# Cantilever beam optimization with finite difference gradients ```python '''Cantilever beam optimization with finite difference gradients''' import numpy as np from modopt import ProblemLite, SLSQP import time E0, L0, b0, vol0, F0 = 1., 1., 0.1, 0.01, -1. def get_problem(n_el): # 16 statements excluding comments, returns, and jac function. E, L, b, vol = E0, L0, b0, vol0 L_el = L / n_el n_nodes = n_el + 1 def obj(x): # Moment of inertia I = b * x**3 / 12 # Force vector F = np.zeros((n_nodes*2,)) F[-2] = F0 # Stiffness matrix c_el = E / L_el**3 * np.array([[12, 6*L_el, -12, 6*L_el], [6*L_el, 4*L_el**2, -6*L_el, 2*L_el**2], [-12, -6*L_el, 12, -6*L_el], [6*L_el, 2*L_el**2, -6*L_el, 4*L_el**2]]) K = np.zeros((n_nodes*2, n_nodes*2)) for i in range(n_el): K[2*i:2*i+4, 2*i:2*i+4] += c_el * I[i] # Displacement vector - solve for u in Ku = F # Apply boundary conditions: u[0] = u[1] = 0, # F[0:1] are unknown reaction forces at the left end. F[0:1] = K[0:1,2:].dot(u[2:]) u = np.concatenate(([0., 0.], np.linalg.solve(K[2:,2:], F[2:]))) # # Construction of sparse stiffness matrix from dense and solution # A_sparse = sp.csr_matrix(K[2:,2:]) # u = np.concatenate(([0., 0.], sp.linalg.spsolve(A_sparse, F[2:]))) # # Construction of sparse stiffness matrix and solution # nnz = 4 + 12 * (n_el - 1) # data = np.zeros((nnz,)) # rows = np.zeros((nnz,), dtype=int) # cols = np.zeros((nnz,), dtype=int) # data[0:4] = c_el[2:,2:].flatten() * I[0] # rows[0:4] = np.array([0, 0, 1, 1]) # cols[0:4] = np.array([0, 1, 0, 1]) # j = 4 # for i in range(1, n_el): # # NW quadrant: sum with SE quadrant of previous element # data[j-4:j] += c_el[:2,:2].flatten() * I[i] # # NE quadrant # data[j:j+4] = c_el[:2,2:].flatten() * I[i] # rows[j:j+4] = np.array([2*i-2, 2*i-2, 2*i-1, 2*i-1]) # cols[j:j+4] = np.array([2*i, 2*i+1, 2*i, 2*i+1]) # # SW quadrant # data[j+4:j+8] = c_el[2:,:2].flatten() * I[i] # rows[j+4:j+8] = np.array([2*i, 2*i, 2*i+1, 2*i+1]) # cols[j+4:j+8] = np.array([2*i-2, 2*i-1, 2*i-2, 2*i-1]) # # SE quadrant # data[j+8:j+12] = c_el[2:,2:].flatten() * I[i] # rows[j+8:j+12] = np.array([2*i, 2*i, 2*i+1, 2*i+1]) # cols[j+8:j+12] = np.array([2*i, 2*i+1, 2*i, 2*i+1]) # j += 12 # K_sparse = sp.csc_matrix((data, (rows, cols)), shape=(2*n_nodes-2, 2*n_nodes-2)) # u = np.concatenate(([0., 0.], sp.linalg.spsolve(K_sparse, F[2:]))) # Compliance c = F.dot(u) return c def con(x): return np.array([L/n_el * b * np.sum(x) - vol]) def jac(x): return L/n_el * b * np.ones((1, n_el)) return ProblemLite(x0=np.ones(n_el), obj=obj, con=con, jac=jac, name=f'cantilever_{n_el}_fd', xl=1e-2, cl=0., cu=0.) if __name__ == '__main__': # # Test to see if the problem is correctly defined # prob = get_problem(50) # print(prob._compute_objective(np.ones(50))) # 39.99999999905752 # print(prob._compute_constraints(np.ones(50))) # [0.09] # exit() # SLSQP print('\tSLSQP \n\t-----') n_el = 50 optimizer = SLSQP(get_problem(n_el), solver_options={'maxiter': 1000, 'ftol': 1e-9}) start_time = time.time() optimizer.solve() opt_time = time.time() - start_time success = optimizer.results['success'] print('\tTime:', opt_time) print('\tSuccess:', success) print('\tOptimized vars:', optimizer.results['x']) print('\tOptimized obj:', optimizer.results['fun']) optimizer.print_results() import matplotlib.pyplot as plt plt.figure() plt.plot(optimizer.results['x']) plt.xlabel('Lengthwise location') plt.ylabel('Optimized thickness') plt.show() assert np.allclose(optimizer.results['x'], [0.14915754, 0.14764328, 0.14611321, 0.14456715, 0.14300421, 0.14142417, 0.13982611, 0.13820976, 0.13657406, 0.13491866, 0.13324268, 0.13154528, 0.12982575, 0.12808305, 0.12631658, 0.12452477, 0.12270701, 0.12086183, 0.11898809, 0.11708424, 0.11514904, 0.11318072, 0.11117762, 0.10913764, 0.10705891, 0.10493903, 0.10277539, 0.10056526, 0.09830546, 0.09599246, 0.09362243, 0.09119084, 0.08869265, 0.08612198, 0.08347229, 0.08073573, 0.07790323, 0.07496382, 0.07190453, 0.06870925, 0.0653583, 0.06182632, 0.05808044, 0.05407658, 0.04975295, 0.0450185, 0.03972912, 0.03363155, 0.02620192, 0.01610863], rtol=0, atol=1e-5) ```