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Stability of Hamiltonian systems with more then two degrees of freedom Stability of Relative Equilibrium Positions of Satellite in a Circular Orbit Stability of Periodic Motions in Satellite Dynamics Stability Theory for Hamiltonian Systems Boris S. Bardin Faculty of Applied Mathematics and Physics Department of Theoretical Mechanics Course of Computer Algebra and Differential Equations Boris Bardin
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Stability of Periodic Motions in Satellite Dynamics - Stability ...Stability of Hamiltonian systems with more then two degrees of freedom Stability of Relative Equilibrium Positions

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  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability of Periodic Motions in SatelliteDynamics

    Stability Theory for Hamiltonian Systems

    Boris S. Bardin

    Faculty of Applied Mathematics and PhysicsDepartment of Theoretical Mechanics

    Course of Computer Algebra and Differential Equations

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Contents

    1 Stability of Hamiltonian systems with more then two degreesof freedom

    Stability for most initial conditionsFormal stability

    2 Stability of Relative Equilibrium Positions of Satellite in aCircular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Contents

    1 Stability of Hamiltonian systems with more then two degreesof freedom

    Stability for most initial conditionsFormal stability

    2 Stability of Relative Equilibrium Positions of Satellite in aCircular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Arnold’s Theorem of Stability for most of initialconditions

    Let us consider a Hamiltonian system of k degrees of freedom.The Birkhoff normal form of the Hamiltonian

    H = H(0)(r) + H(1)(r,ϕ), (1)

    where

    H(0)(r) = ω1r1 + · · ·+ ωk rk +k∑

    i,j=1

    aij ri rj ,

    and H(1)(r,ϕ) are terms of the order higher then two withrespect ri .

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Arnold’s Theorem of Stability for most of initialconditions

    If at r1 = · · · = rk = 0 Hamiltonian (1) satisfy the condition ofnondegeneracy

    Dk = det(∂2H0∂r2

    )6= 0 (2)

    or the condition of isoenergetic nondegeneracy

    Dk+1 = det

    (∂2H0∂r2

    ) (∂H0∂r

    )(∂H0∂r

    )0

    6= 0, (3)then the Hamiltonian system is stable for most of initialconditions (in the sense of Lebesque measure).

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Arnold diffusion

    Conditions (7) and (8) are not the same.

    Example: H(0) = ω1r1 − ω2r2 + (r1 + r2)2

    D2 = 0, D3 = −2(ω1 + ω2)2 6= 0.

    The stable for most of initial conditions system can be unstablein the sense of Liapunov. Such a phenomenon is called Arnolddiffusion.

    The typical case in higher-dimensional problems is topologicalinstability.Arnold’s example (Dokl. Acad. Nauk SSSR, V.156, 1964, 9-12):

    H =12(I21 + I

    22) + ε(cosϕ1 − 1)(1 + µ(sinϕ2 + cos t))

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Nehoroshev’s Theorem

    The KAM theory proves the metric stability, i.e stability for mostof initial conditions

    Nehoroshev’s TheoremSuppose that the unperturbed Hamiltonian H(0)(I) is a steepfunction. Then for a sufficiently small perturbation

    |I(t)− I(0)| < εb for 0 ≤ t ≤ 1ε

    exp(

    1εa

    )in the perturbed Hamiltonian system. Here a and b are positiveconstants that depend on the geometric properties of theunperturbed Hamiltonian.

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Arnold diffusion in resonant casesMarkeev’s Example

    Let us consider the system with Hamiltonian

    H = ω1r1 − ω2r2 + ω3r3 + r1r3 − r1r2 + r2r3 + H(1)(r,ϕ),

    whereH(1)(r,ϕ) = r1r2

    √r3 sin(2ϕ1 + 2ϕ2 + ϕ3).

    and resonance 2ω1 − 2ω2 + ω3 = 0 takes placeThe conditions of Arnold’s theorem are fulfilled

    D4 = (ω1 + ω2)2 6= 0,

    but the Hamiltonian system has the following solution

    2ϕ1 + 2ϕ2 + ϕ3 = π

    r3(t) =12

    r1(t) =12

    r2(t) = r3(0)[1− 6r32

    3 (0)t ].

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Contents

    1 Stability of Hamiltonian systems with more then two degreesof freedom

    Stability for most initial conditionsFormal stability

    2 Stability of Relative Equilibrium Positions of Satellite in aCircular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Formal stability

    Definition: If there exist power series

    G(q,p) = G2(q,p) + G3(q,p) + . . . ,

    such that it is a formal positive definite integral of theHamiltonian system

    dqdt

    =∂H∂p

    ,dpdt

    = −∂H∂q

    , (4)

    then system (4) is called formal stable.

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Moser’s Theorem on Formal stability

    Let us consider a Hamiltonian system of k degrees of freedomwith the Hamiltonian.

    H = ω1r1 + · · ·+ ωk rk + H(1)(r,ϕ), (5)

    here H(1)(r,ϕ) are terms of the order higher then one withrespect ri .If the following conditions

    n∑i=1

    miωi 6= 0, mi ∈ Z, mi ≥ 0,n∑

    i=1

    mi > 0

    are fulfilled, then the system with Hamiltonian (5) is formalstable.(Moser, J. New aspects in the theory of stability of Hamiltoniansystems. Comm. Pure Appl. Math. V.11, 1958, 81–114.)

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Glimm’s Theorem on Formal stability

    Let us suppose that the normal form of the Hamiltonian reads

    H = ω1r1 + · · ·+ ωk rk +k∑

    i,j=1

    aij ri rj + H(1)(r,ϕ), (6)

    andn∑

    i=1

    miωi 6= 0, mi ∈ N, 0 <n∑

    i=1

    |mi | ≤ 4.

    If the quadratic formk∑

    i,j=1

    aij ri rj is definite, then the system with

    Hamiltonian (6) is formal stable.(Glimm, J. Formal stability of Hamiltonian systems. Comm.Pure Appl. Math. V.17, 1964, pp. 509–526.)

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Stability for most initial conditionsFormal stability

    Brjuno’s Theorem on Formal stability

    If the quadratic formk∑

    i,j=1

    aij Ii Ij 6= 0,

    for the vector I = (I1, . . . , Ik ) 6= 0 such that Ii ≥ 0 and Ii aresolutions of the equation

    n∑i=1

    mi Ii = 0,

    then the system with Hamiltonian (6) is formal stable.

    (Brjuno, A. D. Formal stability of Hamiltonian systems.(Russian) Mat. Zametki V.1, 1967, pp. 325–330.)

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Contents

    1 Stability of Hamiltonian systems with more then two degreesof freedom

    Stability for most initial conditionsFormal stability

    2 Stability of Relative Equilibrium Positions of Satellite in aCircular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Relative Equilibrium Positions of Satellite in a CircularOrbit

                                                                                                                       Orbit of the mass center n

    v

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    The Hamiltonian of the Problem

    H =(sin2 ϕ+ θA cos2 ϕ)

    2 sin2 ϑp2ψ +

    [(sin2 ϕ+ θA cos2 ϕ) +

    θAθC

    ]p2ϕ2

    (cos2 ϕ+ θA sin2 ϕ)p2ϑ2− (sin2 ϕ+ θA cos2 ϕ)pψpϕ+

    (1− θA) sin 2ϕ2 sinϑ

    pψpϑ −(1− θA)

    2sin 2ϕ cotϑpψpϕ − pψ

    32

    [θA − 1θA

    a211 +θC − 1θA

    a213

    ]

    where

    a11 = cosψ cosϕ− sinψ sinϕ cosϑ, a13 = sinψ sinϑ

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Variations

    Parameters: θA = A/B and θC = C/BEquilibrium position:

    ψ = ϕ = pϑ = pψ = 0, ϑ =π

    2, pψ =

    1θA

    Let us introduce variations

    q1 = ϑ−π

    2, q2 = ϕ, q3 = ψ,

    p1 = pϑ, p2 = pϕ, p3 = pψ −1θA

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Perturbed Hamiltonian

    H = H2 + H3 + H4 + . . .

    H2 =p212

    +θA

    2θCp22 +

    12θA

    q21 −(θA − 1)(3θA + 1)

    2θ2Aq23+

    + q1p2 −θA − 1θA

    q2p1 +θA2

    p23 +3(θC − θA)

    2θA

    H3 = q21p3 +3(θA − 1)

    θAq1q2q3 + θAq1q2p3 −

    3θA − 1)θA

    q22q3−

    − (θA − 1)q2p1p3

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Contents

    1 Stability of Hamiltonian systems with more then two degreesof freedom

    Stability for most initial conditionsFormal stability

    2 Stability of Relative Equilibrium Positions of Satellite in aCircular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Linear Problem of StabilitySufficient condition of stability

    If the following condition is fulfilled

    θA < θC < 1

    then relative equilibrium is stable in Lyapunov sense.

    Sufficient condition of stability: If the biggest principal axis isdirected along the radius vector of the center of mass and thesmallest one is directed along the normal of the orbit.

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Linear Problem of StabilityNecessary condition of stability

    If parameter values belong to the Domain I then relativeequilibrium is stable in linear approximation.In domain II

    H =12ω1(q21 +p

    21)−

    12ω2(q22 +p

    22)+

    12ω2(q23 +p

    23)+H3+H4+ . . .

    where ω1 > 0, ω2 > 0, ω3 > 0. Nonlinear study isnecessary to solve stability problem.

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Contents

    1 Stability of Hamiltonian systems with more then two degreesof freedom

    Stability for most initial conditionsFormal stability

    2 Stability of Relative Equilibrium Positions of Satellite in aCircular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Nonlinear Problem of StabilityNonresonant case

    In polar variables: qi =√

    2ri sinϕi , pi =√

    2ri cosϕi

    H = H(0)(r1, r2, r3) + H̃(r1, r2, r3, ϕ1, ϕ2, ϕ3)

    where

    H(0) = ω1r1 − ω2r2 + ω3r3++ c200r21 + c110r1r2 + c101r1r3 + c020r

    22 + c101r1r3 + c002r

    23

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Stability for most of initial conditions

    In Domain II outside of curves of resonances up to fourth orderat r1 = r2 = r3 = 0 Hamiltonian (1) satisfy the condition ofnondegeneracy

    D3 = det(∂2H0∂r2

    )6= 0 (7)

    or the condition of isoenergetic nondegeneracy

    D4 = det

    (∂2H0∂r2

    ) (∂H0∂r

    )(∂H0∂r

    )0

    6= 0, (8)Thus, the Hamiltonian system is stable for most of initialconditions (in the sense of Lebesque measure).

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Formal Stability

    If in the domain ri ≤ 0 (i = 1,2,3) the system of equations

    ω1r1 − ω2r2 + ω3r3 = 0c200r21 + c110r1r2 + c101r1r3 + c020r

    22 + c101r1r3 + c002r

    23 = 0

    does not have any solution except trivial one r1 = r2 = r3 = 0,then the equilibrium is formal stable.

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Resonances

    In the considered approximation the following resonances cantake place

    k1ω1 − k2ω2 + k3ω3 = 0 (|k1|+ |k2|+ |k3| = 2,3,4)

    List of resonances which should be taken into account:

    1. ω1 − ω2 − 2ω3 = 0, 2. ω1 − ω2 − ω3 = 0,

    3. ω2 − ω3 = 0, 4. ω1 + ω2 − 2ω3 = 0,

    5. ω1 − ω3 = 0, 6. 2ω2 − ω3 = 0,

    7. ω1 + ω2 − ω3 = 0, 8. ω1 − 3ω2 = 0,

    9. 2ω1 − ω3 = 0,

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Arnold Diffusion

    In points Pi (i = 1,2,3) of the Domain II the fifth orderresonance 4ω2 = ω1 takes place.Equality 16c020 + 4c011 + c002 = 0 is fulfilled

    The Hamiltonian normal form reads

    H = H(0) + γi r22√

    r3 cos(4ϕ2 + ϕ3) + O((r1 + r2 + r4)3)

    The truncated system has the following partial solution

    r1 = 0, r2 = 4r3 > 0.

    Boris Bardin

  • Stability of Hamiltonian systems with more then two degrees of freedomStability of Relative Equilibrium Positions of Satellite in a Circular Orbit

    Hamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability

    Arnold Diffusion

    Boris Bardin

    Stability of Hamiltonian systems with more then two degrees of freedomStability for most initial conditionsFormal stability

    Stability of Relative Equilibrium Positions of Satellite in a Circular OrbitHamiltonian of the Perturbed MotionLinear Problem of StabilityNonlinear Problem of Stability