Separation of variables in the generalized 4th Appelrot class

We consider the analogue of the 4th Appelrot class of motions of the Kowalevski top for the case of two constant force fields. The trajectories of this family fill the four-dimensional surface O^4 in the six-dimensional phase space. The constants of …

Authors: Mikhail P. Kharlamov

Separation of variables in the generalized 4th Appelrot class
Separation of v ariables in the generalized 4th App elrot class ∗ Mikhail P . Kharl a mov Gagarin Str e et 8, V olgo gr ad, 40013 1 Russia e-mail: mharla mov@vags.ru 28.0 1.07 Abstract W e consider the analogue of the 4th App elrot class of mot ions of the Ko w alevski top for the c ase of t wo constan t force fields. The tr a jectories of this family fill the four-dimensional surface O in the six-dimensional p hase sp ace. The constan ts of thr ee first integ rals in in- v olution restricted to this surface fi ll one of the sheets of the bifu rcation d iagram in R 3 . W e p oint out the p air of p artial integ rals t o obtain the explicit parametric equations of this sheet. Th e ind uced system on O is s ho wn to b e Hamiltonian with tw o degrees of fr eedom ha ving the thin set of p oin ts where the induced symplectic structure degenerates. The region of existence of motions in terms of the int egral constan ts is found . W e pro vide the separation of v ariables on O and the alge braic form ulae for the initial p hase v ariables. Key w ords and phras es: Kowalevski top, double field, Appelr ot classes, se pa ration o f v a riables MSC2000 n um bers : 7 0 E17, 70 G4 0 DOI: 10.1134 /S1560 354707030021 1 Preliminaries The equations of motion of the Ko w alevski top in t w o constant fields, expressed in the reference system O e 1 e 2 e 3 of the principal axes of inertia at the fixed p oint O , 2 ˙ ω 1 = ω 2 ω 3 + β 3 , 2 ˙ ω 2 = − ω 1 ω 3 − α 3 , ˙ ω 3 = α 2 − β 1 , ˙ α 1 = α 2 ω 3 − α 3 ω 2 , ˙ β 1 = β 2 ω 3 − β 3 ω 2 , ˙ α 2 = α 3 ω 1 − α 1 ω 3 , ˙ β 2 = β 3 ω 1 − β 1 ω 3 , ˙ α 3 = α 1 ω 2 − α 2 ω 1 , ˙ β 3 = β 1 ω 2 − β 2 ω 1 (1.1) can without loss of generality b e restricted to the phase space P 6 ⊂ R 9 ( ω , α , β ) defined b y the geometric in tegrals α 2 1 + α 2 2 + α 2 3 = a 2 , β 2 1 + β 2 2 + β 2 3 = b 2 , α 1 β 1 + α 2 β 2 + α 3 β 3 = 0 (1.2) ∗ Regular and Cha otic Dyna mics , 20 07, V ol. 1 2, No. 3, pp. 26 7-280 1 (see [1] for details). This sy stem is completely integrable due to the existence of three in tegrals in in v olution [2, 3] H = ω 2 1 + ω 2 2 + 1 2 ω 2 3 − ( α 1 + β 2 ) , K = ( ω 2 1 − ω 2 2 + α 1 − β 2 ) 2 + (2 ω 1 ω 2 + α 2 + β 1 ) 2 , G = 1 4 ( M 2 α + M 2 β ) + 1 2 ω 3 M γ − b 2 α 1 − a 2 β 2 , (1.3) where M α = 2 ω 1 α 1 + 2 ω 2 α 2 + ω 3 α 3 , M β = 2 ω 1 β 1 + 2 ω 2 β 2 + ω 3 β 3 , M γ = 2 ω 1 ( α 2 β 3 − α 3 β 2 ) + 2 ω 2 ( α 3 β 1 − α 1 β 3 ) + ω 3 ( α 1 β 2 − α 2 β 1 ) . (1.4) F or the general case a > b > 0 (1.5) the explicit in tegration has not b een found y et. It is natural to study first the in v a rian t subman- ifolds in P 6 suc h that the induced system has only t w o degrees of f reedom. It is pro v ed in [4, 1] that there exist only three submanifolds M , N , O of this type. The union M ∪ N ∪ O coincides with the set of critical p oin ts of the in tegra l map H × K × G : P 6 → R 3 . (1.6) If b = 0 ( the classical Kow alevski case [5]), then the critical set of the map (1.6) consists of the motions that b elong to the so-called fo ur App elrot classes [6]. The set M , first found in [2] as the zero lev el o f the in tegral K , generalizes the 1st App elrot class. T he phase t o p ology o f the system induced on M w as studied in [7]. The dynamical system o n N generalizing t he 2nd a nd 3rd App elrot classes was explicitly in tegrated in [8]. The prese n t w ork conside rs the restriction of the system (1.1) to the in v ariant subse t O . In tro duce the complex phase v ariables [9] ( i 2 = − 1): x 1 = ( α 1 − β 2 ) + i ( α 2 + β 1 ) , x 2 = ( α 1 − β 2 ) − i ( α 2 + β 1 ) , y 1 = ( α 1 + β 2 ) + i ( α 2 − β 1 ) , y 2 = ( α 1 + β 2 ) − i ( α 2 − β 1 ) , z 1 = α 3 + iβ 3 , z 2 = α 3 − iβ 3 , w 1 = ω 1 + iω 2 , w 2 = ω 1 − iω 2 , w 3 = ω 3 . (1.7) The system (1.1) tak es the form x ′ 1 = − x 1 w 3 + z 1 w 1 , x ′ 2 = x 2 w 3 − z 2 w 2 , y ′ 1 = − y 1 w 3 + z 2 w 1 , y ′ 2 = y 2 w 3 − z 1 w 2 , 2 z ′ 1 = x 1 w 2 − y 2 w 1 , 2 z ′ 2 = − x 2 w 1 + y 1 w 2 , 2 w ′ 1 = − ( w 1 w 3 + z 1 ) , 2 w ′ 2 = w 2 w 3 + z 2 , 2 w ′ 3 = y 2 − y 1 . (1.8) Here the prime stands for d/d ( it ). The set O , b y the definition giv en in the w ork [1], includes as a prop er subset the followin g p oin ts w 1 = w 2 = 0 , z 1 = z 2 = 0 . (1.9) The in v ar ia n t relations (1.9) lead to the family of p endulum motions first found in [4] α = a ( e 1 cos θ − e 2 sin θ ) , β = ± b ( e 1 sin θ + e 2 cos θ ) , α × β ≡ ± ab e 3 , ω = dθ dt e 3 , d 2 θ dt 2 = − ( a ± b ) sin θ . (1.10) 2 The corresp onding v alues of the in tegrals (1.3) satisfy one of the follow ing g = ± ab h, k = ( a ∓ b ) 2 , h > − ( a ± b ) . (1.11) In the sequel w e use functions and expressions hav ing singularities at the p oints (1.9). There- fore, b y default, we ex clude the tra jectories (1.10). The remaining part of O can b e describ ed b y the pair of equations R 1 = 0 , R 2 = 0 , (1.12) where R 1 = w 2 x 1 + w 1 y 2 + w 3 z 1 w 1 − w 1 x 2 + w 2 y 1 + w 3 z 2 w 2 , R 2 = ( w 2 z 1 + w 1 z 2 ) w 2 3 + h w 2 z 2 1 w 1 + w 1 z 2 2 w 2 + w 1 w 2 ( y 1 + y 2 ) + x 1 w 2 2 + x 2 w 2 1 i w 3 + + w 2 2 x 1 z 1 w 1 + w 2 1 x 2 z 2 w 2 + x 1 z 2 w 2 + x 2 z 1 w 1 + ( w 1 z 2 − w 2 z 1 )( y 1 − y 2 ) . (1.13) F or the deriv atives w e hav e, in virtue of (1.8), R ′ 1 = κ 2 R 2 , R ′ 2 = κ 1 R 1 , κ 1 = 1 2 w 1 w 2  ( w 1 w 2 w 3 + z 2 w 1 + z 1 w 2 ) 2 + w 1 w 2 ( x 2 w 2 1 + x 1 w 2 2 )  , κ 2 = 1 2 w 1 w 2 . (1.14) The equations (1 .14) straightforw ardly prov e that the set ( 1.12) is preserv ed b y the phase flo w (1 .1). Besides, it follow s that the P oisson brac k et { R 1 , R 2 } is a partial in tegral on O . The subset in O defined b y the equation { R 1 , R 2 } = 0 (1.15) is the set o f p oints at whic h the induced symplectic structure is degenerate. Belo w we calculate { R 1 , R 2 } using t he appropriate inte grals on O and sho w that the set (1.15) is of measure zero. Th us, the dynamical system induced on O by the sys tem ( 1.1) is almost ev erywhere a Hamiltonian system with t w o degrees of freedom. In particular, a lmost all its in t egra l manifolds consist of t w o- dimensional Liouville tori. 2 P artial integrals Recall that in the classical Kow alevski case ( β = 0) there exists the momen tum in tegral L = 1 2 I ω · α ( I = diag { 2 , 2 , 1 } ) . (2.1) Then the integral G b ecomes equal to L 2 . Let ℓ denote the constan t o f the in tegral (2.1). In App elrot’s notation the 4th class of esp e cia l ly r emarka b le motions is defined b y the follow ing conditions. (i) The second p olynomial of Kow alevski has a multiple ro o t . One of the Ko w alevsk i v ariables remains constan t and equal to the mu ltiple ro ot s of the corresp onding Euler resolve n t ϕ ( s ) = s ( s − h ) 2 + ( a 2 − k ) s − 2 ℓ 2 : ϕ ( s ) = 0 , ϕ ′ ( s ) = 0 . (2.2) 3 (ii) Tw o equatorial comp onents of the angular v elo cit y are constant: ω 1 ≡ − ℓ/s , ω 2 ≡ 0. Giv en β = 0, this fact can b e written in the form I ω · α I ω · e 1 = − s, I ω · β = 0 , I ω · e 2 = 0 . (2.3) The next statemen t establishes the conditions similar to ( 2.3) for the generalized top. Theorem 1. On e ach tr aje ctory b elo n ging to O the r atios I ω · α I ω · e 1 , I ω · β I ω · e 2 ar e c onstant and e qual to e ac h other. Pr o of. Let M = I ω , M j = I ω · e j ( j = 1 , 2 , 3) . (2.4) Due to (1.4) w e also hav e M α = I ω · α , M β = I ω · β . Then the first equation (1.12) yields M α M 1 − M β M 2 = 0 . (2.5) In tro duce the function S = − M α M 1 + M β M 2 M 2 1 + M 2 2 and calculate its time deriv ativ e: dS dt = − ( M 2 1 + M 2 2 ) ω 3 + 4 α 3 M 1 + 4 β 3 M 2 2( M 2 1 + M 2 2 ) 2 ( M α M 2 − M β M 1 ) . In virtue of (2.5) the right hand side is iden tically zero. T herefore S is a partia l integral o n O . Denote b y s the correspo nding constan t: M α M 1 + M β M 2 M 2 1 + M 2 2 = − s. (2.6) F rom (2.5), (2.6) w e obtain M α = − sM 1 , M β = − sM 2 (2.7) with the constan t v alue s . Note that according to (2.7) the function S can b e written in either of the represen t ations S = − 1 4  M α + iM β ω 1 + iω 2 + M α − iM β ω 1 − iω 2  = − 1 2 M α + iM β ω 1 + iω 2 = − 1 2 M α − iM β ω 1 − iω 2 . (2.8) Theorem 2. On the set O the system (1.1) has the p artial inte gr al T = 1 2 ( M α M 1 + M β M 2 ) − 2( α 1 β 2 − α 2 β 1 ) + a 2 + b 2 . (2.9) Pr o of. The time deriv ative of T d T dt = 1 4 ω 3 ( M α M 2 − M β M 1 ) v anishes on O due to (2.5). 4 Denote b y τ the constant of the in tegral T. Remark 1. In the work [1] e q uations similar to (1.12) wer e d e rive d fr om the c ond i tion that the function 2 G + ( τ − a 2 − b 2 ) H + s K (2.10) with L agr an ge’s m ultipliers s, τ has a critic al p oint on P 6 . Using the c o or dinates (1.7) we have fr om (2.8) , (2.9) S = − w 1 ( x 2 w 1 + y 1 w 2 + z 2 w 3 ) + w 2 ( y 2 w 1 + x 1 w 2 + z 1 w 3 ) 4 w 1 w 2 = = − x 2 w 1 + y 1 w 2 + z 2 w 3 2 w 2 = − y 2 w 1 + x 1 w 2 + z 1 w 3 2 w 1 , (2.11) T = 1 2 [ w 1 ( x 2 w 1 + y 1 w 2 + z 2 w 3 ) + w 2 ( y 2 w 1 + x 1 w 2 + z 1 w 3 )] + x 1 x 2 + z 1 z 2 = = − 2 S w 1 w 2 + x 1 x 2 + z 1 z 2 . (2.12) Comp aring (2.11) , (2.12) with the e xpr essions for s, τ given in [1] we se e that on O L agr ange’s multipliers in (2 .10) c oincide with the c onstants of the inte gr als S, T intr o duc e d he r e. Supp osing (1.5), introduce parameters p, r ( p > r > 0 ) suc h tha t p 2 = a 2 + b 2 , r 2 = a 2 − b 2 . (2.13) Let h, k , g denote the constants of the ge neral in tegrals (1.3). Then according to Remark 1, from the results of the w ork [1] w e o btain that on O h = p 2 − τ 2 s + s, k = τ 2 − 2 p 2 τ + r 4 4 s 2 + τ , g = p 4 − r 4 4 s + 1 2 ( p 2 − τ ) s. (2.14) These equations can be considered as para metric equations of the cor r esp onding bifurcation sheet of the in tegral map (1.6). Eliminating τ we h a v e ψ ( s ) = 0 , ψ ′ ( s ) = 0 , (2.15) where ψ ( s ) = s 2 ( s − h ) 2 + ( p 2 − k ) s 2 − 2 g s + p 4 − r 4 4 . If β = 0 ( p 2 = r 2 = a 2 ), then ψ ( s ) = s ϕ ( s ) and the conditions (2 .15) turn to (2.2). Therefore, the set of tra j ectories b elonging to O is the generalization of the set of the esp e cial ly r ema rkable motions of the 4th App elrot class. 3 P arametric equ ations of in tegral manifolds Due to the equations (2.14) the functions S, T form a complete system of first in tegrals on O . In particular, the equations of the in tegral manifold { ζ ∈ P 6 : H ( ζ ) = h, K ( ζ ) = k , G ( ζ ) = g } in this class of motions are equiv alent to the relations (1.12) and the equations S = s, T = τ . (3.1) 5 Using (2.5), (2.11) w e replace the equations R 1 = 0 , S = s b y ( y 2 + 2 s ) w 1 + x 1 w 2 + z 1 w 3 = 0 , x 2 w 1 + ( y 1 + 2 s ) w 2 + z 2 w 3 = 0 . (3.2) A t the same time, from (1.13) and (2.12) the system R 2 = 0 , T = τ is equiv alen t to x 2 z 1 w 1 + x 1 z 2 w 2 + ( τ − x 1 x 2 ) w 3 = 0 , (3.3) 2 s w 1 w 2 − ( x 1 x 2 + z 1 z 2 ) + τ = 0 . (3.4) T o obtain a closed sy stem of equations we m ust add the g eometric integrals (1.2). In terms of the v ariables (1.7) w e get z 2 1 + x 1 y 2 = r 2 , z 2 2 + x 2 y 1 = r 2 , (3.5) x 1 x 2 + y 1 y 2 + 2 z 1 z 2 = 2 p 2 . (3.6) The v ariables (1.7) b y definition satisfy x 2 = x 1 , y 2 = y 1 , z 2 = z 1 , w 2 = w 1 , w 3 ∈ R , (3.7) th us forming a space of real dimension 9. Sev en relations (3.2) – (3.6 ) define the inte gral manifold. In the case of indep endency of the in tegrals S, T this manifold is t wo-dimens ional and consists of Liouville tori filled with quasi-p erio dic motions. Let x = p x 1 x 2 , z = p z 1 z 2 , ξ = 2 s w 1 w 2 . (3.8) Then from (3.4) ξ = x 2 + z 2 − τ . (3.9) F rom (3.5), (3.8) w e obtain ( r 2 − x 1 y 2 )( r 2 − x 2 y 1 ) = z 4 , (3.10) and the equation (3.6) yields y 1 y 2 = 2 p 2 − x 2 − 2 z 2 . (3.11) Hence r 2 ( x 1 y 2 + x 2 y 1 ) = r 4 + 2 p 2 x 2 − ( x 2 + z 2 ) 2 . (3.12) Rewrite (3.5) in the form ( z 1 + z 2 ) 2 = 2 r 2 − ( x 1 y 2 + x 2 y 1 ) + 2 z 2 , ( z 1 − z 2 ) 2 = 2 r 2 − ( x 1 y 2 + x 2 y 1 ) − 2 z 2 (3.13) and substitute (3.12) to obtain r 2 ( z 1 + z 2 ) 2 = Φ 1 , r 2 ( z 1 − z 2 ) 2 = Φ 2 , (3.14) where Φ 1 = ( x 2 + z 2 + r 2 ) 2 − 2( p 2 + r 2 ) x 2 = ( ξ + τ + r 2 ) 2 − 2( p 2 + r 2 ) x 2 , Φ 2 = ( x 2 + z 2 − r 2 ) 2 − 2( p 2 − r 2 ) x 2 = ( ξ + τ − r 2 ) 2 − 2( p 2 − r 2 ) x 2 . (3.15) Note tha t the equilibria ω ≡ 0 of the system (1.1) are included in the family of motions (1.10). On the rest of the tra jectories in O t he determinan t o f the equations (3 .2), (3.3) in w j 6 ( j = 1 , 2 , 3 ) v a nishes iden t ically . Calculate this determinant and eliminate z 2 1 , z 2 2 from (3.5) a nd the pro duct y 1 y 2 from (3.11) to obtain 2 s [( r 2 x 1 − τ y 1 ) + ( r 2 x 2 − τ y 2 )] = − r 2 ( x 1 y 2 + x 2 y 1 )+ +2[2 s 2 ( τ − x 2 ) + p 2 ( τ + x 2 ) − τ ( x 2 + z 2 )] . (3.16) On the other hand, the direct calculation in view of (3.8), (3.11) giv es ( r 2 x 1 − τ y 1 )( r 2 x 2 − τ y 2 ) = r 4 x 2 + τ (2 p 2 − x 2 − 2 z 2 ) − r 2 τ ( x 1 y 2 + x 2 y 1 ) . (3.17) Denote σ = τ 2 − 2 p 2 τ + r 4 , χ = √ k > 0 . (3.18) F rom the second relation (2.14) w e ha ve the iden tity 4 s 2 χ 2 = σ + 4 s 2 τ . (3.19) In tro duce the complex conjugate v ariables µ 1 = r 2 x 1 − τ y 1 , µ 2 = r 2 x 2 − τ y 2 . (3.20) Eliminating x 1 y 2 + x 2 y 1 from (3.16), (3.17) with the help of (3.12) w e come to the syste m 2 s ( µ 1 + µ 2 ) = ξ 2 − 4 s 2 ( x 2 − τ ) − σ , µ 1 µ 2 = τ ξ 2 + σ x 2 − τ σ . (3.21) Cho ose µ ∗ 1 = p 2 sµ 1 − 4 s 2 τ , µ ∗ 2 = p 2 sµ 2 − 4 s 2 τ (3.22) to b e complex conjugate. Then the system (3.21) tak es the form ( µ ∗ 1 + µ ∗ 2 ) 2 = Ψ 1 , ( µ ∗ 1 − µ ∗ 2 ) 2 = Ψ 2 , (3.23) where Ψ 1 = ξ 2 − 4 s 2 ( x + χ ) 2 , Ψ 2 = ξ 2 − 4 s 2 ( x − χ ) 2 . (3.24) As w as to b e exp ected from dimensional reasoning, all phase v ariables could b e expressed in terms of t w o almost ev erywhe re indep enden t auxiliary v aria bles. The a b o v e form ulae emphasize the sp ecial role of the pair ( x, ξ ). F rom (3.22), (3.23) w e find µ 1 = 2 sτ + 1 8 s ( p Ψ 1 + p Ψ 2 ) 2 , µ 2 = 2 sτ + 1 8 s ( p Ψ 1 − p Ψ 2 ) 2 . (3.25) F urther on the calculation sequenc e is as follo ws. F rom (3.14) w e find z 1 , z 2 . Multiplying the equations (3.20) b y x 2 , x 1 resp ectiv ely and using (3.5) w e get x 2 µ 1 = r 2 x 2 − τ x 2 y 1 = r 2 ( x 2 − τ ) + τ z 2 2 , x 1 µ 2 = r 2 x 2 − τ x 1 y 2 = r 2 ( x 2 − τ ) + τ z 2 1 , 7 whence x 1 , x 2 are found. Substituting these v alues bac k to (3 .2 0) we find y 1 , y 2 . As a result, after some ob vious transformations w e obtain the follo wing expressions f o r the configuration v ariables: x 1 = 2 s r 2 4 r 4 ( x 2 − τ ) + τ ( p Φ 1 + p Φ 2 ) 2 16 s 2 τ + ( p Ψ 1 − p Ψ 2 ) 2 , x 2 = 2 s r 2 4 r 4 ( x 2 − τ ) + τ ( p Φ 1 − p Φ 2 ) 2 16 s 2 τ + ( p Ψ 1 + p Ψ 2 ) 2 , (3.26) y 1 = 2 s 4[2 τ ξ − τ ( x 2 − τ ) + σ ] − ( p Φ 1 − p Φ 2 ) 2 16 s 2 τ + ( p Ψ 1 − p Ψ 2 ) 2 , y 2 = 2 s 4[2 τ ξ − τ ( x 2 − τ ) + σ ] − ( p Φ 1 + p Φ 2 ) 2 16 s 2 τ + ( p Ψ 1 + p Ψ 2 ) 2 , (3.27) z 1 = 1 2 r ( p Φ 1 + p Φ 2 ) , z 2 = 1 2 r ( p Φ 1 − p Φ 2 ) . (3.28) Note that all radicals are algebraic. The fo rmal c hoice of signs in (3.26)–(3.28) is defined b y the initia l c hoice in the express ions for µ 1 , µ 2 , z 1 , z 2 . The p o lynomials Φ j , Ψ j ( j = 1 , 2) obv iously split to m ultipliers linear with res p ect to x, ξ . Then, typically , the pro jection of an in tegral manifold on to the ( x, ξ ) -plane has the form of a quadrangle. Fix any inner p oint ( x, ξ ) of suc h pro jection. Then the expre ssions (3.26)–(3.2 8) define eigh t p oin ts of the configuration space w ith differen t set of signs of the radicals p Φ 1 , p Φ 2 , p Ψ 1 Ψ 2 . T o find w 3 , use the energy in tegral. On account of (2.14) it t ak es the form 2 s w 2 3 + 4 s w 1 w 2 − 2 s ( y 1 + y 2 ) = 4 s 2 + 2 p 2 − 2 τ . Substitute 2 s w 1 w 2 from (3.4) and replace 2 p 2 b y its expre ssion fro m ( 3 .6) to obtain 2 s w 2 3 = D , (3.29) where D = ( y 1 + 2 s )( y 2 + 2 s ) − x 1 x 2 (3.30) is the determinant of ( 3 .2) with resp ect to w 1 , w 2 . In particular, this determinan t v anishes a long with w 3 . Due to this fact w e can express w 1 , w 2 either a s linear functions of w 3 , or in in v erse prop ortion to w 3 : w 1 = x 1 z 2 − ( y 1 + 2 s ) z 1 ( y 1 + 2 s )( y 2 + 2 s ) − x 2 w 3 = x 1 z 2 − ( y 1 + 2 s ) z 1 2 s w 3 , w 2 = x 2 z 1 − ( y 2 + 2 s ) z 2 ( y 1 + 2 s )( y 2 + 2 s ) − x 2 w 3 = x 2 z 1 − ( y 2 + 2 s ) z 2 2 s w 3 . (3.31) With tw o p ossibilities of the sign c hoice for w 3 in (3.29) we hav e that the in v erse image in the in tegral manifold { S = s, T = τ } ∩ O of a generic p oint ( x, ξ ) con ta ins 16 p oin ts. W e also need t he explicit form ula for w 3 in terms of x, ξ . F r o m (3.27) w e write y 1 + 2 s = 2 s 4[2 τ ξ − τ ( x 2 − τ ) + 4 s 2 χ 2 ] − ( p Φ 1 − p Φ 2 ) 2 + ( p Ψ 1 − p Ψ 2 ) 2 16 s 2 τ + ( p Ψ 1 − p Ψ 2 ) 2 , y 2 + 2 s = 2 s 4[2 τ ξ − τ ( x 2 − τ ) + 4 s 2 χ 2 ] − ( p Φ 1 + p Φ 2 ) 2 + ( p Ψ 1 + p Ψ 2 ) 2 16 s 2 τ + ( p Ψ 1 + p Ψ 2 ) 2 . (3.32) 8 Note that [16 s 2 τ + ( p Ψ 1 − p Ψ 2 ) 2 ][16 s 2 τ + ( p Ψ 1 + p Ψ 2 ) 2 ] = 64 s 2 ( τ ξ 2 + σ x 2 − τ σ ) . (3.33) Then D = p Φ 1 Φ 2 Ψ 1 Ψ 2 − P 2( τ ξ 2 + σ x 2 − τ σ ) , where P ( x, ξ ) = ξ 4 + 2 τ ξ 3 + 2[( τ − 2 s 2 − p 2 ) x 2 − τ (2 s 2 − p 2 ) − r 4 ] ξ 2 − − 8 s 2 [( τ − 2 χ 2 ) x 2 + τ χ 2 ] ξ − 4 s 2 ( x 2 − χ 2 )[2( τ − p 2 ) x 2 − ( τ 2 − r 4 )] . Let Q ( x, ξ ) = ( ξ + τ + 2 s 2 − p 2 ) 2 − 4 s 2 x 2 + r 4 − (2 s 2 − p 2 ) 2 , P 1 ( x, ξ ) = P ( x, ξ ) + 2 xQ ( x, ξ ) p τ ξ 2 + σ x 2 − τ σ , P 2 ( x, ξ ) = P ( x, ξ ) − 2 xQ ( x, ξ ) p τ ξ 2 + σ x 2 − τ σ . Direct calculation prov es the iden tit y P 1 P 2 ≡ Φ 1 Φ 2 Ψ 1 Ψ 2 . On the other hand, P 1 + P 2 ≡ 2 P . Therefore, D = − ( p P 1 − p P 2 ) 2 4( τ ξ 2 + σ x 2 − τ σ ) , whence w 3 = i p P 1 − p P 2 2 p 2 s ( τ ξ 2 + σ x 2 − τ σ ) . (3.34) Belo w w e use o ne more represen tatio n of w 1 , w 2 not dep ending on w 3 . The system (3.2) yields x 2 w 2 1 = − z 2 w 1 w 3 − ( y 2 + 2 s ) w 1 w 2 , x 1 w 2 2 = − z 1 w 2 w 3 − ( y 1 + 2 s ) w 1 w 2 . Substitute the expressions for w 1 w 3 , w 2 w 3 found from the in v erse prop ortion in (3.31) and eliminate w 1 w 2 b y (3.4) to obtain 2 s x 2 w 2 1 = − ( µ 1 − 2 sτ ) − 2 sx 2 , 2 s x 1 w 2 2 = − ( µ 2 − 2 sτ ) − 2 sx 2 . Then from (3.25) w e find w 1 = i 4 s √ x 2 ( p Θ 1 + p Θ 2 ) , w 2 = i 4 s √ x 1 ( p Θ 1 − p Θ 2 ) , (3.35) where Θ 1 ( x, ξ ) = ( ξ − 2 sx ) 2 − 4 s 2 χ 2 , Θ 2 ( x, ξ ) = ( ξ + 2 sx ) 2 − 4 s 2 χ 2 . (3.36) Note that the pro ducts Θ 1 Θ 2 and Ψ 1 Ψ 2 coincide. The c hoice of the signs in (3.35) is deter- mined b y the condition ( √ x 2 w 1 )( √ x 1 w 2 ) = x ξ / 2 s following from (3.8). The signs of the complex conjugate v alues √ x 1 , √ x 2 m ust b e chosen in suc h a w a y that the express ions (3.35), (3.35) satisfy one of the equations (3.2), (3.3) (then the other t w o hold automatically). Th us, all phase v aria bles are algebraically expressed in terms of tw o auxiliary v ariables x, ξ ; the domain of the latter dep ends on the constan ts of the first in tegrals. 9 4 Singularit ies of th e indu ced sympl ectic s tructure The Hamilto nia n structure of the system (1.1) is provided b y the Pois son brac kets on R 9 ( ω , α , β ). In notation (2.4) these brac k ets are [2] { M j , M k } = ε j k l M l , { M j , α k } = ε j k l α l , { M j , β k } = ε j k l β l , { α j , α k } = { α j , β k } = { β j , β k } = 0 . (4.1) Being restricted to P 6 they correspo nd to Kirillo v’s symplectic form λ ∈ Λ 2 ( P 6 ). Recall the follo wing we ll-kno wn facts. Let N ⊂ P 6 b e a submanifold defined in P 6 b y t w o indep enden t equations f 1 = 0 , f 2 = 0 (4.2) and let X 1 , X 2 b e the Hamiltonian v ector fields with the Hamilton functions f 1 , f 2 . Then the span of X 1 , X 2 at eac h p oin t ζ ∈ N is sk ew orthogo nal to the tangent space T ζ N . Therefore t he restriction of λ to N is non-degenerate at the p o in t ζ if and only if { f 1 , f 2 } ( ζ ) = λ ( X 1 , X 2 )( ζ ) 6 = 0 . (4.3) Let us calculate the bra c ket { R 1 , R 2 } of the functions (1.13). As R 1 is pure imag inary denote R = 1 i { R 1 , R 2 } . (4.4) The ch ange of v a riables (1.7) is linear with constan t co efficien ts, so the rules ( 4.1) are easily transformed for new co ordinates. Omitting tec hnical details w e presen t R in t he fo rm R = F 1 w 3 1 w 3 2 w 2 3 [ w 3 ( w 3 F 2 + F 3 ) 2 − F 4 ] , (4.5) where F 1 = z 1 z 2 w 3 + x 2 z 1 w 1 + x 1 z 2 w 2 , F 2 = w 1 w 2 w 3 + z 2 w 1 + z 1 w 2 , F 3 = 2 w 2 1 w 2 2 + x 2 w 2 1 + x 1 w 2 2 , F 4 = 4 w 2 1 w 2 2 [( w 2 1 w 2 2 + x 2 w 2 1 + x 1 w 2 2 ) w 3 + x 2 z 1 w 1 + x 1 z 2 w 2 ] . (4.6) The v ariables y 1 , y 2 ha v e b een eliminated as the solution of the system (1.12) y 1 = − w 1 w 3 ( x 2 w 1 + z 2 w 3 ) + F 1 w 1 w 2 w 3 , y 2 = − w 2 w 3 ( x 1 w 2 + z 1 w 3 ) + F 1 w 1 w 2 w 3 . (4.7) Fixing the v alues h, k , g , s, τ of the functions (1.3), (2.11), (2.12) we ha v e w 3 F 2 + F 3 = 2 w 1 w 2 h − 2( x 1 x 2 + z 1 z 2 − τ ) , F 4 = 4 w 2 1 w 2 2 w 3 ( τ − k ) . (4.8) Then from (2 .14), (3 .3), (3.4), (3.8), (3.9) w e obtain w 3 F 2 + F 3 = ξ s ( p 2 − τ 2 s − s ) , F 4 = − σ ξ 2 w 3 4 s 4 , F 1 = ξ w 3 , w 3 1 w 3 2 = ξ 3 8 s 3 . (4.9) Finally , the expression (4.5) ta k es the f o rm R = 8 s  s 4 − ( p 2 − τ ) s 2 + p 4 − r 4 4  . ( 4 .10) 10 Ob viously , R is a first integral of the induced system, and the equation s 4 − ( p 2 − τ ) s 2 + p 4 − r 4 4 = 0 (4.11 ) defines the set of the in tegral constants s, τ suc h t ha t on the corresp onding inte gral ma nif o lds the 2-form induced on O b y t he symplectic structure λ degenerates. As the functions (2.11), (2.12) ha v e an algebraic structure, the set (4.11) has co dimension 1 in O . Th us, λ | O is almost ev erywhere non-degenerate. T o lo cate the set (4.11) on the surface (2.1 4) in R 3 ( h, k , g ) notice that, in virtue of (2.14), ∂ ∂ s ( h, k , g ) × ∂ ∂ τ ( h, k , g ) =  s 4 − ( p 2 − τ ) s 2 + p 4 − r 4 4  ( τ − p 2 2 s 4 , 1 2 s 3 , 1 s 4 ) . Therefore, the equation (4.11) defines cuspidal edges of the surface (2.14). 5 Bifurcation diagram and the existenc e of motion s In tro duce the in tegral map J of t he dynamical system o n O J ( ζ ) = ( S ( ζ ) , T( ζ )) ∈ R 2 , ζ ∈ O . (5.1) The bifurcation diagram Σ( J ) of this map is, by definition, the set of pairs ( s, τ ) ov er whic h J is not lo cally trivial. In our case all in tegral manifolds (3.1) are compact. Therefore, Σ( J ) is the set of critical v alues of J . Define the admis s ible r e gion a s the image of the map (5.1), i.e., the set o f v alues ( s, τ ) suc h that the in tegral manifold (3.1) is not empt y . Obv iously , ∂ J ( O ) ⊂ Σ( J ). Due to the ab o v e results the existence o f a t r a j ectory o n O with give n s, τ is equiv alen t to the existence of a p oin t on the ( x, ξ )-plane f o r whic h the v alues (3.26)–(3.28), (3.35), (3.35) satisfy (3.7). It easily follows f rom (3.25), (3.28), (3.8) that the conditions (3.7), in turn, a re equiv alen t to the system o f inequalities Φ 1 ( x, ξ ) > 0 , Φ 2 ( x, ξ ) 6 0 , (5.2 ) Ψ 1 ( x, ξ ) > 0 , Ψ 2 ( x, ξ ) 6 0 (5.3) considered in the quadran t x > 0, s ξ > 0. Theorem 3. The bi f ur c ation di agr am Σ( J ) c onsists of the fol lowing subsets of the ( s, τ ) -plan e : 1 ◦ ) τ = ( a + b ) 2 , s ∈ [ − a, 0) ∪ [ b, + ∞ ); 2 ◦ ) τ = ( a − b ) 2 , s ∈ [ − a, − b ] ∪ (0 , + ∞ ); 3 ◦ ) s = − a, τ > ( a − b ) 2 ; 4 ◦ ) s = − b, τ > ( a − b ) 2 ; 5 ◦ ) s = b, τ 6 ( a + b ) 2 ; 6 ◦ ) s = a, τ 6 ( a + b ) 2 ; 7 ◦ ) τ = 0 , s ∈ (0 , + ∞ ); 8 ◦ ) τ = ( √ a 2 − s 2 + √ b 2 − s 2 ) 2 , s ∈ [ − b, 0) ; 9 ◦ ) τ = ( √ a 2 − s 2 − √ b 2 − s 2 ) 2 , s ∈ (0 , b ]; 10 ◦ ) τ = − ( √ s 2 − a 2 − √ s 2 − b 2 ) 2 , s ∈ [ a, + ∞ ) . 11 Theorem 4. The so l utions of the system (1.1) under the c onditions (1.1 2) exist iff the c onstants of the first i n te gr als (2.11) , (2.12) satisfy one of the fol low i n g 1 ◦ ) − a 6 s 6 − b, τ > ( a − b ) 2 ; 2 ◦ ) − b 6 s < 0 , τ > ( p a 2 − s 2 + p b 2 − s 2 ) 2 ; 3 ◦ ) 0 < s 6 b, τ 6 ( p a 2 − s 2 − p b 2 − s 2 ) 2 ; 4 ◦ ) b 6 s 6 a, τ 6 ( a + b ) 2 ; 5 ◦ ) s > a, − ( p s 2 − b 2 − p s 2 − a 2 ) 2 6 τ 6 ( a + b ) 2 . The complete pro of of these statemen ts is purely techn ical (see [1 0 ]) and con tains the scrupu- lous a nalysis o f the regions on the ( x, ξ )-plane defined by (5 .2), (5.3) and the cases of their structural transformatio ns. Anot her a pproac h is suggested in [1 1] for t he pair ( S, H ). It is based on the classification of the tra jectories in O satisfying the condition rank ( H × K × G ) < 2. Figure 1: The admissible regio n in the ( s, τ )- plane. The admissible region is shaded in Fig.1. The dense lines and curv es represen t t he equations of the bifurcat io n diagram, the dashed curv e illustrates the equation (4.11), i.e., the first in tegrals constan ts suc h that the symplectic structure is degenerate on the corresp onding in tegral manifolds. 6 Separation of v ariables In the sequel w e supp ose that τ σ 6 = 0. In fact, if τ = 0, then from (2.14) w e obtain the relation (2 g − p 2 h ) 2 = r 4 k c har acteristic for the critical manifold N [9]. The equations of motion on N w ere explicitly inte grated in [8]. If σ = 0, then the equations (2.14 ) yield one of the relations (1.11). This case corresp onds to t he set of p oints (1.9). At these p oin ts the manifold O fails to b e smo oth. The corresp onding tra jectories are the p endulum motions (1.10). Considering the second equation (3.21) denote µ = | r 2 x 1 − τ y 1 | = | r 2 x 2 − τ y 2 | . Then µ 2 = τ ξ 2 + σ x 2 − τ σ . (6 .1) This equation defines t he second-order surface M in three-dimensional space R 3 ( x, ξ , µ ). Each tra jectory in O is in a natural wa y represen ted b y a curve on M . 12 Theorem 5. Supp osing τ σ 6 = 0 , i n tr o duc e the variables U = τ ξ + xµ √ σ ( τ − x 2 ) , V = τ ξ − xµ √ σ ( τ − x 2 ) . (6.2) Then the e quations of motion on O sep ar ate dU p Q ( U ) − dV p Q ( V ) = 0 , U dU p Q ( U ) − V dV p Q ( V ) = dt p 2 sτ σ . (6.3) Her e Q ( w ) = ( w 2 − 1)( σ w 2 − 4 s 2 χ 2 )[( √ σ w + τ ) 2 − r 4 ] . (6.4) Pr o of. Consider the lo cal co ordinates u, v on the surface M : ξ = √ σ uv + 1 u + v , x = √ τ u − v u + v , µ = √ τ σ uv − 1 u + v . (6.5) In a ddition to (3 .1 9) note the following tw o iden tities for the constants in tro duced ab ov e, σ + 2 τ ( p 2 ± r 2 ) = ( τ ± r 2 ) 2 . (6.6) The p olynomials (3.15), (3.24), (3.36 ) b ecome Φ 1 = κ ϕ 1 ( u ) ϕ 1 ( v ) , Φ 2 = κ ϕ 2 ( u ) ϕ 2 ( v ) , Ψ 1 = κ ψ 1 ( u ) ψ 2 ( v ) , Ψ 2 = κ ψ 2 ( u ) ψ 1 ( v ) , Θ 1 = κ θ 2 ( u ) θ 1 ( v ) , Θ 2 = κ θ 1 ( u ) θ 2 ( v ) , where κ = 1 / ( u + v ) 2 and ϕ 1 ( w ) = √ σ (1 + w 2 ) + 2( τ + r 2 ) w , ϕ 2 ( w ) = √ σ (1 + w 2 ) + 2( τ − r 2 ) w , ψ 1 ( w ) = 2 s [( χ + √ τ ) w 2 − ( χ − √ τ )] , ψ 2 ( w ) = 2 s [( χ − √ τ ) w 2 − ( χ + √ τ )] , θ 1 ( w ) = √ σ (1 − w 2 ) + 4 s √ τ w , θ 2 ( w ) = √ σ (1 − w 2 ) − 4 s √ τ w . Then from (3 .26)–(3.28) w e find the expressions fo r the configuration v a riables x 1 = 2 sτ r 2 " p ϕ 1 ( u ) ϕ 2 ( v ) + p ϕ 2 ( u ) ϕ 1 ( v ) p θ 1 ( u ) θ 1 ( v ) − p θ 2 ( u ) θ 2 ( v ) # 2 , x 2 = 2 sτ r 2 " p ϕ 1 ( u ) ϕ 2 ( v ) − p ϕ 2 ( u ) ϕ 1 ( v ) p θ 1 ( u ) θ 1 ( v ) + p θ 2 ( u ) θ 2 ( v ) # 2 , (6.7) y 1 = 2 s h p ϕ 1 ( u ) ϕ 2 ( v ) + p ϕ 2 ( u ) ϕ 1 ( v ) i 2 − 4 σ ( u v − 1) 2 h p θ 1 ( u ) θ 1 ( v ) − p θ 2 ( u ) θ 2 ( v ) i 2 , y 2 = 2 s h p ϕ 1 ( u ) ϕ 2 ( v ) − p ϕ 2 ( u ) ϕ 1 ( v ) i 2 − 4 σ ( uv − 1) 2 h p θ 1 ( u ) θ 1 ( v ) + p θ 2 ( u ) θ 2 ( v ) i 2 , (6.8) z 1 = 1 2 r ( u + v ) h p ϕ 1 ( u ) ϕ 1 ( v ) + p ϕ 2 ( u ) ϕ 2 ( v ) i , z 2 = 1 2 r ( u + v ) h p ϕ 1 ( u ) ϕ 1 ( v ) − p ϕ 2 ( u ) ϕ 2 ( v ) i . (6.9) 13 Hence, in particular, √ x 1 = p 2 s τ r p ϕ 1 ( u ) ϕ 2 ( v ) + p ϕ 2 ( u ) ϕ 1 ( v ) p θ 1 ( u ) θ 1 ( v ) − p θ 2 ( u ) θ 2 ( v ) , √ x 2 = p 2 s τ r p ϕ 1 ( u ) ϕ 2 ( v ) − p ϕ 2 ( u ) ϕ 1 ( v ) p θ 1 ( u ) θ 1 ( v ) + p θ 2 ( u ) θ 2 ( v ) . (6.10) Here the arbitrary c hoice o f sign is provided by the algebraic v alue √ 2 sτ . F ro m (3.35) w e hav e √ x 2 w 1 = i 4 s p θ 2 ( u ) θ 1 ( v ) + p θ 1 ( u ) θ 2 ( v ) u + v , √ x 1 w 2 = i 4 s p θ 2 ( u ) θ 1 ( v ) − p θ 1 ( u ) θ 2 ( v ) u + v . (6.11) Substitute (6.10) in to (6.11) t o obtain the expressions f o r the v ariables defining the equatorial comp onen ts of the angular v elo cit y w 1 = ir 4 s √ 2 sτ h p θ 2 ( u ) θ 1 ( v ) + p θ 1 ( u ) θ 2 ( v ) i h p θ 1 ( u ) θ 1 ( v ) + p θ 2 ( u ) θ 2 ( v ) i ( u + v ) h p ϕ 1 ( u ) ϕ 2 ( v ) − p ϕ 2 ( u ) ϕ 1 ( v ) i , w 2 = ir 4 s √ 2 sτ h p θ 2 ( u ) θ 1 ( v ) − p θ 1 ( u ) θ 2 ( v ) i h p θ 1 ( u ) θ 1 ( v ) − p θ 2 ( u ) θ 2 ( v ) i ( u + v ) h p ϕ 1 ( u ) ϕ 2 ( v ) + p ϕ 2 ( u ) ϕ 1 ( v ) i . (6.12) The axial comp onen t is f o und fr o m (3.35), w 3 = i 2 √ 2 sτ σ p θ 1 ( u ) θ 2 ( u ) ϕ 1 ( v ) ϕ 2 ( v ) − p ϕ 1 ( u ) ϕ 2 ( u ) θ 1 ( v ) θ 2 ( v ) ( u + v )( u v − 1) . ( 6 .13) Th us w e hav e express ed a ll phase v aria bles in terms of u, v . T o o bta in t he differential equations for u, v consider the follow ing v ariables s 1 = x 2 + z 2 + r 2 2 x , s 2 = x 2 + z 2 − r 2 2 x . (6.14) The deriv ativ es, in virtue of t he system (1.8), a re s ′ 1 = r 2 4 x 3 ( z 1 + z 2 )( x 1 w 2 − x 2 w 1 ) , s ′ 2 = r 2 4 x 3 ( z 1 − z 2 )( x 1 w 2 + x 2 w 1 ) . (6.15) On the other hand, from (6.14), (6.5) w e ha v e s 1 = √ σ ( uv + 1) + ( τ + r 2 )( u + v ) 2 √ τ ( u − v ) , s 2 = √ σ ( uv + 1) + ( τ − r 2 )( u + v ) 2 √ τ ( u − v ) , whence ∂ s 1 ∂ u = − ϕ 1 ( v ) 2 √ τ ( u − v ) 2 , ∂ s 1 ∂ v = ϕ 1 ( u ) 2 √ τ ( u − v ) 2 , ∂ s 2 ∂ u = − ϕ 2 ( v ) 2 √ τ ( u − v ) 2 , ∂ s 2 ∂ v = ϕ 2 ( u ) 2 √ τ ( u − v ) 2 . 14 Therefore, du dt = 2 √ τ ( u − v ) 2 ϕ 1 ( u ) ϕ 2 ( v ) − ϕ 2 ( u ) ϕ 1 ( v ) [ ϕ 2 ( u ) ds 1 dt − ϕ 1 ( u ) ds 2 dt ] , dv dt = 2 √ τ ( u − v ) 2 ϕ 1 ( u ) ϕ 2 ( v ) − ϕ 2 ( u ) ϕ 1 ( v ) [ ϕ 2 ( v ) ds 1 dt − ϕ 1 ( v ) ds 2 dt ] . (6.16) Substitute the v alues (6.9) –(6.11) into (6.15) and the resulting expressions in to (6 .16). W e obtain f ( u, v ) du dt = p ϕ 1 ( u ) ϕ 2 ( u ) θ 1 ( u ) θ 2 ( u ) 2 u p 2 s τ σ , f ( u, v ) dv dt = p ϕ 1 ( v ) ϕ 2 ( v ) θ 1 ( v ) θ 2 ( v ) 2 v p 2 s τ σ , (6.17) where f ( u, v ) = ( u − v )(1 − uv ) uv =  v + 1 v  −  u + 1 u  . The v ariables (6.2) in terms of u, v hav e the fo rm U = 1 2  u + 1 u  , V = 1 2  v + 1 v  . (6.18) T o b e definite choose u = U − p U 2 − 1, v = V − p V 2 − 1. Then the equations (6.17) yield ( U − V ) dU dt = 1 √ 2 s τ σ p Q ( U ) , ( U − V ) dV dt = 1 √ 2 s τ σ p Q ( V ) (6.19) with the p olynomial (6 .4) of degree 6. This system is obvious ly equiv alent to the system (6.3); the la tter hav e the standard form for hy p erelliptic quadratur es. T o rev eal the connection of Theorem 5 with the bifurcation diagram supp ose that the p oly- nomial (6.4) has a multiple ro ot. The r esultant of Q ( w ) and Q ′ ( w ) is 2 32 a 4 b 4 ( a 2 − b 2 ) 2 s 10 τ 12 σ 8 χ 2 ( a 2 − s 2 ) 2 ( b 2 − s 2 ) 2 . (6.20) According to (2.14), s 6 = 0 on O . The equation σ = 0 g iv es τ = ( a ± b ) 2 . The case χ = 0 provide s the v alues τ = ( p a 2 − s 2 ± p b 2 − s 2 ) 2 . Thus , the bifurcatio n diagram o f J = S × T b elongs to the discriminan t set o f the p olynomial (6.4). This fact is t ypical for systems with separating v ariables. Note that all ro ots o f the p olynomial (6.4) are explicitly expresse d in terms of the in tegral constan ts a long with the ro ots of the p o lynomial ϕ 1 ( w ) ϕ 2 ( w ) θ 1 ( w ) θ 2 ( w ) (6.21) defining the solutions of the system (6 .17). The v ar ia bles in tro duced in this section a re r eal only in the case τ > 0 and σ > 0. F or ot her combinations of signs the definition (6.5) of the lo cal co ordinates u , v needs o b vious mo difications. Then the interv als of o scillations for the v ariables U, V and u , v are easily determined for any giv en v a lues of s, τ or, more exactly , for each connected comp o nen t o f R 2 \ Σ( J ). The obtained differen tial equations and the explicit formulae for the phase v ariables in terms of u, v provide the p o ssibilit y to in v estigate the phase top ology of the case considered and to calculate analytically the n umerical in v aria n ts of the corresp onding Liouville foliation. 15 References [1] M. P . Kharlamo v. Bifurcation diagra ms of the Kow alevski top in t w o constan t fields. R e gul. Chaotic D yn. , 10 (200 5), 381–39 8 . [2] O. I. Bogoy avle nsky . Euler equations on finite-dimension Lie algebras arising in phys ical prob- lems. Commun. Math. Phys. , 95 (198 4), 307–31 5 . [3] A. G. Reyman, M. A. Semeno v-Tian-Shansky . Lax represen tation with a sp ectral parameter for the Kow alewski top and its generalizations. L ett. Math. Ph ys. , 14 (1987), 55 –61. [4] M. P . Kharlamo v. Critical set and bifurcation diagram of the pro blem of motion of the Ko w a levski top in do uble field. Me ch. Tver d. T el a , N 34, 2004, 47 –58. (In R ussian) [5] S. Kow alevski. Sur le probl` eme de la rotation d’un cor ps solide autour d’un p oint fixe. A cta Math. , 12 (188 9), 177 –232. [6] G. G. App elro t . Non-completely symmetric hea vy gyroscop es. In: Motion of a rigid b o dy ab out a fixe d p oint . Collection of pap ers in memory of S.V.Kov alevsk ay . Acad. Sci. USSR, Mosco w- Leningrad, 1940, 61–15 6 . (In Russian) [7] D. B. Z o tev. F o menk o-Z iesc hang inv ariant in the Bogoy av lenskyi case. R e gul. Chaotic Dyn. , 5 (2000), 4 3 7–458. [8] M. P . Kharlamo v, A. Y. Sa vush kin. Separat io n of v ariables and integral ma nif o lds in one par - tial problem of motion o f the generalized Ko w alevski top. Ukr. Math. Bul l. , 1 (2004), 548–565 . [9] M. P . Kharlamo v. One class of solutions with tw o in v ar ian t relat io ns in the problem of motion of the Kow alevsky top in double constan t field. Mekh. tver d. tela , N 32 , 2002 , 3 2–38. (In Russian) [10] M. P . Kharlamov . Bifurcation diagram of the generalized 4th App elrot class. Mekh. tver d. tela , N 35, 2005 , 3 8–48. (In Russian) [11] M. P . Kharlamov , E. G. Sh v edo v. On the existence of motions in the generalized 4th App elrot class. R e gul. Chao tic Dyn. , 11 (2 0 06), 33 7–342. 16

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