def plot(self, U, V, ctr): X1 = arange(min(U) - 2, max(U) + 2, 0.1) x = [1] for i in range(len(U)): x = P.polymul(x, [-1 * U[i], 1]) plt.axis([-10, 10, min(V) - 1, max(V) + 1]) b = [0] for i in range(len(U)): a = P.polydiv(x, [-1 * U[i], 1]) b = P.polyadd( P.polymul((P.polydiv(a[0], P.polyval(U[i], a[0])))[0], [V[i]]), b) Y = P.polyval( X1, P.polymul((P.polydiv(a[0], P.polyval(U[i], a[0])))[0], [V[i]])) plt.plot(X1, Y, 'y') plt.plot(U, V, 'ro') X1 = arange(-5, 5, 0.1) Y = P.polyval(X1, b) plt.plot(X1, Y, 'b', label='Required Polynomial') plt.plot((-8, 8), (0, 0), 'k') plt.grid(b=True, which='both', color='0.65', linestyle='-') Y = list(Y) plt.plot((0, 0), (-max(Y) - 5, max(Y) + 5), 'k') plt.xlabel('x-axis') plt.ylabel('y-axis') plt.legend(loc=1) filename = "this_plot" + str(ctr) + ".png" path = "C:\\Users\HP\Anaconda3\static" fullpath = os.path.join(path, filename) plt.savefig(fullpath)
def chuck(samplerate, sig, shift_hz=1000): rc_imag = [ allpass(samplerate, rc) for rc in [5.49e-06, 4.75e-05, 2.37e-04, 1.27e-03] ] rc_real = [ allpass(samplerate, rc) for rc in [2.00e-05, 1.07e-04, 5.36e-04, 4.64e-03] ] sos_imag = [ signal.tf2sos( polynomial.polymul(rc1[0], rc2[0]), polynomial.polymul(rc1[1], rc2[1]), )[0] for rc1, rc2 in zip(rc_imag[::2], rc_imag[1::2]) ] sos_real = [ signal.tf2sos( polynomial.polymul(rc1[0], rc2[0]), polynomial.polymul(rc1[1], rc2[1]), )[0] for rc1, rc2 in zip(rc_real[::2], rc_real[1::2]) ] # plot_response(sys._getframe().f_code.co_name, sos_real, sos_imag) real = signal.sosfilt(sos_real, sig) imag = signal.sosfilt(sos_imag, sig) analytic = 0.5 * (real - 1j * imag) return pitch_shift(samplerate, analytic, shift_hz)
def getEpsrNumDen(Mat_pol, N_true_poles): ## create num and den list_num, list_den = [], [] for k in range(2 * N_true_poles): list_num.append((Mat_pol[1, k])) list_den.append((-Mat_pol[2, k], 1.)) den = (1) for k in range(2 * N_true_poles): den = poly.polymul(den, list_den[k]) inter = [] pinter = (1) for k1 in range(2 * N_true_poles): pinter = list_num[k1] for k2 in range(2 * N_true_poles): if (k1 != k2): pinter = poly.polymul(pinter, list_den[k2]) inter.append(pinter) num = inter[0] for k in range(1, 2 * N_true_poles): num = poly.polyadd(num, inter[k]) for k in range(len(num)): num[k] /= (1j)**k for k in range(len(den)): den[k] /= (1j)**k num, den = num.real, den.real # np.savetxt('text_num.out', num, delimiter=',') # np.savetxt('text_den.out', den, delimiter=',') num = poly.polyadd(num, den) w2 = (0., 0., -1.) num2 = poly.polymul(w2, num) # print_w2_chi(num2,den) # dnum2, dden = get_der_rational(num2,den) return (num, den, num2)
def get_extended_cycle(p, n, extender): newp = p**n - 1 a = [0, 1] curr = [0, 1] alphas = {0: [1], 1: a} for x in range(2, n): curr = pol.polymul(curr, a) alphas[x] = list(map(int, curr)) curr = list(map(lambda x: -x % p, extender[:-1])) curr = trim(curr) alphas[n] = curr for x in range(n + 1, newp): curr = pol.polymul(curr, a) while (len(curr) > n): nam = int(curr[-1] % p) curr = list( map( lambda x: int(x) % p, pol.polyadd( list(map(lambda x: x * nam, alphas[len(curr) - 1])), curr[:-1]))) curr = list(map(lambda x: int(x) % p, curr)) alphas[x] = list(map(int, curr)) return (alphas)
def plot(self,U,V,ctr): X1=arange(min(U)-2,max(U)+2,0.1) x=[1] for i in range(len(U)): x=P.polymul(x,[-1*U[i],1]) plt.axis([-10,10,min(V)-1,max(V)+1]) b=[0] for i in range(len(U)): a=P.polydiv(x,[-1*U[i],1]) b=P.polyadd(P.polymul((P.polydiv(a[0],P.polyval(U[i],a[0])))[0],[V[i]]),b) Y=P.polyval(X1,P.polymul((P.polydiv(a[0],P.polyval(U[i],a[0])))[0],[V[i]])) plt.plot(X1,Y,'y') plt.plot(U,V,'ro') X1=arange(-5,5,0.1) Y=P.polyval(X1,b) plt.plot(X1,Y,'b',label='Required Polynomial') plt.plot((-8,8),(0,0),'k') plt.grid(b=True, which='both', color='0.65',linestyle='-') Y=list(Y) plt.plot((0,0),(-max(Y)-5,max(Y)+5),'k') plt.xlabel('x-axis') plt.ylabel('y-axis') plt.legend(loc=1) filename = "this_plot"+str(ctr)+".png" path = "C:\\Users\HP\Anaconda3\static" fullpath = os.path.join(path, filename) plt.savefig(fullpath)
def get_der_rational(num, den): dnum = poly.polyder(num) dden = poly.polyder(den) dnum_den = poly.polymul(dnum, den) dden_num = poly.polymul(num, dden) num_new = poly.polysub(dnum_den, dden_num) den_new = poly.polymul(den, den) return (num_new, den_new)
def gram_schmidt(A): n = A.shape[1] # numero de vectores columna for j in range(n): for k in range(j): #A[:, j] -= np.dot(A[:, k], A[:, j]) * A[:, k] A[:, j] -= quad(P.polymul(A[:, k], A[:, j]), -1, 1) * A[:, k] A[:, j] = A[:, j] / quad(P.polymul(A[:, j], A[:, j]), -1, 1) return A
def test_coeff_convert(): """Test the function convertion from factored coeffs to end coeffs.""" assert np.allclose(fcoeffs2coeffs(np.array([1.0, 2, 1, 1])), P.polymul([1, 1, 2], [1, 1])) assert np.allclose(fcoeffs2coeffs(np.array([1.0, 2, 1.2])), P.polymul([1, 1, 2], 1.2)) assert np.allclose(fcoeffs2coeffs(np.array([1.0, 2])), P.polymul([1, 1], 2))
def egcd(a, b, p): x,y, u,v = np.array([0]),np.array([1]), np.array([1]),np.array([0]) while not np.all(a == 0): q, r = P.polydiv(b,a)[0]%p, P.polydiv(b, a)[1]%p print(q,r) m, n = (x-P.polymul(u, q))%p, (y-P.polymul(v,q))%p b,a, x,y, u,v = a,r, u,v, m,n gcd = b return gcd, x, y
def test_fcoeffs2coeffs(): """Test the function expanding factored polynomials""" assert np.allclose( fcoeffs2coeffs(np.array([1.0, 2, 1, 1])), P.polymul([1, 1, 2], [1, 1]) ) assert np.allclose( fcoeffs2coeffs(np.array([1.0, 2, 1.2])), P.polymul([1, 1, 2], 1.2) ) assert np.allclose(fcoeffs2coeffs(np.array([1.0, 2])), P.polymul([1, 1], 2))
def ButterworthD2(N, w, Ts): Nr = int(N / 2) a = np.array(myPoli.num(2 * Nr)) * Ts**(2 * Nr) * w**N b = np.array(myPoli.polynomialMultiplier(N, Nr)) if N % 2 == 1: n = [w * Ts + 2, w * Ts - 2] d = [w * Ts, w * Ts] b = poly.polymul(b, n) a = poly.polymul(a, d) print a, b
def d2d(b, a, T): nb = len(b) na = len(a) b_new = _polytustin(b, T) a_new = _polytustin(a, T) if nb > na: a_new = polymul(a_new, polypow([1, (T - 1) / (T + 1)], nb - na)) elif na > nb: b_new = polymul(b_new, polypow([1, (T - 1) / (T + 1)], na - nb)) return b_new / a_new[0], a_new / a_new[0]
def calculate_rst(b_minus, b_plus, a_minus, a_plus, a_m, a0=np.ones(1), d=1, p=0, r_e=0): """Calculate the coefficient of the rst""" perturbation = P.polypow(zero(1), p) s2, r0 = solve_diophantine(P.polymul(perturbation, a_minus), P.polymul(delay(d), b_minus), P.polymul(a_m, a0)) b_m_plus, _ = solve_diophantine(P.polymul(delay(d), b_minus), P.polypow(zero(1), r_e + 1), a_m) t0 = P.polymul(a0, b_m_plus) r = P.polymul(r0, a_plus) s = P.polymul(s2, P.polymul(b_plus, perturbation)) t = P.polymul(t0, a_plus) print("R = ", ", ".join(map(str, r))) print("S = ", ", ".join(map(str, s))) print("T = ", ", ".join(map(str, t))) return r, s, t
def PolyGCD(a: numpy.array, b: numpy.array): """Iterative Greatest Common Divisor for polynomial""" # if len(a) < len(b): # a, b = b, a x, xt, y, yt = (1, ), (0, ), (0, ), (1, ) while any(num != 0.0 for num in b): q = polydiv(a, b)[0] a, b = b, polydiv(a, b)[1] x, xt = xt, polysub(x, polymul(xt, q)) y, yt = yt, polysub(y, polymul(yt, q)) return a, x, y
def ButterworthC(N, w, Ts): Nr = int(N / 2) i = 1j a = [w**N] b = [1] # print poly.polymul(a,b) for k in range(1, Nr + 1): rad = np.pi * (2 * k - 1) / (2 * N) n = [1, 2 * w * np.sin(rad), w**2] b = poly.polymul(b, n) if N % 2 == 1: b = poly.polymul(b, [1, w]) print a, b
def root_finding_poly(self): """ R = p^2 - (1 - x^2) * q^2 Returns ------- coef : np.ndarray Coefficients of a root-finding polynomial `R(x)`. Every zero of the `PseudoPolynomial` is also a zero of `R(x)`. """ return remove_zeros(pol.polysub(pol.polymul(self.p, self.p), pol.polymul(pol.polymul(self.q, self.q), (1, 0, -1))))
def plot(points): s, X, F = points[:], [], [] while (s != ''): i = s.index('(') j = s.index(',', i) X.append(float(s[i + 1:j])) k = s.index(')', j) F.append(float(s[j + 1:k])) s = s[k + 2:] fig = plt.figure() plt.clf() sub = fig.add_subplot(111) X1 = np.arange(min(X) - 2, max(X) + 2, 0.1) num_plots = len(X) colormap = plt.cm.gist_ncar plt.gca().set_color_cycle( [colormap(i) for i in np.linspace(0.2, 0.9, num_plots)]) x = [1.0] for i in range(len(X)): x = P.polymul(x, [-1 * X[i], 1]) b = [0.0] for i in range(len(X)): a = P.polydiv(x, [-1 * X[i], 1]) b = P.polyadd( P.polymul((P.polydiv(a[0], P.polyval(X[i], a[0])))[0], [F[i]]), b) Y = P.polyval( X1, P.polymul((P.polydiv(a[0], P.polyval(X[i], a[0])))[0], [F[i]])) sub.plot(X1, Y) Y = P.polyval(X1, b) Y1 = P.polyval(np.arange(min(X), max(X) + 0.1, 0.1), b) interpol_obj = sub.plot(X1, Y, 'k', linewidth=2) sub.plot(X, F, 'ro', markersize=8) plt.grid(True) fig.legend(interpol_obj, ['Interpolating Polynomial'], fancybox=True, shadow=True, loc='upper left') plt.axis([min(X) - 3, max(X) + 3, min(Y1) - 2, max(Y1) + 2]) plt.xlabel('x axis') plt.ylabel('y axis') plt.title('Interpolate') canvas = FigureCanvas(fig) output = StringIO.StringIO() canvas.print_png(output) response = make_response(output.getvalue()) response.mimetype = 'image/png' return response
def get_poly(n): if n > len(Bessel.polynomials): if n == 1: Bessel.polynomials.append(Polynomial(coef=[1, 1])) elif n == 2: Bessel.polynomials.append(Polynomial(coef=[3, 3, 1])) else: b_n_2 = poly.polymul(Polynomial(coef=[0, 0, 1]), Bessel.get_poly(n - 2)) b_n_1 = poly.polymul(Polynomial(coef=[2 * n - 1]), Bessel.get_poly(n - 1)) b_n = poly.polyadd(b_n_1, b_n_2) Bessel.polynomials.append(b_n[0]) return Bessel.polynomials[n - 1]
def test_pseudopoly_multiplication(A, r, rseed=42): # float * polynomial poly = random_polynomial(2, 3, r=r, rseed=rseed) poly2 = PseudoPolynomial(A * poly.p, A * poly.q, r=r) assert A * poly == poly2 assert poly * A == poly2 # polynomial * pseudopoly A = [1, 3, 2, 4] result = PseudoPolynomial(p=pol.polymul(A, poly.p), q=pol.polymul(A, poly.q), r=poly.r) assert A * poly == result assert poly * A == result
def fast_power_poly(base, power, r, Z_n): result = 1 while power > 0: # If power is even if power % 2 == 0: # Divide the power by 2 power = power / 2 # Multiply base to itself base = P.polymul(base, base) #base = P.polydiv(square, modulus)[1] # base = base mod (x^r-1) x = np.nonzero(result)[0] for i in x[x>=r]: if base[i] != 0: base[i % r] += base[i] base[i] = 0 # Keep the coefficients in Z_n base = base % Z_n else: # Decrement the power by 1 and make it even power = power - 1 # Take care of the extra value that we took out # We will store it directly in result result = P.polymul(result, base) #result = P.polydiv(mult, modulus)[1] #print(np.nonzero(result)) x = np.nonzero(result)[0] for i in x[x>=r]: #print(i) if result[i] != 0: result[i % r] += result[i] result[i] = 0 # Keep the coefficients in Z_n result = result % Z_n # Now power is even, so we can follow our previous procedure power = power / 2 base = P.polymul(base, base) #base = P.polydiv(square, modulus)[1] x = np.nonzero(result)[0] for i in x[x>=r]: if base[i] != 0: base[i % r] += base[i] base[i] = 0 # Keep the coefficients in Z_n base = base % Z_n return result
def negPNX(n): if n == 1: return (1) if n < 1: return if n in negPNXDict: return negPNXDict[n] first = P.polymul((3, 2 * n - 4), negPNX(n - 1)) second = P.polymul((0, 4), (1, -1)) deriv = P.polyder(negPNX(n - 1)) second = P.polymul(second, deriv) third = posPNX(n - 1) ret = P.polyadd(first, second) ret = P.polyadd(ret, third) negPNXDict[n] = ret return ret
def polynomials_mult(x, y, mod, poly_mod): return np.int64( np.round( poly.polydiv( poly.polymul(x, y) % mod, poly_mod )[1] % mod))
def evaluate_keygen_v1(sk, size, modulus, T, poly_mod, std2): """Generate a relinearization key using version 1. Args: sk: secret key. size: size of the polynomials. modulus: coefficient modulus. T: base. poly_mod: polynomial modulus. std2: standard deviation for the error distribution. Returns: rlk0, rlk1: relinearization key. """ n = len(poly_mod) - 1 l = np.int(np.log(modulus) / np.log(T)) rlk0 = np.zeros((l + 1, n), dtype=np.int64) rlk1 = np.zeros((l + 1, n), dtype=np.int64) for i in range(l + 1): a = gen_uniform_poly(size, modulus) e = gen_normal_poly(size, 0, std2) secret_part = T**i * poly.polymul(sk, sk) b = np.int64( polyadd(polymul_wm(-a, sk, poly_mod), polyadd_wm(-e, secret_part, poly_mod), modulus, poly_mod)) b = np.int64(np.concatenate((b, [0] * (n - len(b))))) # pad b a = np.int64(np.concatenate((a, [0] * (n - len(a))))) # pad a rlk0[i] = b rlk1[i] = a return rlk0, rlk1
def posPNX(n): if n == 1: return (1) if n < 1: return if n in posPNXDict: return posPNXDict[n] first = P.polymul((1, 2 * n - 2), posPNX(n - 1)) second = P.polymul((0, 4), (1, -1)) deriv = P.polyder(posPNX(n - 1)) second = P.polymul(second, deriv) third = P.polymul((0, 1), (negPNX(n - 1))) ret = P.polyadd(first, second) ret = P.polyadd(ret, third) posPNXDict[n] = ret return ret
def Lagrange(L,M): polylist=[] n=len(L) w=(-1*L[0],1) for i in range(1,n): w=P.polymul(w,(-1*L[i],1)) result=array([0.0 for i in range(len(w)-1)]) derivative=P.polyder(w) for i in range(n): polylist.append((P.polydiv(w,(-1*L[i],1))[0]*M[i])/P.polyval(L[i],derivative)) result+=polylist[-1] polynomial="" for i in range(len(result)-1,0,-1): if(result[i]!=0): if(result[i]>0 and i!=(len(result)-1)): polynomial+=" + "+str(result[i])+"x^"+str(i)+" " elif(result[i]>0 and i==(len(result)-1)): polynomial+=str(result[i])+"x^"+str(i)+" " else: polynomial+=" - "+str(-1*result[i])+"x^"+str(i)+" " if(result[0]!=0): polynomial+=" + "+str(result[0]) if result[0]>0 else " - "+str(-1*result[0]) plot(L,M,polylist,result) return (polynomial)
def poly_mul_mod(op1, op2, coeff_mod, poly_mod): """Multiply two polynomials and modulo every coefficient with coeff_mod. Args: op1 (list): First Polynomail (Multiplicand). op2 (list): Second Polynomail (Multiplier). Returns: A list with polynomial coefficients. """ # For non same size polynomials we have to shift the polynomials because numpy consider right # side as lower order of polynomial and we consider right side as heigher order. if len(op1) != poly_mod: op1 += [0] * (poly_mod - len(op1)) if len(op2) != poly_mod: op2 += [0] * (poly_mod - len(op2)) poly_len = poly_mod poly_mod = np.array([1] + [0] * (poly_len - 1) + [1]) result = ( poly.polydiv( poly.polymul(np.array(op1, dtype="object"), np.array(op2, dtype="object")) % coeff_mod, poly_mod, )[1] % coeff_mod ).tolist() if len(result) != poly_len: result += [0] * (poly_len - len(result)) return [round(x) for x in result]
def plot(points): s,X,F=points[:],[],[] while(s!=''): i=s.index('(') j=s.index(',',i) X.append(float(s[i+1:j])) k=s.index(')',j) F.append(float(s[j+1:k])) s=s[k+2:] fig=plt.figure() plt.clf() sub=fig.add_subplot(111) X1=np.arange(min(X)-2,max(X)+2,0.1) num_plots=len(X) colormap = plt.cm.gist_ncar plt.gca().set_color_cycle([colormap(i) for i in np.linspace(0.2, 0.9, num_plots)]) x=[1.0] for i in range(len(X)): x=P.polymul(x,[-1*X[i],1]) b=[0.0] for i in range(len(X)): a=P.polydiv(x,[-1*X[i],1]) b=P.polyadd(P.polymul((P.polydiv(a[0],P.polyval(X[i],a[0])))[0],[F[i]]),b) Y=P.polyval(X1,P.polymul((P.polydiv(a[0],P.polyval(X[i],a[0])))[0],[F[i]])) sub.plot(X1,Y) Y=P.polyval(X1,b) Y1=P.polyval(np.arange(min(X)-0.1,max(X)+0.1,0.1),b) interpol_obj=sub.plot(X1,Y,'k',linewidth=2) sub.plot(X,F,'ro',markersize=8) plt.grid(True) fig.legend(interpol_obj,['Interpolating Polynomial'],fancybox=True,shadow=True,loc='upper left') plt.axis([min(X)-3,max(X)+3,min(Y1)-2,max(Y1)+2]) plt.xlabel('x axis') plt.ylabel('y axis') plt.title('Interpolate') #plt.show() canvas = FigureCanvas(fig) output = StringIO.StringIO() canvas.print_png(output) response = make_response(output.getvalue()) response.mimetype = 'image/png' return response
def extended_euclid_poly(a, b, p): """ Повертає d=НСД(x,y) і x, y такі, що ax + by = d """ if np.all(b == 0): print ("b=0", a, b) return a, np.array([1]), np.array([0]) d, x, y = extended_euclid_poly(b, P.polydiv(a, b)[1] % p, p) print (d, x, y) return d, y, (x - P.polymul(P.polydiv(a,b)[0], y)) % p
def test_polymul(self): for i in range(5): for j in range(5): msg = "At i=%d, j=%d" % (i, j) tgt = np.zeros(i + j + 1) tgt[i + j] += 1 res = poly.polymul([0] * i + [1], [0] * j + [1]) assert_equal(trim(res), trim(tgt), err_msg=msg)
def n_k(order, coef_func): if order < 0: raise ValueError() if order == 0: return Polynomial([0, 1]) elif order > 0: return pl.polymul(n_k(order - 1, coef_func), Polynomial([coef_func(order), 1]))[0] / (order + 1)
def mult(a, b, type=1): kex_start = timeit.default_timer() if type == 1: c = p.polymul(a, b) else: c = np.fft.irfft(np.fft.rfft(a, 2 * n) * np.fft.rfft(b, 2 * n), 2 * n) kex_end = timeit.default_timer() return c, kex_end - kex_start
def polymul(a, b): """ Multiply polynomial a by polynomial b. a and b are lists from highest order term to lowest. """ val = polynomial.polymul(a[::-1], b[::-1]) val = val[::-1] return val
def test_polymul(self) : for i in range(5) : for j in range(5) : msg = "At i=%d, j=%d" % (i,j) tgt = np.zeros(i + j + 1) tgt[i + j] += 1 res = poly.polymul([0]*i + [1], [0]*j + [1]) assert_equal(trim(res), trim(tgt), err_msg=msg)
def generalized_hankel_matrices(self, phis, pols): G = np.zeros((len(phis), len(phis)), dtype=complex) G1 = np.zeros((len(phis), len(phis)), dtype=complex) prow = [monicPolynomial(npol.polymul(pols[1].coef, pols[j].coef), coef_type='normal').f_polynomial() for j in range(len(phis))] for i,j in itertools.product(range(len(phis)), range(len(phis))): G [i,j] = self.inner_prod(phis[i], phis[j]) G1[i,j] = self.inner_prod(phis[i], prow[j]) return G, G1
def interpolate(pointList): size = len(pointList) if len(pointList) == 1: return (fr(pointList[0][1]),) result = [fr(0)] for index_i in range(0, size): x_i = fr(pointList[index_i][0]) y_i = fr(pointList[index_i][1]) member = [y_i] for index_j in range(0, size): if index_i == index_j: continue x_j = fr(pointList[index_j][0]) member = polymul(member, [-x_j, fr(1)]) multiplier = [fr(1, x_i - x_j)] member = polymul(member, multiplier) result = polyadd(result, member) return result
def polymul_wm(x, y, poly_mod): """Multiply two polynomials Args: x, y: two polynomials to be multiplied. poly_mod: polynomial modulus. Returns: A polynomial in Z[X]/(poly_mod). """ return poly.polydiv(poly.polymul(x, y), poly_mod)[1]
def mul(a, b, prime, exp, min0): a.reverse() b.reverse() min0.reverse() ans = [] mul0 = poly.polymul(a, b) ans = poly.polydiv(mul0, min0)[1] ans = list(map(int, ans)) ans.reverse() return ans
def polycomp(c1, c2): """ Compose two polynomials : c1 o c2 = c1(c2(x)) The arguments are sequences of coefficients, from lowest order term to highest, e.g., [1,2,3] represents the polynomial 1 + 2*x + 3*x**2. """ # TODO: Polynomial(Polynomial()) seems to do just that? # using Horner's method to compute the result of a polynomial cr = [c1[-1]] for a in reversed(c1[:-1]): # cr = cr * c2 + a cr = polynomial.polyadd(polynomial.polymul(cr, c2), [a]) return cr
def evaluate(self, nodes, interval=None): """Computes weights for stored polynomial and given nodes. The weights are calculated with help of the Lagrange polynomials .. math:: \\alpha_i = \\int_a^b\\omega (x) \\prod_{j=1,j \\neq i}^{n} \\frac{x-x_j}{x_i-x_j} \\mathrm{d}x See Also -------- :py:meth:`.IWeightFunction.evaluate` : overridden method """ super(PolynomialWeightFunction, self).evaluate(nodes, interval) a = self._interval[0] b = self._interval[1] n_nodes = nodes.size alpha = np.zeros(n_nodes) for j in range(n_nodes): selection = list(range(j)) selection.extend(list(range(j + 1, n_nodes))) poly = [1.0] for ais in nodes[selection]: # builds Lagrange polynomial p_i poly = pol.polymul(poly, [ais / (ais - nodes[j]), 1 / (nodes[j] - ais)]) # computes \int w(x)p_i dx poly = pol.polyint(pol.polymul(poly, self._coefficients)) alpha[j] = pol.polyval(b, poly) - pol.polyval(a, poly) #LOG.debug("Computed polynomial weights for nodes {:s} in {:s}." # .format(nodes, self._interval)) del self._interval self._weights = alpha
def Lagrange(self,A,B): from numpy import array from numpy.polynomial import polynomial as P n=len(A) w=(-1*A[0],1) for i in range(1,n): w=P.polymul(w,(-1*A[i],1)) result=array([0.0 for i in range(len(w)-1)]) derivative=P.polyder(w) for i in range(n): result+=(P.polydiv(w,(-1*A[i],1))[0]*B[i])/P.polyval(A[i],derivative) s=self.plot(list(result),A,B) return s
def test_polydiv(self) : # check zero division assert_raises(ZeroDivisionError, poly.polydiv, [1], [0]) # check scalar division quo, rem = poly.polydiv([2],[2]) assert_equal((quo, rem), (1, 0)) quo, rem = poly.polydiv([2,2],[2]) assert_equal((quo, rem), ((1,1), 0)) # check rest. for i in range(5) : for j in range(5) : msg = "At i=%d, j=%d" % (i,j) ci = [0]*i + [1,2] cj = [0]*j + [1,2] tgt = poly.polyadd(ci, cj) quo, rem = poly.polydiv(tgt, ci) res = poly.polyadd(poly.polymul(quo, ci), rem) assert_equal(res, tgt, err_msg=msg)
def Newton(self,A,B): from numpy import array from numpy.polynomial import polynomial as P n=len(A) mat=[[0.0 for i in range(n)] for j in range(n)] for i in range(n): mat[i][0]=B[i] for i in range(1,n): for j in range(n-i): mat[j][i]=(mat[j+1][i-1]-mat[j][i-1])/(A[j+i]-A[j]) res=array((mat[0][0],)) for i in range(1,n): prod=(-1*A[0],1) for j in range(1,i): prod=P.polymul(prod,(-1*A[j],1)) res=P.polyadd(res,array(prod)*mat[0][i]) s=self.plot(list(res),A,B) return s
def Lagrange(self,U,V): n=len(U) w=(-1*U[0],1) for i in range(1,n): w=P.polymul(w,(-1*U[i],1)) result=array([0.0 for i in range(len(w)-1)]) derivative=P.polyder(w) for i in range(n): result+=(P.polydiv(w,(-1*U[i],1))[0]*V[i])/P.polyval(U[i],derivative) temp=list(result); cofficient=temp l=len(cofficient); temp=[]; for i in range(l-1): temp.append(str(cofficient[l-(i+1)])+'x^'+str(l-(i+1))+str('+')) temp.append(str(cofficient[0])+'x^'+str(0)); str1=''.join(temp) return(str1)
def p389(dice): t=time.clock() probs={n:1/dice[0] for n in range (1,dice[0]+1)} ks=[n for n in range(1,dice[0]+1)] for n in dice[1:]: newWays={} p0=np.array([0.]+[1. for i in range(n)])/n pks=np.copy(p0) for k in ks: if k>1: pks=P.polymul(p0,pks) for s in range(k,len(pks)): newWays[s]=newWays.get(s,0)+probs[k]*pks[s] probs.update(newWays) ks=sorted([k for k,v in probs.items()]) EX=sum([k*prob for k,prob in probs.items()]) EX2=sum([k**2*prob for k,prob in probs.items()]) var=EX2-EX**2 print(EX,var) print(time.clock()-t)
def __mul__(self, other): if isinstance(other, Polynomial): result = polynomial.polymul(self._poly, other._poly) else: result = [0] * other + self._poly return Polynomial(poly=result)
def longitudinal(velocity, density, S_gross_w, mac, Cm_q, Cz_alpha, mass, Cm_alpha, Iy, Cm_alpha_dot, Cz_u, Cz_alpha_dot, Cz_q, Cw, Theta, Cx_u, Cx_alpha): """ output = SUAVE.Methods.Flight_Dynamics.Dynamic_Stablity.Full_Linearized_Equations.longitudinal(velocity, density, S_gross_w, mac, Cm_q, Cz_alpha, mass, Cm_alpha, Iy, Cm_alpha_dot, Cz_u, Cz_alpha_dot, Cz_q, Cw, Theta, Cx_u, Cx_alpha) Calculate the natural frequency and damping ratio for the full linearized short period and phugoid modes Inputs: velocity - flight velocity at the condition being considered [meters/seconds] density - flight density at condition being considered [kg/meters**3] S_gross_w - area of the wing [meters**2] mac - mean aerodynamic chord of the wing [meters] Cm_q - coefficient for the change in pitching moment due to pitch rate [dimensionless] (2 * K * dC_m/di * lt/c where K is approximately 1.1) Cz_alpha - coefficient for the change in Z force due to the angle of attack [dimensionless] (-C_D - dC_L/dalpha) mass - mass of the aircraft [kilograms] Cm_alpha - coefficient for the change in pitching moment due to angle of attack [dimensionless] (dC_m/dC_L * dCL/dalpha) Iy - moment of interia about the body y axis [kg * meters**2] Cm_alpha_dot - coefficient for the change in pitching moment due to rate of change of angle of attack [dimensionless] (2 * dC_m/di * depsilon/dalpha * lt/mac) Cz_u - coefficient for the change in force in the Z direction due to change in forward velocity [dimensionless] (usually -2 C_L or -2C_L - U dC_L/du) Cz_alpha_dot - coefficient for the change of angle of attack caused by w_dot on the Z force [dimensionless] (2 * dC_m/di * depsilon/dalpha) Cz_q - coefficient for the change in Z force due to pitching velocity [dimensionless] (2 * K * dC_m/di where K is approximately 1.1) Cw - coefficient to account for gravity [dimensionless] (-C_L) Theta - angle between the horizontal axis and the body axis measured in the vertical plane [radians] Cx_u - coefficient for the change in force in the X direction due to change in the forward velocity [dimensionless] (-2C_D) Cx_alpha - coefficient for the change in force in the X direction due to the change in angle of attack caused by w [dimensionless] (C_L-dC_L/dalpha) Outputs: output - a data dictionary with fields: short_w_n - natural frequency of the short period mode [radian/second] short_zeta - damping ratio of the short period mode [dimensionless] phugoid_w_n - natural frequency of the short period mode [radian/second] phugoid_zeta - damping ratio of the short period mode [dimensionless] Assumptions: X-Z axis is plane of symmetry Constant mass of aircraft Origin of axis system at c.g. of aircraft Aircraft is a rigid body Earth is inertial reference frame Perturbations from equilibrium are small Flow is Quasisteady Zero initial conditions Cm_a = CF_z_a = CF_x_a = 0 Neglect Cx_alpha_dot, Cx_q and Cm_u Source: J.H. Blakelock, "Automatic Control of Aircraft and Missiles" Wiley & Sons, Inc. New York, 1991, p 26-41. """ #process # constructing matrix of coefficients A = (- Cx_u, mass * velocity / S_gross_w / (0.5*density*velocity**2.)) # X force U term B = (-Cx_alpha) # X force alpha term C = (-Cw * np.cos(Theta)) # X force theta term D = (-Cz_u) # Z force U term E = (-Cz_alpha, (mass*velocity/S_gross_w/(0.5*density*velocity**2.)-mac*0.5/velocity*Cz_alpha_dot)) # Z force alpha term F = (- Cw * np.sin(Theta), (-mass*velocity/S_gross_w/(0.5*density*velocity**2.)-mac*0.5/velocity*Cz_q))# Z force theta term G = (0.) # M moment U term H = (-Cm_alpha, -mac*0.5/velocity*Cm_alpha_dot) # M moment alpha term I = (0., - mac*0.5/velocity*Cm_q, Iy/S_gross_w/(0.5*density*velocity**2)/mac) # M moment theta term # Taking the determinant of the matrix ([A, B, C],[D, E, F],[G, H, I]) EI = P.polymul(E,I) FH = P.polymul(F,H) part1 = P.polymul(A,P.polysub(EI,FH)) DI = P.polymul(D,I) FG = P.polymul(F,G) part2 = P.polymul(B,P.polysub(FG,DI)) DH = P.polymul(D,H) GE = P.polymul(G,E) part3 = P.polymul(C,P.polysub(DH,GE)) total = P.polyadd(part1,P.polyadd(part2,part3)) # Use Synthetic division to split polynomial into two quadratic factors poly = total / total[4] poly1 = poly * 1. poly2 = poly * 1. poly3 = poly * 1. poly4 = poly * 1. poly1[4] = poly[4] - poly[2]/poly[2] poly1[3] = poly[3] - poly[1]/poly[2] poly1[2] = poly[2] - poly[0]/poly[2] poly2[4] = 0 poly2[3] = poly1[3] - poly[2]*poly1[3]/poly[2] poly2[2] = poly1[2] - poly[1]*poly1[3]/poly[2] poly2[1] = poly1[1] - poly[0]*poly1[3]/poly[2] poly3[4] = poly[4] - poly2[2]/poly2[2] poly3[3] = poly[3] - poly2[1]/poly2[2] poly3[2] = poly[2] - poly2[0]/poly2[2] poly4[3] = poly3[3] - poly2[2]*poly3[3]/poly2[2] poly4[2] = poly3[2] - poly2[1]*poly3[3]/poly2[2] poly4[1] = poly3[1] - poly2[0]*poly3[3]/poly2[2] # Generate natural frequency and damping for Short Period and Phugoid modes short_w_n = (poly4[2])**0.5 short_zeta = poly3[3]*0.5/short_w_n phugoid_w_n = (poly2[0]/poly2[2])**0.5 phugoid_zeta = poly2[1]/poly2[2]*0.5/phugoid_w_n output = Data() output.short_natural_frequency = short_w_n output.short_damping_ratio = short_zeta output.phugoid_natural_frequency = phugoid_w_n output.phugoid_damping_ratio = phugoid_zeta return output
def lateral_directional(velocity, Cn_Beta, S_gross_w, density, span, I_z, Cn_r, I_x, Cl_p, J_xz, Cl_r, Cl_Beta, Cn_p, Cy_phi, Cy_psi, Cy_Beta, mass): """ output = SUAVE.Methods.Flight_Dynamics.Dynamic_Stablity.Full_Linearized_Equations.lateral_directional(velocity, Cn_Beta, S_gross_w, density, span, I_z, Cn_r, I_x, Cl_p, J_xz, Cl_r, Cl_Beta, Cn_p, Cy_phi, Cy_psi, Cy_Beta) Calculate the natural frequency and damping ratio for the full linearized dutch roll mode along with the time constants for the roll and spiral modes Inputs: velocity - flight velocity at the condition being considered [meters/seconds] Cn_Beta - coefficient for change in yawing moment due to sideslip [dimensionless] (no simple relation) S_gross_w - area of the wing [meters**2] density - flight density at condition being considered [kg/meters**3] span - wing span of the aircraft [meters] I_z - moment of interia about the body z axis [kg * meters**2] Cn_r - coefficient for change in yawing moment due to yawing velocity [dimensionless] ( - C_D(wing)/4 - 2 * Sv/S * (l_v/b)**2 * (dC_L/dalpha)(vert) * eta(vert)) I_x - moment of interia about the body x axis [kg * meters**2] Cl_p - change in rolling moment due to the rolling velocity [dimensionless] (no simple relation for calculation) J_xz - products of inertia in the x-z direction [kg * meters**2] (if X and Z lie in a plane of symmetry then equal to zero) Cl_r - coefficient for change in rolling moment due to yawing velocity [dimensionless] (Usually equals C_L(wing)/4) Cl_Beta - coefficient for change in rolling moment due to sideslip [dimensionless] Cn_p - coefficient for the change in yawing moment due to rolling velocity [dimensionless] (-C_L(wing)/8*(1 - depsilon/dalpha)) (depsilon/dalpha = 2/pi/e/AspectRatio dC_L(wing)/dalpha) Cy_phi - coefficient for change in sideforce due to aircraft roll [dimensionless] (Usually equals C_L) Cy_psi - coefficient to account for gravity [dimensionless] (C_L * tan(Theta)) Cy_Beta - coefficient for change in Y force due to sideslip [dimensionless] (no simple relation) mass - mass of the aircraft [kilograms] Outputs: output - a data dictionary with fields: dutch_w_n - natural frequency of the dutch roll mode [radian/second] dutch_zeta - damping ratio of the dutch roll mode [dimensionless] roll_tau - approximation of the time constant of the roll mode of an aircraft [seconds] (positive values are bad) spiral_tau - time constant for the spiral mode [seconds] (positive values are bad) Assumptions: X-Z axis is plane of symmetry Constant mass of aircraft Origin of axis system at c.g. of aircraft Aircraft is a rigid body Earth is inertial reference frame Perturbations from equilibrium are small Flow is Quasisteady Zero initial conditions Neglect Cy_p and Cy_r Source: J.H. Blakelock, "Automatic Control of Aircraft and Missiles" Wiley & Sons, Inc. New York, 1991, p 118-124. """ #process # constructing matrix of coefficients A = (0, -span * 0.5 / velocity * Cl_p, I_x/S_gross_w/(0.5*density*velocity**2)/span ) # L moment phi term B = (0, -span * 0.5 / velocity * Cl_r, -J_xz / S_gross_w / (0.5 * density * velocity ** 2.) / span) # L moment psi term C = (-Cl_Beta) # L moment Beta term D = (0, - span * 0.5 / velocity * Cn_p, -J_xz / S_gross_w / (0.5 * density * velocity ** 2.) / span ) # N moment phi term E = (0, - span * 0.5 / velocity * Cn_r, I_z / S_gross_w / (0.5 * density * velocity ** 2.) / span ) # N moment psi term F = (-Cn_Beta) # N moment Beta term G = (-Cy_phi) # Y force phi term H = (-Cy_psi, mass * velocity / S_gross_w / (0.5 * density * velocity ** 2.)) I = (-Cy_Beta, mass * velocity / S_gross_w / (0.5 * density * velocity ** 2.)) # Taking the determinant of the matrix ([A, B, C],[D, E, F],[G, H, I]) EI = P.polymul(E,I) FH = P.polymul(F,H) part1 = P.polymul(A,P.polysub(EI,FH)) DI = P.polymul(D,I) FG = P.polymul(F,G) part2 = P.polymul(B,P.polysub(FG,DI)) DH = P.polymul(D,H) GE = P.polymul(G,E) part3 = P.polymul(C,P.polysub(DH,GE)) total = P.polyadd(part1,P.polyadd(part2,part3)) poly = total / total[5] # Generate the time constant for the spiral and roll modes along with the damping and natural frequency for the dutch roll mode root = np.roots(poly) root = sorted(root,reverse=True) spiral_tau = 1 * root[0].real w_n = (root[1].imag**2 + root[1].real**2)**(-0.5) zeta = -2*root[1].real/w_n roll_tau = 1 * root [3].real output = Data() output.dutch_natural_frequency = w_n output.dutch_damping_ratio = zeta output.spiral_tau = spiral_tau output.roll_tau = roll_tau return output
p2 = obj.insertPol(gr1,p2) print "La suma es:"+str(npy.polyadd(p1,p2)) elif op == 3: print "Resta" gr1 = input("Grado del polinomio 1") p1 = obj.insertPol(gr1,p1) gr1 = input("Grado del polinomio 2") p2 = obj.insertPol(gr1,p2) print "La resta es:"+str(npy.polysub(p1,p2)) elif op == 4: print "Multiplicacion" gr1 = input("Grado del polinomio 1") p1 = obj.insertPol(gr1,p1) gr1 = input("Grado del polinomio 2") p2 = obj.insertPol(gr1,p2) print "La multiplicacion es:"+str(npy.polymul(p1,p2)) elif op == 5: print "Igualdad" gr1 = input("Grado del polinomio 1") p1 = obj.insertPol(gr1,p1) gr1 = input("Grado del polinomio 2") p2 = obj.insertPol(gr1,p2) elif op == 6: print "Polinomio Opuesto" gr1 = input("Ingresa el grado del polinomio") p1 = obj.insertPol(gr1,p1) for i in range (0,len(p1)): p1[i]=-p1[i] print p1 else: print "No es una opcion valida"
def polymul(c1, c2): from numpy.polynomial.polynomial import polymul return polymul(c1, c2)
print "a",a print "b",b break # TESTING SUBTRACTION FUNCTION a=P.polysub(c1,c2).tolist() b=q.subPoly(c1,c2) if(a!=b): print "Failed on Case:" print "a subtract b" print "a",a print "b",b break # TESTING MULTIPLICATION FUNCTION a=P.polymul(c1,c2).tolist() b=q.multPoly(c1,c2) if(a!=b): print "Failed on Case:" print "a * b" print "a",a print "b",b break # TESINGING DIVISION FUNCTION if q.trim(c2)==[0]: continue try: [a1,a2]=P.polydiv(c1,c2) a1=q.trim(a1.tolist()) a2=q.trim(a2.tolist())