outline Model equations and Integrals The Hill type

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outline • • Model equations and Integrals The Hill type stability of two-planet systems

outline • • Model equations and Integrals The Hill type stability of two-planet systems The Hill type stability of many-planet systems Constructing systems of many and heavy planets collaborators : Tsiganis Kleomenis Antoniadou Kiki Mourtetzikoglou A. Skoulidou Despina

 • 3801 planets • 2842 planetary systems • 632 multiple planet systems

• 3801 planets • 2842 planetary systems • 632 multiple planet systems

The N-planet model bodies of masses m 0, m 1, m 2, . .

The N-planet model bodies of masses m 0, m 1, m 2, . . , m. N m 0>>mi Position vectors Ri, in an inertial frame with origin the CM Angular momentum Energy Lagrange-Jacobi identity, Sudman’s Inequality, moment of Inertia

The Hill stability in the General 3 -body problem (Marchal and Bozis, 1981) generalized

The Hill stability in the General 3 -body problem (Marchal and Bozis, 1981) generalized semimajor axis generalized semi-latus rectum ρ : mean quadratic distance ν : mean harmonic distance

The Hill stability in the General 3 -body problem m 2 m 0 m

The Hill stability in the General 3 -body problem m 2 m 0 m 1 Possible triangles of the three body if L 1 L 2

The Hill stability in the General 3 -body problem Critical values For the planetary

The Hill stability in the General 3 -body problem Critical values For the planetary case m 1<<m 0 , m 2<<m 0 Condition for Hill stability

Hill stability in 2 -planet systems Gladman’s reformulation (1993) Minimum separation of elliptic orbits

Hill stability in 2 -planet systems Gladman’s reformulation (1993) Minimum separation of elliptic orbits : inner planet at apocenter (distance from m 0 is d=1) outer planet at pericenter) Condition for Hill stability

Hill stability in 2 -planet systems – circular motion μ 1=μ 2=mp or in

Hill stability in 2 -planet systems – circular motion μ 1=μ 2=mp or in approximation orbit 1 orbit 2

2 planet system of equal planetary masses m 1=m 2=mp (initial conditions = circular

2 planet system of equal planetary masses m 1=m 2=mp (initial conditions = circular orbits) tmax =50 Kyears

Hill stability for N-planet systems • An N-planet system is Hill stable if all

Hill stability for N-planet systems • An N-planet system is Hill stable if all sequential pairs of planets (mi , mi+1) are Hill-stable (generalized Hill radius) Hill-1 A different approximation comes from Numerical simulations (Champers 1996, Obertas et al 2017) Smith and Lissauer 2009, Veras & Mustill 2014, Obertas et al 2017 If Δi, i+1 is the initial planetary orbital distance, then disruption of the system is obtained if Hill-2

3 planet system of equal planetary masses m 1=m 2=m 3 = mp initial

3 planet system of equal planetary masses m 1=m 2=m 3 = mp initial conditions = circular orbits, a 2/a 1=a 3/a 2 tmax =50 Kyears

Mass limit for Stability of resonant systems The approach of Pichierri, Morbidelli and Crida

Mass limit for Stability of resonant systems The approach of Pichierri, Morbidelli and Crida (2018) • Evolve the system including dissipative forces (planetary migration) for approaching small libration amplitude solutions. • Remove dissipative forces and slowly increase the planet masses. The mass growth preserves the original libration amplitude (adiabatic invariant) • Follow the system numerically untill its disruption. The mass reached is the limiting mass for stability. * 2 -planet simulations with equal mass planets 3: 2 resonance

Mass limit for Stability of real systems with many planets Can there exist planetary

Mass limit for Stability of real systems with many planets Can there exist planetary systems with heavy planets at distances close to the critical Hill separation distance ?

Systems of many planets : The Trappist-1 normalized units ad =1 m. Star =

Systems of many planets : The Trappist-1 normalized units ad =1 m. Star = 0. 08 Msun = 1

Trappist-1 Data from S. L. Grimm et al, 2018 normalized units ad =1 m.

Trappist-1 Data from S. L. Grimm et al, 2018 normalized units ad =1 m. Star = Msun

Trappist-1 initial normalized masses and semimajor axes

Trappist-1 initial normalized masses and semimajor axes

Hill-stability for Trappist-1 b-c λ=1. 14 c-d λ=0. 026 mi ae /ai d-e λ=25.

Hill-stability for Trappist-1 b-c λ=1. 14 c-d λ=0. 026 mi ae /ai d-e λ=25. 7 e-f λ=1. 21 f-g g-h λ=1. 23 λ=0. 28 λ=me /mi

Trappist-1: slowly varying masses (Simulation 1)

Trappist-1: slowly varying masses (Simulation 1)

Trappist-1: slowly varying masses

Trappist-1: slowly varying masses

Heavy Trappist-1 m’i =mi x 3. 7

Heavy Trappist-1 m’i =mi x 3. 7

Heavy Trappist-1 (Frappist-1 K) m’i = mi x 2. 8

Heavy Trappist-1 (Frappist-1 K) m’i = mi x 2. 8

Hill-stability for Frappist-1 K b-c λ=1. 14 c-d λ=0. 02 mi ae /ai d-e

Hill-stability for Frappist-1 K b-c λ=1. 14 c-d λ=0. 02 mi ae /ai d-e λ=34 e-f λ=1. 21 f-g g-h λ=1. 23 λ=0. 28 λ=me /mi

Trappist-1: slowly varying masses (Simulation 2)

Trappist-1: slowly varying masses (Simulation 2)

Trappist-1: slowly varying masses

Trappist-1: slowly varying masses

Heavy Trappist-1 (Frappist-1 V) m’i =mi + 1. 89 x 10 -4

Heavy Trappist-1 (Frappist-1 V) m’i =mi + 1. 89 x 10 -4

Hill-stability for Frappist-1 V b-c mi c-d λ=1. 026 λ=0. 826 ae /ai d-e

Hill-stability for Frappist-1 V b-c mi c-d λ=1. 026 λ=0. 826 ae /ai d-e e-f λ=1. 13 λ=1. 023 f-g g-h λ=1. 04 λ=0. 87 λ=me /mi

conclusions • Gladman’s Hill-criterion (Δ<3. 4 RΗ) is sufficient to guarantee instability when resonances

conclusions • Gladman’s Hill-criterion (Δ<3. 4 RΗ) is sufficient to guarantee instability when resonances are not present • The multiplanet Hill-criterion (Δ<9 RΗ) seems that overestimates the limits for instability • High mass limits of stability can be determined by slowly increasing the planetary masses and by starting from a low mass stable configuration