Nonholonomic variational systems Jana Musilová Masaryk University Brno Olga Rossi University of Ostrava La Trobe University, Melbourne Abstract - I The inverse variational problem is a natural part of calculus of variations. There is a question if given equations of motion arise from a Lagrangian system, or not. This is completely answered by Helmholtz conditions. In our presentation we deal with the nonholonomic mechanics. The inverse problem of the calculus of variations for second order ODE in the context of nonholonomic constraints is investigated. Relationships between Chetaev equations, constrained Euler-Lagrange equations coming from a nonholonomic variational principle, closed 2-forms on constraint manifolds, and a corresponding generalization of Helmholtz conditions are studied. Abstract – II It appears that every unconstrained variational system remains variational under an arbitrary nonholonomic constraint. On the other hand, the appropriate constraint can be used for transforming an initially non-variational system to the constraint variational one. We present some simple examples. The approach is based on the geometrical theory of nonholonomic mechanics on fibred manifolds, first presented and developed by Olga Rossi. Outline of the presentation Setting of the problem Fibred manifolds, variational systems, Helmholtz conditions Nonholonomic structure, reduced equations, constraint calculus Nonholonomic variational systems, nonholonomic Helmholtz conditions Examples: ballistic motion, damped planar oscillator Setting of the problem mechanical system ( t , q , q ), 1 m nonholonomic constraint f ( t , q , q ) 0, 1 i k , 1 k m 1 i Chetaev constraint force i f i F , rank k q q Chetaev equations d L i f q dt q q f L ChE with constraints: system of i i m +k mixed 1st and 2nd order ODE for m components of the system trajectory c(t) and k Lagrange multipliers μiσ Fibred manifolds – general fibred manifold and their jet prolongations (Y , , X ), : Y X , dim X n , dim Y n m , J Y J r sections r 1 Y J Y Y X 1 : X Y , id X , : X J Y , r id X , r J , J ( t ) ( t , q ( t ), q ( t ), r q-forms r , q ( r ) ( t )) horizontal: 0 for every vertical v. field on J Y r contact: J 0 for every sect ion of r * k contact: is ( k 1) contact for every vertic al canonical decom position : r 1, r h p1 * p q Fibred manifolds - notation used prolongations of (Y , π , X) 1 2 J Y (evolution space of the system ), J Y fibred coordinates Y: (V , ), ( t , q ), (U , ), U (V ), ( t ) 1 J Y : (V1 , 1 ), V1 (1,0 ) (V ), 1 ( t , q , q ) 1 1 J Y : (V 2 , 2 ), V 2 ( 2 ,0 ) (V ), 2 ( t , q , q , q ) 2 contact bases of 1-forms J Y : (d t , , d q ) 1 J Y : (d t , , , d q ) 2 dq q dt, dq q dt Variational (Lagrangian) system - 1st order variational ( ) S [ ] integral J 1 * L (t , q , q ) d t horizontal 1-form variational derivative ( ) d S [ u ] du u 0 1 d 1 u u 0u , ( u , 0u ) 1st variational formula du * J J 1 1 * u 0 one-param eter group of ( , 0 ) * L dt 1 0u ( ) J J 1 1 J u J J 1 d 1 * L q J J 1 1 * Lepage equivalent o f Variational system – motion equations Extremals stationary sections of the variational integral d S [ u ] du 0 J J 1 d 0 fo r every vert ical 1 * u 0 Euler-Lagrange form L E p1 d , E E d t , E q d L dt q Euler-Lagrange equations E J 0, E 2 J 0 J 2 1 * J 1 d 0, 1 m Dynamical system – inverse problem dynamical E E (t , q , q , q ) d t , 1 m form E A ( t , q , q ) B ( t , q , q ) q associated mechanical system A d t B d q F E p1 , [ ] A d t B d q equations of motion m o d 2 -co n t J 0 1 * 1 vertical vecto r field o n J Y main theorem of the inverse problem 1 The dynamical system [α] is variational iff it contains a closed representative. Then it is unique. Helmholtz conditions Helmholtz conditions of variationality { B } alt ( , ) A d B q d t sym ( , ) 0, A 1 d A 0 2 dt q q alt ( , ) B 0, q alt ( , ) F F , F A 1 A 4 q q Lagrangian (e.g. Vainberg-Tonti) 1 L q 0 0 E ( t , uq , uq , uq ) d u Nonholonomic structure - notations constraint submanifold canonical embedding canonical distribution constrained mechanical system Q : {( t , q , q ) J Y | q 1 m k i g ( t , q , q )} J Y i l 1 1 l m k , codim Q k : Q (t , q , q ) (t , q , q , q l l C span { }, 0 C i i * m k i m k i ( t , q , q )) J Y g i q l 1 l subbundle of T Q , codim C k physics: [ ] [ ], F d t geom etry: [ Q ] * m od 2 cont, I ( C ) 0 [ Q ] [ Al d t B ls d q ] l l Constraint calculus - I constraint derivative F F F F m k i l d c F (t , q , q ) dt dq d q d q mk i l t q q q l * F F l F i q g l m k i t q q i F F g l F F l i d t d q l m k i l l m k i q q q q q constraint derivative operators d c dt t q l q l g i q m k i , c q l q l g i q q l m k i , c q l q l i i d c c d c d c g l l c l g q , q , q l m k i l l t t q q dt t q dt dt q c Constraint calculus – II Euler-Lagrange constraint operators l c q l d c dt q l , l l q s 2 q q l s Chetaev vector fields Z Z 0 c t Z l c q l Z l q l Z 0 t Z l q i 0 i g l 0 l l Z g ( Z Z q ) Z , l m k i l q q q c c C span , l , l t q q l com ponents defined on Q , dim C 2 m 2 k 1 Reduced equations path of [αQ] (trajectory) in coordinates J Q 0, J 1 * 1 integral section of C for every 1 -vertical vector field C (q m k i g ) J 0, ( Al B ls q ) J 0 i 1 s 2 coefficients (Einstein summation) i j i i g g g g Al Al Am k i Bl ,m k i B m k j ,m k i q l l q q t q i i j i g g g g B ls B ls B l , m k i Bm k i ,s B m k j ,m k i s l l s q q q q Initially variational system unconstrained L (t , q , q ) d t Lagrangian system reduced equations consistent with the nonholonomic variational principle L0 g 2 Al l ( L 0 ) L i l ( g ), B ls i q q l 2 s Li q q l ( L 0 ) L i l ( g ) 0, 1 i k i L0 L , Li L q mk i i fu n ctio n s o n Q l s Nonholonomic variational systems Definition ~ the main Theorem (equivalent definition with that based of the nonholonomic variational principle) A constrained mechanical system [αQ] is called constraint variational, if it contains a closed representative. Proposition If a constrained system arises from an unconstrained variational system then it is constraint variational for an arbitrary constraint. Proof is the direct consequence of the definition αQ = ι*α Constraint Helmholtz conditions - I closed representative [ Q ], d 0, d Al d t B ls d q Fls l l s l s ( bi d t bil c il d q ) i j , Fls F sl , ij i l l i j ji constraint Lagrangian and reduced equations c L0 d t Li , L0 d t i bi L0 q m k i d c L i dt L0 2 bil q m k i q l Lj c Li q l g q L0 q l Li , l ( L0 ) Li l ( g ) 0 i j m k i , c il g j m k i q 2 Lj l q l i Li q , ij l Li mk j q (i, j ) Constraint Helmholtz conditions - II conditions for “free” functions bi , bil , cil , γil (1) B (2) 2gi B ls l r c is r q alt ( s , r ) q q alt ( s , r ) (3) 2 i Al d c B ls g i l ( g ) c is l s bi s d t s ym ( l . s ) q q q sym ( l , s ) (4 ) 1 d c Al s 2 d t q ls alt ( l , s ) 0 i 1 d c c Al c g i i ( l ( g ) c is ) l ( g ) bis bi s l s q q q alt ( l , s ) 2 d t alt ( l , s ) Constraint Helmholtz conditions - III bi , bil , cil , γil conditions for “free” functions (5) (6 ) Al q m k i B ls q m k i i 2 ij l ( g ) g 2 2 ij s 2-contact 2-form (7 ) q i q q l c bi l 2 bj bil q g s q q l c c is q l j m k i d c bil dt g 2 c js q q l bj q j m k i F 2 i 1 Al d c B ls g i Fls s l ( g ) c is bi l s 2 q dt q q alt ( l , s ) 1 Al A s 1 i i Fls s ( g ) c ( g ) c is s il l l 4 q q 4 g 0 j m k i 0 Constraint Helmholtz conditions - IV additional conditions for functions bi , bil , cil , γil (8) (9) bil bi q l d c c il dt c jl g q j m k i a d c ij bi h 2 ia 0 mk j mk i dt q q alt ( i , j ) C i c il (12) ( i C i ) c il l q ( t , q ) ij ij mk j mk j q alt ( i , j ) q alt ( i , j ) q l c il ( t , q ), ij m ki j (i , j ) (t , q ) q alt ( i , j ) (10) (11) i ( t , q , q ), C i ( t , q , q ), ij ( t , q , q ), c il ( t , q ), ij ( t , q ) l l l Classical mechanical systems – I unconstrained variational system 1 Lagrangian L E-L equations V d m 1 m q m q 0 2 q dt q 2 m q q V ( t , q ), m m const. constraint and reduced equations q m k i g ( t , q , q l ), Al B ls q 0 i s adding (non-variational) forces V 1 m d m q F m q 0, B B , A A F 2 q dt q Classical mechanical systems – II reduced equations i g s B ls B ls , Al Al Fl , Al B l s q Fl Fm k i 0 l q sufficient condition for variationality m –k equations for k (m –k ) unknown derivatives i i g g 0 Fl F m k i l l q q every solution (if exist any) leads to the variational system with the same cil , bil , bi as for the unconstrained case, and L0 L , Li L q m k i Example – ballistic motion - I motion in homogeneous gravitational field L 1 2 mx 2 1 m y m G y , m x 0, m G m y 0, y g ( t , x , y , x ) 2 2 m A 0 mG , B 0 0 d c g g , A1 m G m x dt g 2 , B11 m 1 x d c g b1 m G dt c11 m g x L0 L L1 L y g , b1 1 m x , 1 1 0 (antisym .) 1 2 mx g 2 2 mGy mg, * Example – ballistic motion - II comments to previous results (1), (2), (4) … automatically fulfilled by alternation, remaining conditions (3), (5), (6) give (3) 2 d c g g g m G 0 b1 1 ( g ) c11 m 2 x dt x (5) 2 d c g g g d c g c b1 d c b11 g m G b m b 0 11 1 xy dt x y dt x dt y (6) g g b1 1 c c11 0 c11 2 m xy x x x 2 b11 is given by (8) Example – ballistic motion - III ballistic curve motion in the homogeneous gravitational field with the additional non-variational friction force Stokes model x m x 0, m G y m y 0, F f v , y g ( t , x , y , x ) m A x , ( m G y ) , B 0 0 m 2 d c g g g g A1 m , B11 m 1 G x g x dt x x Example – ballistic motion - IV turning to the constraint variational system (I) xg g x 0 x x 2 g 2 0 g (t , x , y ) x d c 1 m , b11 b1 m G 2 2 x dt 2 x 2 x c1 1 (II) mx x 2 , 1 1 0 (antisym .) g x g 0 g x x (t , x , y ) (t , x , y ) x x 2 2 Example – ballistic motion - V special case of the constraint ( t , x , y ) v const., g 2 v x 2 reduced equation A1 B11 x 0 free functions mGx v x 2 b1 m G , b11 0, c11 2 mv v x 2 [Swacyzna, Volný] 2 v x 2 mx 2 2 x0 2 (*) , 11 0 (antisym .) constraint Lagrangian and reduced equation e.g. c m G y d t m v x 2 2 1 1 ( L 0 ) L1 1 ( g ) 0 the sam e as (*) Example – ballistic motion - VI other special case of the constraint (t , x , y ) 2 G y , g reduced equation A1 B11 x 0 mGx 2G y x free functions b1 2 m G , b11 0, c11 2 2G y x 2mGy 2G y x mx 2G y x 2 2 2 x0 (*) , 11 0 (antisym .) constraint Lagrangian and reduced equation e.g. c m 2G y x 2 1 i.e. L0 0 1 ( L 0 ) L1 1 ( g ) 0 the sam e as (*) Example – damped oscillator - I undamped oscillator – planar motion L 1 m(x y ) 2 2 2 1 k ( x y ), kx m x 0, ky m y 0, y g ( t , x , y , x ) 2 2 2 m A kx ky , B 0 0 m 2 g g A1 k x y , B11 m 1 m x x d t x g d c g b1 ky m L0 L d c g dt m 2 , b11 m x g 2 2 k 2 g x , c11 m x y 2 2 g x , L1 , 1 1 0 (antis ym .) L y mg , * Example – damped oscillator - II comments to previous results (1), (2), (4) … automatically fulfilled by alternation, remaining conditions (3), (5), (6) give (3) 2 d c g g g ky m b1 1 ( g ) c11 m 0 2 x dt x (5) 2 d c g g d c g g b1 k m ky m xy dt x y dt (6) g g b11 c c11 c 2 m 0 11 xy x x x 2 b11 is given by (8) g c b1 d c b11 b11 0 dt y x Example – damped oscillator - III damping frictional force added motion of the oscillator with considering the additional non-variational friction force - Stokes model kx x m x 0, ky y m y 0, F f v , y g ( t , x , y , x ) m A ( kx x ) , ( ky y ) , B 0 0 m 2 g g g A1 k x y x g m , B11 m 1 x x dt x x g d c g Example – damped oscillator - IV turning to the constraint variational system we can consider the same functions as for ballistic motion (I) xg b1 ky c1 1 (II) g x 0 x x m d c 2 x mx x 2 2 dt 2 g 2 0 , b1 1 g 2 m 2 x (t , x , y ) x 2 x , 1 1 0 (antisy m . ) g x g 0 g x x (t , x , y ) (t , x , y ) x x 2 Example – damped oscillator - V special case of the constraint ( t , x , y ) v const., g 2 v x 2 2 reduced equation A1 B11 x 0 k x free functions 2 mv 2 x0 2 2 2 v x v x xy mx b1 ky , b11 0, c11 v x 2 2 (*) , 11 0 (antisym .) constraint Lagrangian and reduced equation e.g. c 1 k ( x y ) dt m v x 2 2 2 2 1 ( L 0 ) L1 1 ( g ) 0 the sam e as (*) 2 1 Example – damped oscillator - VI “super” special case of the constraint x 2 m 2 y y g 2 2 x k 2E m 2 y x m k 2 2 E const. y 2 x 2 x 2 reduced equation (expected??) 2 x 1 2 kx m x 0 kx m x 0 g constraint Lagrangian c L 0 d t L1 , L1 m x L1 ( t , x , y ), L 0 ky L 0 , 1 ( L 0 ) 2 kx 1 2 2 e.g. L 0 E k ( x y ), L1 m x , i.e. L 0 L , L1 2 2 2 L y Example – damped oscillator - VII another special case of the constraint x m k y g y 2 2 x 2 x 2 reduced equation kx 2 kyx g kxx g 2 2 2 x mx 1 2 0 g constraint Lagrangian e.g. L0 0, L1 m x m 2 k m ( x y ) x , i.e. L 0 L , L1 2 2 2 L y Examples of open problems the problem of finding all solutions of constraint Helmholtz conditions for given unconstrained equations of motion and given constraint trivial constraint problem – for a given solution of constraint Helmholtz conditions to find all constraint Lagrangians leading to given reduced equations constraints leading to constraint variational system for initially non-variational equations References 0. 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