Complete Solutions for the Approximate Synthesis of Spherical Four-Bar Function Generators

Author:

O’Connor Sam11,Plecnik Mark1,Baskar Aravind1,Joo James2

Affiliation:

1. University of Notre Dame Department of Aerospace and Mechanical Engineering, , Notre Dame, IN 46556

2. Wright-Patterson Air Force Base Air Force Research Laboratory, Structures Technology Branch, Aerospace Systems Directorate, , OH 45433

Abstract

Abstract Kinematic synthesis to meet an approximate motion specification naturally forms a constrained optimization problem. Instead of using local methods, we conduct global design searches by direct computation of all critical points. The idea is not new, but performed at scale is only possible through modern polynomial homotopy continuation solvers. Such a complete computation finds all minima, including the global, which allows for a full exploration of the design space, whereas local solvers can only find the minimum nearest to an initial guess. We form equality-constrained objective functions that pertain to the synthesis of spherical four-bar linkages for approximate function generation. We consider the general case where all mechanism dimensions may vary and a more specific case that enables the placement of ground pivots. The former optimization problem is shown to permit 268 sets of critical points, and the latter permits 61 sets. Critical points are classified as saddles or minima through a post-process eigenanalysis of the projected Hessian. The discretization points are contained within the coefficients of the stationarity polynomials, so the algebraic structure of the synthesis equations remains invariant to the number of points. The results of our computational work were used to design a mechanism that coordinates the folding wings. We also use this method to parameterize mechanism dimensions for a family of hyperbolic curves.

Funder

Air Force Research Laboratory

Division of Civil, Mechanical and Manufacturing Innovation

Publisher

ASME International

Reference18 articles.

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