arXiv:2002.08794v1 [astro-ph.EP] 20 Feb 2020 xie ytersnne ni ls noneswt plane with encounters close resonanc until resonances into the ac pushed by excited widely are asteroids is e Yarkovsky belt it by mainly main Nowadays, the 1998). that al. cepted et (Farinella up brought e Yarkovsky 1998 until Gladman unsolved remained and disagreement (Morbidelli This meteorites ages CRE iron 199 the and al. with stony et inconsistent most is (Farinella e which years 1997), cosmic-ray million al. with few et a Gladman meteoroids of of ages fraction deli (CRE) large posure shall a mechanism co Earth by this the As- However, resonances to NEOs. other. into of each ejected source be with major to lisions thought the once be were to teroids considered is Jupiter a et and Bottke e.g. (see (NEOs) review). a a objects for members near-Earth 2006, family of asteroid of origin dispersion the the the as (1999), such Vokrouhlický aspects, by given model e Yarkovsky linear continuousl decrease complete or increase the to asteroid the e lead of accumulated axis pressure jor the radiation and net re- force, recoil the and rotatio tiny the asteroid, Sun of the Because the of while. from a revolution after radiation out energy the the receives radiates therma of asteroid re-radiation An anisotropic ergy. and absorption the from e Yarkovsky Introduction 1. fe J7 after edo Send eray2,2020 21, February Astronomy h 7 The Mars of orbits between in belt main the in zone resonant The h eoac n nteopst ieo h eoac ihr with resonance the of the side to opposite mainly the attributed on and is resonance it the and considerably, up pumped be n nlnto u otecmie nunefo ohtere the both from influence initi combined the the rate, to drifting Yarkovsky due the inclination on and depend to found are akvk e Yarkovsky ul uhdb akvk e Yarkovsky by pushed ously e words. Key discussed. simulat are numerical it of by asteroids results of our transportation using explained is members n seod.Tefato fatrista aesuccessf make that asteroids of fraction The asteroids. ing u oteisaiiyo Ms hyaecniee stepri the as considered are They e MMRs. the simulations of numerical instability the to due o aiyta eiersetvl nteinradotrsi outer and inner the on respectively reside that family Eos 3 2 1 4 ff / rn eussto requests print nttt fSaeAtooyadEtaersra Explora Extraterrestrial and Astronomy Space of Institute e aoaoyo oenAtooyadAtohsc nMini in Astrophysics and Astronomy Modern of Laboratory Key colo srnm n pc cec,NnigUniversity, Nanjing Science, Space and Astronomy of School nttt fAtooy ainlCnrlUiest,Jhon University, Central National Astronomy, of Institute M)i n fteipratrsnne ntemain the in resonances important the of one is MMR) 3 rni fatrisars h / ikodgpudrthe under gap Kirkwood 7/3 the across asteroids of Transit / enmto eoac MR ihJptr(here- Jupiter with (MMR) resonance motion mean 3 ff ff & c a enitoue oslepolm nmany in problems solve to introduced been has ect c rdcsanngaiainlfreta arises that force non-gravitational a produces ect Astrophysics ff c ly nipratrl natrisditn nteinne the in drifting asteroids in role important an plays ect eeta ehnc io lnt,atris eea m – general asteroids: planets, minor – mechanics celestial huL-. e-mail: L.-Y., Zhou : ff c,adltrterecnrcte a be may eccentricities their later and ect, aucitn.ResTran no. manuscript ff cso h 7 the of ects ff c norgoso di of regions into ect agB Xu Yang-Bo ff c rvstesemima- the drives ect z / [email protected] M ihJptr(J7 Jupiter with MMR 3 1 , akvk effect Yarkovsky 2 iYn Zhou Li-Yong , ff rn enmto eoacs(Ms n hneetdatra after ejected then and (MMRs) resonances motion mean erent ff c was ect .With y. lcosn hog h eoac n h saigrt from rate escaping the and resonance the through crossing ul oa to s and n eo h eoac.TeJ7 The resonance. the of de ts. en- l l,TounCt 20,Taiwan 32001, City Taoyuan gli, ABSTRACT in(J AT,NnigUiest,China University, Nanjing CAST), & (NJU tion liciainadtemgaigdrcin h excitation The direction. migrating the and inclination al ver sett h orsodn aiycnr.Teeitneof existence The centre. family corresponding the to espect os ial,terpeiheto seod nteJ7 the in asteroids of replenishment the Finally, ions. eoac.I h bevtoa aa aiymmesaeal are members family data, observational the In resonance. nd of x- es 3; l- ). l. oac n akvk e Yarkovsky and sonance - cplsuc fna-at bet.W netgt nthis in investigate We objects. near-Earth of source ncipal 6 ini vne ajn 106 China 210046, Nanjing Avenue, Xianlin 163 / M)o h rnpraino seod rmKrnsfamil Koronis from asteroids of transportation the on MMR) 3 tyo dcto,NnigUiest,China University, Nanjing Education, of stry it faot00 U(orulcýe l 06,teJ7 the 2006), al. et (Vokrouhlický AU 0.01 about of width a Ms oeatrismycostersnnewiesome J7 while The resonance the in. the trapped especially be cross resonances, may may by others asteroids modified Some Howev be MMRs. region. will non-resonant the migration in the axis semi-major in freely eimjrai)adEsfml ntergthn side. hand right Eos the smaller of J7 simulations on (with few the a transiting side family made asteroids have hand Eos (2006) al. left and et Vokrouhlický the axis) on semi-major family Koronis namely eod nteJ7 found so the Kirk- of 1991) in behaviours the (1989, teroids chaotic for Yoshikawa and variations responsible position. eccentricity and its large unstable around be gap to wood thought is MMR J7 l aygetyi h eoac.Ltr h eua resona secular the Later, resonance. the ν in greatly vary ily epme pt . tms.Tesrcueo h J7 the of structure The most. at regio 0.8 chaotic to this up in pumped asteroids be of eccentricity The region. ntelf adsd ftersnnei diint hs in those to addition in resonance members the Eos of few side a hand are there left that the showed on (2014) al. et Milani evn saslciebrirfrditn asteroids. drifting for barrier selective a as serving aepc sJptr(rStr)de,wr on nteregio the of overlapping in the found and were 1995), does, Morbidelli Saturn) and (or (Moons Jupiter as pace same ocuin,icuigta o aiycno xedt the to J7 extend the cannot of family side Eos other that including conclusions, a loivsiae yTiai ta.(03,adteinst the and again. (2003), confirmed al. was et ity Tsiganis by investigated also was etdsieishg re.Lctdat Located order. high its despite belt 1,2,3 5 / M nrdcscasta oiae h oini this in motion the dominates that chaos introduces MMR 3 and oa ytm ntemi et ayatrisaecontinu- are asteroids many belt, main the In System. Solar r w ao seodfmle eieaon h J7 the around reside families asteroid major Two A tos miscellaneous ethods: n igHe Ip Wing-Huen and , ff ce yteYrosye Yarkovsky the by ected ν 6 hr h eieino natri rcse tthe at precesses asteroid an of perihelion the where , / / M,btteecnrct i o necessar- not did eccentricity the but MMR, 3 M cslk eetv are omigrat- to barrier selective a like acts MMR 3 ff c sdsusd nyteecnrct can eccentricity the Only discussed. is ect / M.Hwvr h lsicto by classification the However, MMR. 3 / M n ie oequalitative some given and MMR 3 3 , 4 ff / c,a seodi bet drift to able is asteroid an ect, M ssc resonance, a such is MMR 3 a ril ubr ae1o 10 of 1 page number, Article 7 / 3 ≈ / M n the and MMR 3 2 feccentricity of eido time of period h resonance the . 5 Uadwith and AU 957 hs family these ofudin found so ae by paper
c S 2020 ESO and y ν / / MMR, 3 5 MMR 3 , eas- me ν can n 6 abil- nces and er, / 3 n A&A proofs: manuscript no. ResTran the resonance (see Section 4). Tsiganis et al. (2003) found that ing longitude of the ascending node Ω, argument of perihelion all asteroids in the J7/3 MMR have short dynamical lifetimes, ω and mean anomaly M, having not long-term influence on the ◦ ◦ so that there must be a continuous supplement of asteroids, for orbital evolution, are set arbitrarily Ω0 = 100 , ω0 = 274 and ◦ which they found that the diurnal Yarkovsky effect could provide M0 = 285 . a flux of members from both Koronis and Eos families enough In addition, to investigate the resonance transit in the oppo- for maintaining the population in the J7/3 MMR. site direction, we make other two sets of test particles labelled As more and more asteroids have been identified as mem- Korout and Eosin, which are the same as Korin and Eosout except bers of both families, it is desirable to revisit the transiting of for the initial semi-major axes. Korout and Eosin are placed at asteroids across the J7/3 MMR in greater detail, as a coherent a0 = 2.962AU and a0 = 2.948 AU, respectively. process, and in a full dynamical model. We report here our inves- The recoil force of Yarkovsky effect is dependent on a se- tigations on the transit of asteroids across the J7/3 MMR under ries of physical parameters, most of which have not been mea- the influence of Yarkovsky effect. The rest of this paper is orga- sured accurately yet. As a compromise, Yarkovsky effect is gen- nized as follows. In Sect.2, we introduce the dynamical model erally degenerated into an equivalent drift rate of semi-major and initial setting of the numerical simulations. In Sect. 3, the axisa ˙Y . For a “typical” asteroid at a = 2.9 AU with radius results of simulations will be presented. In Sect.4, we compare R = 1km and rotation period P = 8hrs, assuming typical pa- our results with observational data, and the supplement of aster- rameters as follows (Vokrouhlický et al. 2006): albedo p = 0.13, oids into the J7/3 MMR is discussed. And finally, conclusions thermal conductivity K = 0.005W/m/K, specific heat capacity 3 are summarised in Sect.5. C = 680J/kg/K, surface density ρs = 1.5g/cm , bulk density ρ = 2.5g/cm3 and spinning obliquity γ = 0◦, its Yarkovsky drift rate can be calculated,a ˙Y = 0.128 AU/Gyr (Xu et al. 2020; 2. Dynamical model with Yarkovsky force Zhou et al. 2019). The currently known smallest asteroids of To investigate the behaviour of asteroids transiting the J7/3 Koronis family and Eos family have radii of about 0.5km, i.e. MMR, we numerically simulate their orbital evolutions. The dy- half of the above mentioned example asteroid, whose Yarkovsky namical model adopted in our simulations consists of the Sun, all drifting thus will be twice quicker |a˙Y | = 0.256 AU/Gyr. Con- planets but Mercury and massless fictitious asteroids (test parti- sidering the uncertainties of parameters, the maximal drift rate may be larger than this value, while the minimum can be as cles). It is worthy to note that four terrestrial planets were gen- ◦ erally ignored in the study of dynamics of main belt asteroids small as 0 (e.g. if γ = 90 ). To make our simulations be able to (e.g. Tsiganis et al. 2003). We exclude only the innermost planet represent all possible situations, we set 8 different drifting rates Mercury in our model because its small mass and short orbital |a˙Y | = 0.02, 0.05, 0.08, 0.1, 0.2, 0.3, 0.4, 0.5 AU/Gyr. In general, period make its perturbation ignorable, and also to include Mer- most of asteroids affected by Yarkovsky effect will be in this do- cury requires much more computations. We adopt the zeroth cor- main of migration speed. rection of Mercury by adding its mass to the Sun. We adopt the Our aim is to investigate the orbital evolution of test par- Earth-Moon barycentre instead of the separate Earth and Moon ticles when they are crossing through the J7/3 MMR region as usual (e.g. Dvorak et al. 2012; Zhou et al. 2019). The initial under the influence of Yarkovsky effect, thus the timespan of orbits of the planets at epoch JD2457400.5 are derived from the our simulation T should be long enough to allow the migra- JPL’s HORIZONS system1(Giorgini et al. 1996). tion of asteroid into and out of the resonance to complete. How- To simulate the motion of asteroid members of both Koronis ever, asteroids may “wander” in the resonance for a while rather and Eos families near the J7/3 MMR, we generatetwo sets of test than cross it immediately without any hesitation. The time de- particles, one on the inner side of the resonance (ap < a7/3), and lay in the resonance can be estimated using the functional de- the other on the outer side. The inner set mimicking members of pendence of the trapping time in the resonance on |a˙Y | and the Koronis family is labelled Korin after Koronis hereinafter, and strength of the resonance as proposed by Milic´ Žitnik (2016); the outer set (with ap > a7/3) Eosout after Eos family by the same Milic´ Žitnik and Novakovic´ (2016), where the strength of J7/3 token. Each set includes 1000 test particles, and we will check MMR can be found in Gallardo (2006). After some attempts, we how they transit through the J7/3 MMR under the influence of finally set T = 0.02 AU/|a˙Y| empirically, which ensures that al- Yarkovsky effect. most all of test particles leave the resonance in the end in our The initial positions of these test particles are chosen care- simulations. We note that the integration time T for the adopted fully. A test particle too far away from the J7/3 MMR will waste |a˙Y | in this paper will be from 40Myr to 1Gyr. plenty of integration time on its way approaching to the reso- The software package Mercury6 (Chambers 1999), with an nance, while too close to the J7/3 MMR will miss the process of additional Yarkovsky force subroutine, is adopted to simulate the drifting into the resonance from the non-resonant region. After orbits. The hybrid integrator is used, which is basically a sym- some attempts, we set the initial semimajor axis a0 = 2.948 AU plectic integrator switching to Bulirsch-Stoer only during plan- for Korin and a0 = 2.962AU for Eosout. etary close encounters. The Yarkovsky force is included in the The proper eccentricities ep of Koronis family and Eos fam- subroutine mfo_user with the samemethodas Zhou et al.(2019). ily are both approximately in the range from 0.04 to 0.10. ◦ ◦ They have different proper inclinations ip, averagely 2 and 10 for Koronis and Eos family, respectively (Milani and Kneževic´ 3. Results 2003). Following the same strategy applied in Tsiganis et al. Yarkovsky effect (mainly the diurnal effect) may increase the (2003), we set the initial osculating eccentricities e0 randomly i = ◦ semi-major axis if the asteroid has a prograde rotation (the spin- vary from 0.08 to 0.14 and initial osculating inclinations 0 3 ◦ Kor i = ◦ Eos ning obliquity γ smaller than 90 ), or drive the asteroid toward for in and 0 11 for out. These numbers are used just to ◦ make the test particles have the same proper elements as the as- the Sun for the retrograde rotator (γ> 90 ). We simulate the out- ward migration and crossing of the J7/3 MMR for asteroids from teroids of these two families. The rest angular elements, includ- ◦ ◦ two sets of initial conditions Korin (i0 = 3 ) and Eosin (i0 = 11 ) 1 ssd.jpl.nasa.gov/horizons.cgi both from a0 = 2.948 AU. And other two sets Korout and Eosout
Article number, page 2 of 10 Xu, Zhou & Ip: Transit of asteroids across the 7/3 Kirkwood gap under the Yarkovsky effect
◦ ◦ both from a0 = 2.962 AU but with i0 = 3 and 11 respectively 3.1. Fraction of resonance crossing are for the inward migration and crossing of the resonance. A test particle should migrate 0.02AU at the end of our nu- In our simulations for four sets of initial conditions of test parti- merical integration if it did not feel any resistance. But the J7/3 cles, we record the number of orbits that have made successful MMR is able to trap asteroids (though temporarily), thus some crossing by the end of numerical integration, and we summarize test particles (in fact very few) might still stay in the resonance all the results in Fig. 2. Eight values of |a˙Y | from 0.02AU/Gyr to until the end of integration. For those not in the resonance, some 0.5AU/Gyr are adopted, as mentioned previously. The positive have been ejected from the neighbourhood via close encounters a˙Y for outward migration and negativea ˙Y for inward migration, with planets after their orbits were excited by the resonance, and and cases for two initial inclinations are plotted in the same fig- the rest of them cross the resonant region successfully and con- ure. tinue their migration. Generally we may tell whether an object is in the resonance 1.0 by checking the resonant angle, but for high-orderresonance like fit the J7/3 MMR in a complicated dynamical model,the critical an- fit ) 0.8 gle seldom keeps oscillating all along. Instead, we adopt an indi- ( rect method similar to that in Milic´ Žitnik and Novakovic´ (2016) to check if a test particle has crossed over the resonancesafely or 0.6 is still in the resonance. The key point of this method lies in the fact that the J7/3 MMR must modify the migration speed of test particles. We present in Fig.1 an example of the semi-major axis 0.4 evolution of a test particle to show our method of identifying the resonance crossing. 0.2 crossing fraction fraction crossing
a˙ Y = 0.5 AU/Gyr 2.975 0.0 0.0 0.1 0.2 0.3 0.4 0.5 0.6 |a˙ | (AU/Gyr) 2.970
Fig. 2. The crossing fraction against Yarkovsky drifting rate |a˙Y |. 2.965 Crosses and solid circles are for outward and inward migration respec- ◦ ◦ tively, while blue and red indicate initial inclination i0 = 3 and 11 . 2.960 Lines are fitting curves (see text). (AU) a
2.955 Apparently in Fig.2 the crossing fraction increases with in-
2.950 creasing |a˙Y |. Asteroids with large drifting rates cross the reso- nance easily, which is a foregone conclusion (Brož 2006). An-
2.945 other interesting feature in Fig. 2 is the different crossing frac- 0 5 10 15 20 25 30 35 40 t (Myr) tions for opposite migrating directions. The transiting from the outer side to the inner side of J7/3 MMR (of Eosout and Korout) is always easier than the inverse transiting (Eosin and Korin). Fig. 1. An example of resonance crossing. The black lines are piecewise The difference in crossing fraction of opposite directions for Ko- linear fitting to guide eyes. ronis family (low inclination) is much more significant than that for Eos family (high inclination). This difference is due to the As shown in Fig.1, three stages of evolution can be seen asymmetry of dynamical structure of J7/3 MMR (Tsiganis et al. clearly. When t . 11Myr before entering the resonance and 2003), and the degree of asymmetry is higher at low inclina- & t 24Myr after escaping from the resonance, averagely the tion (Korin and Korout) than that at high inclination (Eosin and semi-major axis drifting rate is just the given Yarkovsky drift- Eosout). Additionally, test particles at low inclination cross the ingratea ˙Y = 0.5 AU/Gyr, i.e. the migration is determined solely resonance more easily than those at high inclination, because by the Yarkovsky effect. While in between these two stages, the the dynamical structures of J7/3 MMR at different inclinations semi-major axis is nearly constant, implying that the J7/3 MMR are different (Tsiganis et al. 2003). takes control of the motion. The relationship between the crossing fraction α and the Therefore, we monitor the semi-major axis drifting rate in Yarkovsky drifting rate |a˙Y | can be numerically fitted using a our numerical simulations, and fit the time series of semi-major function as axis using the least squares method in a running window with width of 2Myr, which is 1/20 of the shortest integration time in C2 our simulations. The test particles always start to migrate at the α = C1 |a˙Y | + C3 , (1) given speeda ˙Y . Their migration will then be suppressed by the resonance after entering into the J7/3 MMR, in which the orbits might be excited and ejected. Except only a few ones staying in where Ck (k = 1, 2, 3) are pending constants. For a better vision, the resonance all along thereafter, most survivors from the J7/3 we plot in Fig.2 only the fitting curves for results of Korin and MMR will continue the migration at the same given speeda ˙Y . Eosout, which are two sets of test particles referring to the real As soon as the drifting rate was found to return back to the given asteroids of Koronis family and Eos family, respectively. Later in a˙Y , the test particle is considered to have successfully crossed this paper, these functional relationships will be used to estimate the J7/3 MMR. the supplement flux of family members into the J7/3 MMR.
Article number, page 3 of 10 A&A proofs: manuscript no. ResTran
3.2. Orbital Excitation tion of test particles in all our simulations. For asteroids success- fully crossing through the resonance, a statistical estimation of ff The orbits of asteroids may be excited by the combined e ects the variations of eccentricity and inclination can be obtained by ff of the resonance and the Yarkovsky e ect. Currently, some as- calculating the difference between the maximum and the min- / teroids have been found in the J7 3 MMR although it has been imum of the corresponding mean orbital element (∆e and ∆i) proven to be dynamically unstable. The orbital state of these as- during the evolution. The mean orbital elements are derived in a teroids is attributed to their sources and the excitation processes. running window with width of 0.2Myr. For those asteroids that Checking the orbital evolutions of test particles in the sim- failed to cross the resonance, being either trapped in or ejected ulations, we find that the objects that make successful crossing out of the resonance, in order to reveal the dynamical influences / ff through the J7 3MMRhaveverydi erent behaviours from those solely from the combined Yarkovsky effect and the J7/3 MMR, that fail to cross. Four randomly selected but typical cases of we should eliminate the part of excitation that attributes to close the evolutions of eccentricity and inclination are presented in encounters with planets. To do so, we expel the orbital evolution Fig.3, two for objects that successfully crossed the resonance, since a short period before the first-time-ever close encounter and other two for objects that failed to cross the resonance. As with a planet (defined as when the asteroid is within 3 Hill radii shown, for the former case, both the eccentricity and the incli- from the correspondingplanet), which is reported by the integra- nation are barely excited, but for the latter case the eccentricities tor package Mercury6. Then the ∆e and ∆i are calculated just as are evidently pumped up, especially during the late stage of the in the former case of successful crossing. We summarize the re- resonance regime. Seemingly, the inclinations increase consider- sults as follows and present as an example the case for the initial ably but this excitation is mainly due to close planetary encoun- set Kor in Fig. 4. ters after the objects have obtained the high eccentricity and left in the resonance. 1.0 failed to cross successfully crossed 0.8 successfully crossed 0.20 0.6 e 0.15 0.4 ∆
0.10 0.2 e 0.0 0.05 6 0.00
8 4 ◦
6 i 2 ) ∆
◦ 4 (
i 0 2 0.08 0.09 0.10 0.11 0.12 0.13 0.14 e 0 0 5 10 15 20 25 30 35 40 t (Myr) Fig. 4. The excitations of eccentricity ∆e (top) and inclination ∆i (bot- tom) against initial eccentricity e for initial set Kor . The Yarkovsky failed to cross in 1.0 drifting ratea ˙Y = 0.05 AU/Gyr. Green dots refer to test particles that successfully crossed through the J7/3 MMR, while red dots for those 0.8 that failed to. The dashed line represents the average value of red dots. 0.6 e 0.4 As shown in Fig. 4, the variations of eccentricity obviously
0.2 split into two distinct groups, one for test particles that success- fully crossed the J7/3 MMR and the other one for those failed. 0.0 In the former case, the excitation of eccentricity is less than 0.1, 40 while the eccentricities in the latter case increase by about 0.4 30 in average, with the maximal ∆e being larger than 0.7, which
) is consistent with the result in Moons and Morbidelli (1995). ◦ 20 (
i In these extreme cases, asteroids with eccentricity up to 0.7 or 10 higher will have a chance to become NEOs directly, without any close encounters with other planets. 0 0 5 10 15 20 25 In addition, it seems that there is no evident relationship be- t (Myr) tween the excitation and initial value of eccentricity. And sur- Fig. 3. The evolutions of eccentricity and inclination for two asteroids prisingly, no test particle appears in the intermediate zone be- that successfully crossed the resonance (upper two panels) and two as- tween the above mentioned groups, implying that the Yarkovsky teroids that failed to cross the resonance (lower two panels). In each drift and the resonance contribute to the orbital excitation in a panel two objects are distinguished by colours. The arrows in corre- complicated way. The excitation mainly attributes to the reso- sponding colour denote the the moments of entering and leaving the nance. In fact, without the Yarkovsky drift, the eccentricity of resonance. All examples are randomly selected from the set of orbits asteroids in the J7/3 MMR undergoes slow chaotic diffusion for Korin and the Yarkovsky drifting rate isa ˙Y = 0.5 AU/Gyr. millions of years and this process is then followed by a fast in- crease and large oscillations of eccentricity until the asteroid is To find out the statistical results about the dynamical exci- scattered away (Tsiganis et al. 2003). After the Yarkovsky drift tation, we reckon the variations of the eccentricity and inclina- is introduced, such dynamical evolution route may be well kept
Article number, page 4 of 10 Xu, Zhou & Ip: Transit of asteroids across the 7/3 Kirkwood gap under the Yarkovsky effect for some objects (see Fig. 3, bottom two panels), thus their ec- Yarkovsky effect, additional decreasing arises mainly because centricities are significantly pumped up and they fail to cross the Yarkovsky effect influences the stability, as well as because through the resonance. a few particles may be lost when they are forced to cross the There is also a certain probability that the forced migration boundary of this resonance, where a broad chaotic zone associ- may interrupt the above mentioned process, preventing the aster- ated with the resonance separatix and the accumulated secondary oids from entering the quick excitation phase, and finally convey resonances (e.g. Henrard & Sato 1990; Malhotra and Dermott the asteroids through the J7/3 MMR. In this case, the eccentric- 1990; Ferraz-Mello et al 1996) is located. We summarize the de- ity excitation arises from the slow chaotic diffusion as well as creasing of surviving ratio (normalized number of particles) in the Yarkovsky migration. the Resonant Groups with respect to time in Fig.5. Brož and Vokrouhlický (2008) found that the Yarkovsky ef- fect might drive the eccentricity of a prograde spinning aster- 1.0 Koronis oid locked in a first-order MMR to increase, or decrease if 0.8 the asteroid was a retrograde rotator. Similar phenomenon has a˙ = 0 5 AU/Gyr 0.6 a˙ = 0 1 AU/Gyr ) / been observed, e.g. in the 3 2 MMR with Jupiter (Milani et al. ˙