 LIB "orbitparam.lib";
ring R = 0,(t(1..3)),dp;
matrix L1[3][3] = 0,1,0, 0,0,0, 0,0,0;
matrix L2[3][3] = 0,0,1, 0,0,0, 0,0,0;
matrix L3[3][3] = 0,1,1, 0,0,1, 0,0,0;
list L = L1,L2,L3;
matrix v[3][1] = 1,2,3;
parametrizeOrbit(L,v);
==> [1]:
==> 2
==> [2]:
==> _[1,1]=1/6*t(1)^2+5/3*t(1)+t(2)+1
==> _[2,1]=t(1)+2
==> _[3,1]=3
==> [3]:
==> [1]:
==> 2
==> [2]:
==> 1
==> [4]:
==> [1]:
==> t(1)
==> [2]:
==> t(2)
ring R1 = 0,(t(1..2)),dp;
matrix L1[4][4] = 0,1,0,0, 0,0,0,0, 0,0,0,1, 0,0,0,0;
matrix L2[4][4] = 0,0,1,0, 0,0,0,1, 0,0,0,0, 0,0,0,0;
list L = L1,L2;
matrix v[4][1] = 1,2,3,4;
parametrizeOrbit(L,v);
==> [1]:
==> 2
==> [2]:
==> _[1,1]=1/4*t(1)*t(2)+1/2*t(1)+3/4*t(2)+1
==> _[2,1]=t(2)+2
==> _[3,1]=t(1)+3
==> _[4,1]=4
==> [3]:
==> [1]:
==> 3
==> [2]:
==> 2
==> [4]:
==> [1]:
==> t(1)
==> [2]:
==> t(2)
