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Using infinitesimal symmetries for determining the first Maxwell time of geometric control problem on SH(2)
            X 1 , . . . , X k , this yields a system of order k, con-  manifold M of the system is three-dimensional,
            sisting of equations of the form Equation (8).    where, for any point q = (x, y, z) ∈ M, x and y
            Next, we compute the Lie derivative of g. We      are position variables and z is the angular orien-
            have:                                             tation variable of the unicycle on the hyperbolic
                                         !
                             n                                plane. A motion m(x, y, z) on the configuration
                           X
               L v (g) = L v   a i dq i ⊗ dq i                manifold M, parameterized by x, y, z ∈ R, is a
                            i=1                               transformation that maps a point a(a 1 , a 2 ) to a
                        n
                       X                                      point b(b 1 , b 2 ), such that:
                     =    a i L v (dq i ⊗ dq i )
                       i=1                                             b 1 = a 1 cosh z + a 2 sinh z + x,
                        n
                       X                                               b 2 = a 1 sinh z + a 2 cosh z + y.
                     =    2a i dq i L v (dq i )
                                                              Composition of two motions m 1 (x 1 , y 1 , z 1 ) and
                       i=1
                        n                                     m 2 (x 2 , y 2 , z 2 ) is another motion m 3 (x 3 , y 3 , z 3 )
                       X
                     =    2a i dq i (i(v) d(dq i ) + d(i(v) dq i ))  given as:
                       i=1                                       m 3 (x 3 , y 3 , z 3 ) = m 1 (x 1 , y 1 , z 1 ).m 2 (x 2 , y 2 , z 3 )
                        n
                       X                                      where,
                     =    2a i dq i d(i(v) dq i )
                                                                      x 3 = x 2 cosh z 1 + y 2 sinh z 1 + x 1 ,
                       i=1
                        n
                       X                                              y 3 = x 2 sinh z 1 + y 2 cosh z 1 + y 1 ,
                     =    2a i dq i d(dq i (v))
                                                                      z 3 = z 1 + z 2
                       i=1
            where i(v), is the interior product.  Condition   The identity motion m Id is given by x = y = z =
            L v (g) = 0 provides a system of order   n(n+1)  ,  0, and inverse of a motion m(x, y, z) is given by
                                                                          1
                                                                       1
                                                                    1
                                                       2      m −1 (x , y , z ) where,
            consisting of equations of the form:
                                                                          1
               n         n                n                              x = −x cosh z + y sinh z,
                             ∂h 1             ∂h n
              X         X                X
                  k i h i +  l i  + . . . +  r i   = 0, (9)              y = x sinh z − y cosh z,
                                                                          1
                             ∂q i             ∂q i
              i=1       i=1              i=1
                                                                          1
                                                                         z = −z.
            where k i , l i , and r i are some scalar functions.
            Soving the system associated with Equations (8)
                                                                  The motions of the pseudo-Euclidean plane
            and (9), we determine the functions h i and, con-
                                                              exhibit a group structure, with composition serv-
            sequently, the generators v i of our Lie algebra of
                                                              ing as the group operation. This group, known as
            symmetries. As a consequence, we can state the
                                                              the special hyperbolic group SH(2), also possesses
            following result:
                                                              a smooth manifold structure, which qualifies it as
            Proposition 2. The infinitesimal symmetries of    a Lie group. One can equivalently formulate prob-
            control system Equations (2)-(4) can be identified  lem Equation (10) as a sub-Riemannian problem
            by calculating the flow associated with the vector  on SH(2):
            field v i at time s, denoted by
                                                                  ˙ q = u 1 X 1 (q) + u 2 X 2 (q),
            γ i (s, t) = (q 1 (s, t), . . . , q n (s, t)). This flow is ob-                        2
            tained by solving the system of differential equa-    q ∈ M = SH(2),    u = (u 1 , u 2 ) ∈ R ,
            tions:                                                q(0) = q 0 = m Id ,  q(t 1 ) = q 1 ,   (11)
             ∂γ i (s, t)                                                Z  t 1
                     = v i (γ i (s, t)),  γ i (0, t) = (q 1 (t), . . . , q n (t)).  1  2  2
               ∂s                                                 J =        u + u 2  dt → min
                                                                               1
                                                                       2  0
            4. Infinitesimal symmetries on SH(2)              where,
                and the first Maxwell time
                                                                   X 1 = cosh z ∂ x + sinh z ∂ y ,  X 2 = ∂ z .
            4.1. Geometric control problem on SH(2)           The problem under consideration is formulated
                                                              on a sub-Riemannian manifold (M, ∆, g). Here,
            The motion of a unicycle on a hyperbolic plane
            can be described using the following driftless con-  M represents the underlying smooth manifold,
                                                              ∆ = span{X 1 , X 2 } denotes a distribution of rank
            trol system
                                                             2, and g is a Riemannian metric defined on ∆ such
                             ˙x = u 1 cosh z,
                                                              that g(X i , X j ) = δ ij , explicitly g = dx −dy +dz .
                                                                                                2    2    2
                               ˙ y = u 1 sinh z,       (10)
                                                              The vector fields X 1 and X 2 , which span the dis-
                            
                               ˙ z = u 2 ,                    tribution ∆, are left-invariant with respect to the
                            
            where u 1 is the translational velocity and u 2 is  group structure associated with M. One can see
            the angular velocity. The configuration and state  that the family
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