The main goal of this work is to present an integrated system for the optimization of plane structures with elastoplastic behavior. The methodology proposes an alternative for the conservative way in which structures traditionally have been optimized, i.e., that they present linear elastic behavior. The computational system is said to be integrated because it congregates distinct modules for the solution of the problem, such as geometric modelling, finite element mesh generation, non-linear structural response analysis, sensitivity analysis, mathematical programming and optimization of structures. The geometry of the plane structure`s boundary is defined by cubic (parametric) B-splines curves. Those, in turn, are determined by a set of interpolation points (key points) and boundary constraints at their ends. The correct definition of the structure`s geometry is responsible for the success of the optimization process.The structural response to the applied loading is evaluated by the finite element method. For that, the domain of the structure must be discretized. In the present work, an automatic unstructured mesh generator of isoparametric finite elements has been used. The equilibrium layout of the structure is obtained by an iterative/incremental procedure using the standard Newton-Raphson method. Locally, the equilibrium is satisfied by applying an implicit stress return mapping algorithm at points which violate the yield criterion of the material. The tangent stiffness matrix is updated at each analysis iteration and it is obtained in a way which is consistent with the return mapping algorithm, so that the asymptotic quadratic rate of convergence of the Newton-Raphson method is preserved. The use of a quadratic recursive programming algorithm in the optimization procedure involves the gradient evaluation of the objective function and constraints. For that, a semi-analytical method for the calculation of the response sensitivities, which appear in the gradient expressions, has been implemented. The technique takes into account the plastic effects which take place during the loading of the structure and is considered - exact- up to round-off errors, which occurs when the magnitude of the perturbation is so small that the hardware cannot accurately represent it.The examples presented demonstrate that the consideration of the elastoplastic behavior of the material during the optimization process leads to structural layouts which are more efficient than of those obtained under the assumption of linear elastic relationship between strains and stresses.