their propagation velocity of foreshock cavitons in 560 the solar wind frame. The X axis shows the velocity from the timing or the MDD and STD methods in 561 the solar wind frame, and the Y axis denotes the size of foreshock cavitons. The blue horizontal and 562 vertical lines denote error bars. (b) The angle between the normal direction of the boundary of 563 foreshock cavitons and the ambient magnetic field. The caviton observed on Mar 26, 2005 is 564 marked as ’1’. In both plots, the blue thin diamonds denote the timing result, while the pink asterisks 565 denote the MDD and STD results. 566 iew Ac ce ev rR ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 20 of 41 Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 21 of 41 Leading Edge:2002−02−16 08:32:56−08:32:59 Leading Edge:2002−02−16 08:33:07−08:33:10 8 10.5 Bt (nT) (a) Bt (nT) 10 9.5 9 7.5 (e) 7 8.5 8 08:32:57 08:32:58 Time 40 rR σ3=3.8km/s U3=97.8km/s σ4=3.7km/s U4=98.3km/s 20 0 50 100 150 percentage (c) 40 20 0 ie Ac ce U(km/s) 60 ev 200 −300 −200 V1=−218.7km/s σ1=32.7km/s V2=−219.2km/s σ2=32.7km/s V3=−221.4km/s σ3=32.6km/s V4=−217.5km/s σ4=32.6km/s V =−219.2km/s σ =32.9km/s −100 0 100 200 60 40 20 σ =4.1km/s U =98.6km/s 0 percentage σ2=4.1km/s U2=99.9km/s 0 w U1=100.3km/s σ1=4.7km/s U2=91.2km/s σ2=4.1km/s U3=90.8km/s σ3=4.2km/s U4=87.4km/s σ4=4.2km/s U =92.4km/s σ =6.4km/s 0 50 On 60 ly 40 20 0 300 −300 −200 U−dot(Vsw,n)(km/s) 20 150 200 V1=−200.1km/s σ1=32.4km/s V2=−217.4km/s σ2=32.6km/s V3=−216.0km/s σ3=32.6km/s V4=−217.3km/s σ4=32.5km/s V =−212.7km/s σ =33.7km/s −100 0 100 200 (g) 300 60 o n1=(−0.97 0.05 0.22) σ1=1.1 n2=(−0.98 0.11 0.18) σ2=1.0o n3=(−0.98 0.16 0.14) σ3=1.0o n4=(−0.96 0.24 0.14) σ4=1.0o n =(−0.97 0.14 0.17) σ =1.8o −20 −10 0 θn ,n i 10 20 percentage (d) 100 (f) U−dot(Vsw,n)(km/s) 60 40 08:33:09 U(km/s) percentage percentage Fo σ1=4.4km/s U1=98.6km/s 60 80 08:33:08 Time 80 80 (b) 08:33:07 pt ed 08:32:56 percentage 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences 30 40 20 n1=(−0.91 0.22 0.35) σ1=0.4o n2=(−0.94 0.17 0.30) σ2=0.7o n3=(−0.93 0.16 0.32) σ3=0.6o n4=(−0.93 0.15 0.34) σ4=0.6o n =(−0.93 0.18 0.33) σ =1.8o −20 j −10 0 θn ,n i 10 j Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english 20 (h) 30 Cluster MDD and STD Analysis 2002−02−16 (a) Bt [nT] 10 9 8 rR 7 −5 10 −10 10 1 0.5 λ3 −0.5 −1 200 nx ny ly On 0 n1 λ2 iew Ac ce (b) Vn1 [km/s] λ1 ev λvalues 6 (c) C1 C2 C3 C4 Fo 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 22 of 41 pt ed SCIENCE CHINA Technological Sciences nz Vx 100 (d) Vy 0 Vz −100 −200 08:32:43 08:32:53 08:33:03 Vt 08:33:13 08:33:23 08:33:33 Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 23 of 41 Spacecraft Frame Solar Wind Frame Timing results MDD & STD results Timing results MDD & STD results Timing results MDD & STD results 100km/s 100km/s 100km/s 100km/s iew On ly 0 10 Ac 10 ev ZGSE(RE) 0 rR ce ZGSE(RE) Fo 20 0 10 XGSE(RE) (a) 20 0 (b) 10 20 XGSE(RE) 0 (c) 10 20 XGSE(RE) Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english 20 10 pt 10 ed Timing results MDD & STD results YGSE(RE) 20 YGSE(RE) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 SCIENCE CHINA Technological Sciences 0 (d) 10 20 XGSE(RE) 20 2.5 2.0 1.5 1.0 0.5 ed 160 140 1 For 120 Rev iew B, U 3.0 1 pt 3.5 Timing results MDD & STD results ce 4.0 Page 24 of 41 180 Ac 4.5 Size (RE) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 SCIENCE CHINA Technological Sciences 100 Timing results MDD & STD results O80n 60 ly 1 1 40 (a) 0.0300 250 200 150 100 50 0 50 100 Velocity of cavitons in the solar wind frame (km/s) 20 00 (b) 2 Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english 4 6 8 Series number 10 12 Page 25 of 41 Propagation properties of foreshock cavitons: Cluster 2 observations 3 WANG MengMeng1,2, YAO ShuTao1, SHI QuanQi1*, ZHANG Hui3, TIAN AnMin1, 4 DEGELING Alexander William1, ZHANG Shuai1, GUO RuiLong4, SUN WeiJie5, 5 LIU Ji2, BAI ShiChen1, SHEN XiaoChen1, ZHU XiaoQiong1, FU SuiYan6, PU 6 ZuYin6 7 1School 8 2National 9 3Geophysical 10 11 12 4Institute 5Department Space Science Center, Chinese Academy of Sciences, Beijing, 100190, China Institute, University of Alaska Fairbanks, Fairbanks, Alaska, 99775, USA of Geology and Geophysics, Chinese Academy of Sciences, Beijing, 100029, China of Space Physics and Applied Technology, Peking University, Beijing, 100871, China *Corresponding author (email: sqq@sdu.edu.cn) Abstract rR 14 of Space Science and Physics, Shandong University, Weihai, 264209, China of Climate and Space Sciences and Engineering, University of Michigan, Ann Arbor, 48113, USA 6Institute 13 pt ed 1 Fo 15 Foreshock cavitons are transient phenomena observed in the terrestrial foreshock region. 16 They are characterized by a simultaneous depression of magnetic field magnitude and plasma 17 density, which are bounded with enhancements of these two parameters and surrounded by ultra 18 low frequency (ULF) waves. Previous studies focused on the interplanetary magnetic field 19 (IMF) conditions, solar wind (SW) conditions, and the growth of the foreshock waves related 20 to the generation of foreshock cavitons. Previously, a multipoint spacecraft analysis method 21 using Cluster data was applied to analyze only two foreshock cavitons, and this method did not 22 consider uncertainties. In this study, multipoint spacecraft analysis methods, including the tim- 23 ing method, the Minimum Directional Difference (MDD) method, and the Spatiotemporal Dif- 24 ference (STD) method are applied to determine the velocity in both spacecraft and solar wind 25 frames. The propagation properties show good agreement with previous results from simula- 26 tions and observations that most cavitons move sunward in the solar wind frame, with the ve- 27 locities larger than the Alfvén speed. The propagation properties of foreshock cavitons support 28 the formation mechanism of cavitons in previous simulations, which suggested that cavitons 29 are formed due to the nonlinear evolution of compressive ULF waves. We find that there is 30 clear decreasing trend between the size of cavitons and their velocity in the solar wind frame. 31 In addition, the timing method considering errors has been applied to study the evolution prop- 32 erties by comparing the velocities with errors of the leading and trailing edges, and we identify 33 three stable cavitons and one contracting caviton, which has not been studied before. Most 34 cavitons should remain stable when they travel toward the Earth’s bow shock. The relationship 35 between the size of foreshock cavitons and their distance from the bow shock is also discussed. iew Ac ce ev ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences 36 Key words foreshock transient phenomena, cavitons, nonlinear evolution of ULF waves, prop- 37 agation and evolution properties of structures, multipoint spacecraft methods 38 1 Introduction When the supermagnetosonic magnetized solar wind encounters the Earth’s magnetosphere, 40 the bow shock forms. The nature of the bow shock depends on the angle 𝜃𝐵𝑛 between the 41 interplanetary magnetic field (IMF) and the shock normal [1]. The shock is either quasi-parallel 42 (𝜃𝐵𝑛 < 45°) or quasi-perpendicular (𝜃𝐵𝑛 > 45°) . The foreshock, located upstream of the 43 quasi-parallel shock and the “shock foot” of the quasi-perpendicular shock [2] [3] [4], is popu- 44 lated with particles backstreaming from the bow shock, ULF waves [5][6] [7][8], hot flow 45 anomalies (HFAs) [9], spontaneous hot flow anomalies (SHFAs) [10] [11], and foreshock cav- 46 ities [12] [13]. These transients can modify the solar wind before they encounter the bow shock. 47 Global hybrid simulations performed by Omidi [14] and Blanco-Cano et al. [15] [16] sug- 48 gested that a new category of transient structure called foreshock caviton exist in the foreshock 49 region. Foreshock cavitons are transient phenomena as common as HFAs and SHFAs in the 50 foreshock region, which saturate at a width of several 𝑅𝐸 , with a depressed core plasma density 51 and magnetic field strength bounded by a rim of enhanced plasma density and magnetic field 52 strength [14] [15] [16]. Cavitons are not associated with IMF discontinuities, and there is no 53 plasma heating or flow deflection inside the structures, which is in contrast to HFAs. Omidi et 54 al. [14] referred to cavitons as ‘foreshock cavities’ in their simulation of formation of foreshock 55 cavitons. However, foreshock cavitons are always embedded in a sea of ULF waves, which is 56 in contrast to other isolated cavities with no ULF waves nearby. Diffuse ions are found inside 57 and outside foreshock cavitons, while diffuse ions are only found inside foreshock cavities. 58 Schwartz et al. [13] suggested foreshock cavities are formed by thermal expansion because of 59 the magnetic field in cavities connected to the bow shock, which contrasts with notion that the 60 wave interactions generate foreshock cavitons. Hence, Blanco-Cano et al. [15] [16] used the 61 term, foreshock cavitons, to describe these new structures. pt ed 39 iew Ac ce ev rR Fo ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 26 of 41 62 The interaction of ULF waves in the foreshock contributes to the formation of foreshock 63 cavitons. Under the condition of radial IMF, the foreshock region is permeated by parallel prop- 64 agating sinusoidal fluctuations with right- or left-hand circular polarization, and fast, linearly 65 polarized, oblique (FLO) waves. The nonlinear evolution of these two types of ultra-low fre- 66 quency (ULF) waves generates foreshock cavitons [14] [15][16]. Global hybrid simulations 67 performed by Blanco-Cano et al. [16] showed that foreshock cavitons could exist under a wide 68 range of IMF [17] [18] orientations depending on the Mach number. They found that major 69 features of foreshock cavitons do not vary with the IMF orientation. Statistical studies of fore- 70 shock cavitons [20] [21] have shown that foreshock cavitons are observed for a wide range of 71 IMF orientation and SW conditions. The time duration of cavitons is 65s and the size is 4.6𝑅𝐸 72 on average. Inside cavitons, the variations of plasma density and magnetic field magnitude are Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 27 of 41 73 highly correlated. The foreshock-bow shock system is a significant region for the solar wind-magnetosphere 75 coupling process. There are a plethora of multi-scale plasma physics processes and phenomena 76 in foreshock, making it an important and excellent laboratory to study plasma physics. The 77 generation and evolution of foreshock cavitons are an intrinsic process of the foreshock-bow 78 shock system and play a considerable role in reformation of the system. Hybrid simulations 79 suggest that the interaction between foreshock cavitons and the bow shock generate another 80 transient phenomenon, namely, SHFAs [10][11]. Several cavitons even generate complicated 81 and large structures if they arrive at the bow shock at the same time. They play an important 82 role in the deformation of the bow shock and can lead to ripples on the surface of bow shock. 83 Cavitons may lead to disturbances in the magnetosheath and surface waves on the magneto- 84 pause [10] [11] [22] [23] [24]. Considering the magnetospheric response [25], foreshock cavi- 85 tons are no less important than foreshock transients such as HFAs with large dynamic pressure 86 pulses [26] [27]. Given that cavitons exhibit similar sudden dynamic pressure decreases, cavi- 87 tons may generate ULF waves in the magnetosphere [28] [29] [30] [31] [32] and drive magne- 88 tospheric vortices [33]. Foreshock cavitons may evolve into SHFAs, which can make the 89 plasma more inhomogeneous and contribute to the formation of magnetosheath jets [34] and 90 magnetosheath filamentary structures (MFS) [35]. Successive expansion and contraction of the 91 magnetosphere caused by SHFAs are significant, which may excite ULF waves in the inner 92 magnetosphere [36] [37] [38] [39] [40] [41]. pt ed 74 iew Ac ce ev rR Fo 93 As foreshock cavitons form, they are convected by the solar wind towards the bow shock. 94 Blanco-Cano et al. [16] found that cavitons propagate sunward in the solar wind frame, as 95 weakly compressive waves. In their simulations, the velocity of the example caviton in the solar 96 wind frame is 98 km/s, which equals 1.9 𝑉𝐴 [16]. Kajdič et al. [19] analyzed two foreshock 97 cavitons observed by the multi-spacecraft Cluster mission. The two cavitons propagate sunward 98 in the solar wind frame at a speed of 188 km/s and 120 km/s. However, only the timing method 99 without calculating errors has been applied to calculate the velocities of these two cavitons [19]. 100 Although theories and simulations provide the formation conditions and the evolution of fore- 101 shock cavitons, no observations of the evolution of foreshock cavitons have been reported. ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences 102 In this paper, we perform a study of the propagation properties of a series of foreshock cavi- 103 tons using several multipoint spacecraft analysis methods, including the timing method [42], 104 the Minimum Directional Derivative (MDD) method [43] and the Spatiotemporal Difference 105 (STD) method [44]. Four cavitons with both velocities of leading edge and trailing edge con- 106 sidering errors are classified into three stable structures and one contracting structure. We also 107 examine the possible relationship between the size of foreshock cavitons and the distance from 108 cavitons to the bow shock. 109 2 Data and Methods Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences 110 2.1 Data and Event Selection 111 Cluster mission consists of four identical spacecraft (C1, C2, C3, C4). We obtain the mag- 112 netic field data with 0.2s resolution from the Fluxgate Magnetometer (FGM) [45] [46] [47] 113 onboard all four spacecraft, and we obtain the ion data with 4s resolution from the Hot Ion 114 Analyzer (HIA) of the Cluster Ion Spectrometer (CIS) [48] on C1. We obtain the solar wind 115 and IMF data with 1-min resolution from the OMNI database, which indicate parameters near 116 the nose of the Earth’s bow shock. All foreshock caviton events analyzed here are taken from [20], which presented 92 fore- 118 shock cavitons selected using C1 data from 2001 to 2006. Firstly, foreshock cavitons observed 119 by all four Cluster spacecraft are selected. Then, we select the cavitons with clear leading and 120 trailing boundaries and with the similar profiles observed by four spacecraft. Following these 121 criteria, twelve foreshock cavitons are selected and their propagation properties are investi- 122 gated. Further criteria, including the shape parameters of the tetrahedral spacecraft configura- 123 tion can improve the precision of the timing analysis, MDD analysis, and STD analysis. 124 2.2 Timing method pt ed 117 rR Fo 125 The timing method has been widely applied to determine the velocity and normal direction 126 of shocks, magnetic holes, magnetic peaks, and HFAs [42] [49] [50] [51] [52] [53]. To calculate 127 the velocities and normal of the boundaries of foreshock cavitons, we apply a similar method 128 by analyzing magnetic field data detected by four Cluster spacecraft [54] [55]. By solving the 129 following equation, iew Ac ce ev 130 𝑈(𝑡𝑖 − 𝑡𝑗 ) = (𝑟⃗𝑖 − 𝑟⃗𝑗 ) ∙ 𝑛⃗⃗, 131 the unit normal direction 𝑛⃗⃗ and velocity magnitude U of the foreshock caviton leading and 132 trailing boundaries are obtained. Here, ∆𝑡 = 𝑡𝑖 − 𝑡𝑗 is the time lag between two spacecraft 133 observing the same boundary, and 𝑟⃗𝑖𝑗 = 𝑟⃗𝑖 − 𝑟⃗𝑗 is their corresponding difference in position 134 vectors. As Cluster mission consists of four spacecraft, three differences in position vectors, 135 𝑟⃗12 , 𝑟⃗13 , 𝑟⃗14and three time lags, ∆𝑡12 = 𝑡1 − 𝑡2 , ∆𝑡13 = 𝑡1 − 𝑡3 , ∆𝑡14 = 𝑡1 − 𝑡4 are determined. 136 Furthermore, we estimate the uncertainty of velocity magnitude and normal direction according 137 to [54]. An empirical relative error of time lag is δt = 0.1∆t . As the relative uncertainty of 138 the distance between satellites is 0.01, the time lag uncertainty contributes more to the error of 139 results and is considered dominant. A pair of satellites can give an interval [∆t − δt, ∆t + δt]. 140 The interval is divided into 11 equidistant points. In total 113 calculations of velocity and normal 141 are given due to three time intervals determined by four satellites. The mean velocity and nor- 142 mal are given and the standard deviations estimate the uncertainty. (1) ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 28 of 41 143 2.3 The MDD method 144 The Minimum Directional Derivative (MDD) method is a dimensionality determination Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 29 of 41 technique with the help of multipoint measurements described by Shi et al. [43]. The eigenval- 146 ⃗⃗)(∇𝐵 ⃗⃗)𝑇 indicate the dimensionality and the principal direcues and eigenvectors of L = (∇𝐵 147 tions of the structure (where T denotes the transposition). Three directions corresponding to 148 the maximum, intermediate and minimum variations of magnetic field are determined straight- 149 forwardly by the MDD method, which can help us investigate the time variation of a structure’s 150 characteristic direction. It is proved that the MDD method is feasible for the determination of 151 the normal direction of 1-D structures including magnetic holes [50] [51] [56], and magnetic 152 peaks [52]. pt ed 145 153 2.4 The STD method 154 The Spatiotemporal Difference (STD) method [44] can be applied to calculate the velocity 155 of quasi-stationary structures in any dimensionality using multipoint magnetic field measure- 156 ments. Further, we can resolve time-variations of the velocity from the STD results. By esti- 157 ⃗⃗, the vemating the time variation of the magnetic field and the magnetic gradient tensor ∇𝐵 158 ⃗⃗𝑠𝑡𝑟 , is obtained from the equation of locity of the structure in the spacecraft frame, 𝑉 159 ⃗⃗ = 0. ∇𝐵 160 3 Propagation and evolution properties of foreshock cavitons ⃗⃗𝑠𝑡𝑟 ∙ +𝑉 iew Ac ce Propagation properties ⃗⃗ 𝜕𝐵 𝜕𝑡 ev 3.1 rR 161 Fo 162 3.1.1 Timing analysis 163 Timing method is applied to calculate the velocity of foreshock cavitons in the spacecraft 164 and the solar wind frames. Here, the GSE coordinate system is used. We obtain the velocity of 165 foreshock cavitons in the solar wind frame from 166 𝑉 = 𝑈 − 𝑣⃗𝑠𝑤 ∙ 𝑛⃗⃗. On (2) 167 Here U is the velocity of caviton in the spacecraft frame obtained from the timing analysis, 168 as before. U is along the normal direction, 𝑛⃗⃗. The average value of the solar wind velocity 169 measured by CIS-HIA over a 10 minute interval including the cavitons is used to eliminate 170 fluctuations. In accordance with [48], an uncertainty in the solar wind velocity 𝑣⃗𝑠𝑤 of 10% in 171 magnitude and +/-5° in direction are considered. We carried out four timing calculations and 172 considered all four calculations to generate our results, including velocities, normal directions 173 and uncertainty estimates, represented as error bars in Figure 4. If the error bar crosses zero, 174 the caviton is probably stationary with respect to the solar wind. Examples of timing analysis 175 are shown in Figure 1. Figure 1(a-d) show the results for the leading boundary, and figure 1(e- 176 h) show the results for the trailing boundary. The mean speed of the leading boundary in the 177 spacecraft frame is 98.6 km/s and the uncertainty is 4.1 km/s as shown in Figure 1b. The average 178 velocity of leading boundary in the solar wind frame is −219.2 ± 32.9km/s along 𝑛⃗⃗𝐿 = 179 (−0.97, 0.14, 0.17) with uncertainty of 1.8°. Figures 1e-1h show the detailed velocity of the 180 trailing boundary with 𝑉𝑇 = −212.7 ± 33.7 𝑘𝑚/𝑠 𝑎𝑛𝑑 𝑛⃗⃗ 𝑇 = (−0.93,0.18,0.33) . Magnetic ly 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences 181 field data with different resolutions were employed to check the reliability of the results. The 182 results agree with those using data with 0.2 s cadence. The velocity with error not including 183 zero shows that the caviton is moving in the solar wind plasma. 3.1.2 MDD and STD analysis 185 Here, we apply the MDD and STD methods to calculate the dimensionality and velocity 186 vector and compare the results with those from the timing method. The analysis results of the 187 same case shown in Figure 1 are shown in Figure 2. As the MDD method suggested, the relative 188 size of the three eigenvalues indicate the dimensionality information of the structure. If 𝜆1 ≫ 189 𝜆2 , 𝜆3 ,we can regard the structures as quasi-1D, and 𝜆1 is the eigenvalue of the maximum 190 variant direction of the magnetic field. The maximum variant direction 𝑛⃗⃗1 represents the nor- 191 mal of the boundary of foreshock caviton. The ratio of the average 𝜆1 and 𝜆2 in the limited 192 period indicated by orange shadow is 8.7 for the leading boundary. For the trailing boundary, 193 the ratio in the limited period indicated by the blue shadow is 19.6. Therefore, we regard this 194 caviton as quasi-1D structure. pt ed 184 rR Fo 195 The propagation velocity of the leading boundary in the solar wind frame is -219.3 km/s 196 along 𝑛⃗⃗𝐿 = (−0.88, −0.29, 0.37)and for trailing boundary, the velocity is -222.0 km/s along 197 𝑛⃗⃗ 𝑇 = (−0.96, −0.27, 0.02). Here, L denotes the leading boundary and T denotes the trailing 198 boundary. These results fall within the velocity error from timing method as shown in Figure 199 4(a). Statistical results iew Ac ce ev 200 3.1.3 201 The propagation velocity along the normal of the foreshock cavitons are given by equation 202 (2). The velocity vector of the cavitons in the spacecraft frame is equal to U multiplied by 𝑛⃗⃗, 203 while the velocity vector of the cavitons in the solar wind frame is equal to V multiplied by 𝑛⃗⃗. 204 Velocity magnitudes and directions of the twelve foreshock cavitons calculated by timing, 205 MDD and STD methods are plotted in GSE-XY and GSE-XZ planes. Velocity vectors in both 206 the spacecraft frame and the solar wind frame are plotted in Figure 3. In the spacecraft frame, 207 foreshock cavitons are moving towards the Earth. Eleven cavitons are propagating sunwards in 208 the solar wind frame, which is consistent with previous observations [19] and the predictions 209 of simulations [16]. Another caviton observed on Mar 26, 2005 has a velocity in the solar wind 210 frame that is close to zero, for which the error bar crosses zero. ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 30 of 41 211 Sizes of foreshock cavitons are calculated using both the timing velocities and STD veloci- 212 ties in the spacecraft frame. As foreshock cavitons propagate in the solar wind frame, we esti- 213 mate the spatial extents of the cavitons by multiplying their speed in the spacecraft frame by 214 their durations, rather than multiplying their durations by the solar wind velocity [20]. Since 215 foreshock cavitons remain stable when they travel towards the bow shock, the velocities of one 216 boundary are used to calculate the extents of cavitons. Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 31 of 41 217 Figure 4 (a) shows a plot of the estimated size in RE of foreshock cavitons against their 218 propagation velocity in the solar wind frame. This figure shows the trend that smaller foreshock 219 cavitons have significantly higher velocity than larger ones in the solar wind frame. 220 normal of one edge of foreshock cavitons is obtained from the timing method and MDD & STD 221 method, we calculate the angle between the normal direction and the ambient magnetic field 222 vector. This indicates the direction of propagation for a 1-D structure [43] [44]. The results are 223 shown in Figure 4 (b). The average magnetic field value over a 10 minute interval excluding 224 the cavitons is used. We can see that the foreshock cavitons are propagating along the parallel 225 or anti-parallel direction. These results are obtained using two independent techniques (timing 226 and MDD and STD analysis as described above), with both techniques revealing the same trend. pt ed Since the 227 3.2 Evolution of foreshock cavitons 228 Here we show a stable caviton structure observed on 16 February 2002 by comparing the 229 velocities with errors of the leading edge and the trailing edge. The detailed process is as fol- 230 lows. The timing analysis shows that the leading edge travels at a speed of about −219.2 ± 231 32.9 km/s along the direction n ⃗⃗L = (−0.93, 0.14, 0.17) in the solar wind, while the trailing 232 edge moves at a speed of about −212.7 ± 33.7km/s along the direction n ⃗⃗T = 233 (−0.93, 0.18, 0.33) in the solar wind frame. Here, L denotes the leading boundary and T de- 234 notes the trailing boundary as before. We calculate the difference of velocities between the 235 leading boundary and trailing boundary by projecting the trailing boundary velocity to the nor- 236 mal of the leading boundary and subtracting the leading boundary velocity magnitude: 237 ∆V = |𝑉𝑇 𝑐𝑜𝑠𝜃𝑛⃗⃗𝐿,𝑛⃗⃗𝑇 − 𝑉𝐿 | 238 where θn⃗⃗L,n⃗⃗T is the angle between the normal of the leading edge and trailing edge. As ∆V = 239 9.3km/s < σL + σT = 32.9 + 33.7 = 66.6km/s, we conclude that the leading edge and the 240 trailing edge of the caviton move at velocities that are indistinguishable given the error esti- 241 mates of the measurements. Consequently, the caviton can be regarded as a stable structure as 242 suggested in Xiao et al [53]. iew Ac ce ev rR Fo (3) ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences 243 Only four out of twelve cavitons have usable timing velocities considering errors of both the 244 leading boundary and trailing boundary, and we investigate the evolution properties of these 245 four cavitons. Three cavitons are stable, and only one shows property of contraction. Our results 246 indicate that cavitons remain stable when they are convected toward the bow shock. 247 4 Summary and Discussions 248 By using the timing method, MDD and STD method, we analyze the propagation and evo- 249 lution properties of twelve foreshock cavitons. We find that all cavitons move earthward in the 250 spacecraft frame and the normal of the edge of cavitons are nearly parallel or anti-parallel to 251 the ambient magnetic field. The velocities of cavitons in the solar wind frame are also calculated. Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences Eleven cavitons of all cavitons move sunward in the solar wind frame. These results are con- 253 sistent with previous ones from simulations and observations. We also find that the caviton 254 observed on March 26, 2005 has features consistent with those of a mature caviton structure. 255 We find a clear decreasing trend between foreshock caviton size and their propagation velocity 256 in the solar wind frame. As for the evolution properties, the results suggest that most foreshock 257 cavitons remain stable when they propagate towards the bow shock. We find that there is no 258 clear correlation between the size of foreshock cavitons and their distance from the bow shock. 259 In the simulation of [16], one caviton moves upstream in the solar wind frame at a speed of 260 1.9 times of the Alfven speed. By Cluster observations, Kajdič et al. [19] found that two cavi- 261 tons move at 188 km/s and 120 km/s towards the sun in the solar wind frame. We have also 262 found that foreshock cavitons have a variety of propagation velocities, which is consistent with 263 simulation [16]. The nature of ULF waves and the nonlinear evolution of the waves contribute 264 to the propagation properties of cavitons. Weakly compressive waves propagate upstream in 265 the reference frame of background plasma, which is similar to the propagation direction of 266 cavitons. The normal of the edge of cavitons are nearly parallel or anti-parallel to the ambient 267 magnetic field, which suggests that parallel propagating weakly compressive waves are neces- 268 sary for the generation of foreshock cavitons. Consequently, the propagation properties imply 269 that foreshock cavitons form due to the nonlinear evolution of circularly polarized, parallel 270 propagating ULF waves and compressive, linearly polarized, oblique ULF waves. We find that 271 in all but one case, foreshock cavitons propagate sunward, and their speed can be shown to be 272 larger than the Alfvén speed. Previous results from simulations and observations have found 273 sunward propagating foreshock cavitons with speeds greater than the Alfvén speed. We appear 274 to have found one counter-example. pt ed 252 iew Ac ce ev rR Fo On 275 For the caviton observed on Mar 26, 2005, the uncertainty in its velocity in the solar wind 276 frame is greater than its magnitude – in other words it has an error bar across zero. In this case 277 we consider that it is likely that the caviton is stationary with respect to the solar wind, however 278 the size of the uncertainty in velocity for this event is significant; on the order of the Alfven 279 speed. Compared to other cavitons in our study, this event is observed within a higher speed 280 solar wind (larger than 600 km/s) and lower plasma density (less than 3 cm-3) environment. 281 This caviton does not show a double peak internal structure [19]. There are few small fluctua- 282 tions or high-frequency waves in the interior, and the profile of magnetic field magnitude is 283 similar to that of plasma density. Blanco-Cano et al. finds that the width of cavitons should 284 increase slightly during their evolution [16], and that towards the end of their evolution, the 285 profiles of magnetic field magnitude and density should become similar. Therefore, this caviton 286 appears to be a mature structure with fewer wave features compared to the newly generated 287 cavitons, possibly because these fluctuations have dissipated over time in this case. 288 ly 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 32 of 41 The correlation between the size of foreshock cavitons and their velocity in the solar wind Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 33 of 41 frame shows that the bigger scale the foreshock caviton has, the slower it moves in the solar 290 wind flow. There is clear decreasing trend between the size of foreshock cavitons and their 291 velocity in the solar wind frame. It is reasonable to expect that, although the structures were 292 found to be 1-D based on the scale-size of the Cluster satellite configuration, they may be at 293 least 2-D on a larger scale. If we assume that they have roughly the same shape, then size 294 measurements we have obtained are a proxy for their scale size. A structure of a given size 295 propagating with respect to the solar wind will be subject to an effective drag force that in- 296 creases with the structure’s size (which can be calculated by integrating the total pressure forces 297 around the structure). This may make the larger cavitons more easily be slowed down in the 298 solar wind plasma frame, explaining our observations. pt ed 289 299 We studied the propagation properties of foreshock cavitons, which are similar to the propa- 300 gation properties of solitary waves reported in [50] [59]. Both cavitons and solitary waves are 301 fast-mode structures/waves, and they propagate in the background plasma frame. However, the 302 size of foreshock cavitons exceeds tens to several hundred ion gyroradii and there is no corre- 303 lation between the propagation velocity in solar wind and the velocity of fast magnetosonic 304 waves. Therefore, foreshock cavitons do not correspond to these kinds of solitary waves. ev rR Fo Among the four foreshock cavitons in our study, three cavitons are stable and one is con- 306 tracting, indicating these are mature or near mature structures. The mature foreshock cavitons 307 are structures with a high correlation between the decrements in density and magnetic field 308 magnitude [20]. Due to the enhancement of the pressure of suprathermal ions, the total pressure 309 inside and outside foreshock cavitons is very similar, [16] [19] and the cavitons can maintain 310 equilibrium. However, when the cavitons are steepening and evolving, their sizes evaluated 311 from the density profile become larger as the structures will expand. These cavitons cannot be 312 selected using rigorous criteria [20] and we are still unable to diagnose their evolution from 313 generation to maturity using spacecraft data. iew Ac ce 305 ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences 314 We find that there is no clear correlation between the size of foreshock cavitons and their 315 distance from the bow shock, which may be due to the origin of foreshock cavitons and their 316 evolution properties. The bow shock model presented in [54] [55] [56] under the corresponding 317 IMF and solar wind conditions is used to calculate the distance from the cavitons to the bow 318 shock. Hybrid simulations have shown that foreshock cavitons can appear in a broad area of 319 the ion foreshock [16] and be carried by the solar wind toward the bow shock. The foreshock 320 region is populated by the weakly compressive waves generated by field-aligned ions [63]. Fast, 321 linearly polarized, oblique waves will grow significantly on the condition that the backstream- 322 ing ions are cold. The density striations in the perpendicular direction caused by waves are 323 essential for the formation of foreshock cavitons. The nonlinear interaction of the two kinds of 324 waves generates foreshock cavitons. The process does not need a trigger and can be generated Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences self-consistently around the bow shock, which is an intrinsic process in foreshock region. Fore- 326 shock cavitons will not disappear on the way to the bow shock. The evolution properties in our 327 study show that cavitons will not expand or contract, instead, caviton width will change only 328 slightly when they are carried toward the bow shock. The width of cavitons depends on their 329 initial size. Therefore, the relationship between the size of cavitons and their distance from the 330 bow shock is not clear. On the other hand, even if foreshock cavitons will expand or contract 331 during their travel toward the bow shock, we cannot obtain the correlation between the size of 332 foreshock cavitons and their distance from the bow shock, as cavitons can be observed on their 333 way to the bow shock and their evolution stages are different from one-another. pt ed 325 334 As hybrid simulations performed by Omidi et al. [10] suggested that SHFAs form due to the 335 interaction between foreshock cavitons and the bow shock, more work is required to understand 336 the relation between foreshock cavitons and SHFAs. Using high-resolution plasma data from 337 the Magnetospheric Multiscale (MMS) mission, the particles properties inside foreshock cavi- 338 tons can be analyzed. 339 Acknowledgments We acknowledge the Cluster Team for providing data. All Cluster data is 340 obtained from the Cluster Science Archive (http://www.cosmos.esa.int/web/csa/). We also 341 acknowledge NASA's Space Physics Data Facility (SPDF) for providing OMNI data 342 (https://omniweb.gsfc.nasa.gov/). This work was supported by the National Natural Science 343 Foundation of China (grants 41574157, 41628402, and 41774153), and Hui Zhang is partially 344 supported by NSF AGS-1352669. 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Zhang H, Khurana K K, Kivelson M G, et al. Three-dimensional lunar wake reconstructed from ARTEMIS data. J. Geophys. Res. Space Physics, 2014, 119: 5220–5243 63. Sun W J, Fu S Y, Parks G K, et al. Field-aligned currents associated with dipolarization fronts. Geophys. Res. Lett., (2013),40: 4503-4508 Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english iew Ac ce ev rR Fo 504 On 505 Figure 1 Timing analysis results for one typical foreshock caviton. The left four panels (a-d) are for the 506 leading boundary, and the right four panels (e-h) are for the trailing boundary. Four different magnetic 507 field magnitudes marked by the four colored horizontal lines in Figures 1(a) are used to determine the 508 time when the spacecraft crossed the caviton, corresponding to the different histograms of the same color 509 in Figures 1b-1d. The magnetic field observed by the Cluster spacecraft (Figure 1a). And the black, red, 510 green, and blue curve denotes Cluster 1, 2, 3, 4, respectively. Histograms of the velocities of the boundary 511 in the spacecraft frame (Figure 1b). Histograms of the velocities in the solar wind frame (Figure 1c). 512 Histograms of angles between any two normal vectors of leading boundary (Figure 1d). And the ultimate 513 results of velocity, normal and their uncertainty considering four calculations are written in bold in every 514 subgraph. Figures 1e-1h are results for the trailing boundary of this caviton, and the formats are the same 515 as in Figures 1a-1d. ly 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences pt ed Page 39 of 41 516 Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english 517 518 ev rR Fo Figure 2 MDD and STD analysis result: (a) magnetic field magnitude in GSE coordinates. (b) eigenvalues 𝜆1 , 𝜆2 , 𝑎𝑛𝑑 𝜆3 . (c) normal along the maximum derivative direction of magnetic field. (d) velocity 520 along the maximum direction. The red shadowed area indicates the leading edge, while the blue shad- 521 owed area is the trailing edge. 522 iew Ac ce 519 ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 40 of 41 pt ed SCIENCE CHINA Technological Sciences Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english Page 41 of 41 pt ed 523 rR Fo 524 525 Figure 3 Distribution of foreshock cavitons in GSE XY and XZ plane, with velocity vector in 526 the spacecraft frame (a and b) and in the solar wind frame (c and d). GSE coordinate syste m is used. The azure arrows denote the timing results, and the pink arrows denote the MDD Ac ce 527 ev and STD results. A bow shock model presented by Chao et al.[60] is used, under typical solar 529 wind condition s (𝐵𝑍 = −0.35𝑛𝑇, 𝐷𝑝 = 2.48𝑛𝑇, 𝑀𝑚𝑠 = 6.96, 𝑎𝑛𝑑 𝛽 = 2.08). The green curve iew 528 530 denotes the nominal bow shock. The caviton observed on Mar 26, 2005 is marked by a 531 black solid dot. 532 ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 SCIENCE CHINA Technological Sciences Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english SCIENCE CHINA Technological Sciences pt ed 533 534 Fo 535 Figure 4 (a) The size of foreshock cavitons versus their propagation velocity of foreshock cavitons in 536 the solar wind frame. The X axis shows the velocity from the timing or the MDD and STD methods in 537 the solar wind frame, and the Y axis denotes the size of foreshock cavitons. The blue horizontal and 538 vertical lines denote error bars. (b) The angle between the normal direction of the boundary of foreshock 539 cavitons and the ambient magnetic field. The caviton observed on Mar 26, 2005 is marked as ’1’. 540 In both plots, the blue thin diamonds denote the timing result, while the pink asterisks denote the MDD 541 542 and STD results. iew Ac ce ev rR ly On 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 Page 42 of 41 Downloaded to IP: 192.168.0.24 On: 2019-03-25 08:44:28 http://engine.scichina.com/doi/10.1007/s11431-018-9450-3 http://tech.scichina.com/english