MATLAB仿真天線陣代碼知識(shí)講解

1、Good is good, but better carries it.精益求精，善益求善。MATLAB仿真天線陣代碼-天線陣代碼/downloads164/sourcecode/math/detail750575.html一、clcclearallf=3e9;N1=4;N2=8;N3=12;a=pi/2;%饋電相位差i=1;%天線電流值lambda=(3e8)/f;%lambda=c/f波長(zhǎng)d=lambda/2;beta=2.*pi/lambda;W=-2*pi:0.001:2*pi;y1=sin(N1.*W./2)./(N1.*(sin(W./2);%歸一化陣因子y1=abs(y1);r1

2、=max(y1);y2=sin(N2.*W./2)./(N2.*(sin(W./2);%歸一化陣因子y2=abs(y2);r2=max(y2);y3=sin(N3.*W./2)./(N3.*(sin(W./2);%歸一化陣因子y3=abs(y3);r3=max(y3);%歸一化陣因子繪圖程序,figure(1)subplot(311);plot(W,y1);gridon;%繪出N=4等幅等矩陣列的歸一化陣因子xlabel(f=3GHz,N=4,d=1/2波長(zhǎng),a=/2)subplot(312);plot(W,y2);gridon;%繪出N=8等幅等矩陣列的歸一化陣因子xlabel(f=3GHz

3、,N=8,d=1/2波長(zhǎng),a=/2)subplot(313);plot(W,y3);gridon;%繪出N=12等幅等矩陣列的歸一化陣因子xlabel(f=3GHz,N=12,d=1/2波長(zhǎng),a=/2)%-%只有參數(shù)N改變的天線方向圖t=0:0.01:2*pi;W=a+(beta.*d.*cos(t);z1=(N1/2).*(W);z2=(1/2).*(W);W1=sin(z1)./(N1.*sin(z2);%非歸一化的陣因子K1K1=abs(W1);%-W=a+(beta.*d.*cos(t);z3=(N2/2).*(W);z4=(1/2).*(W);W2=sin(z3)./(N2.*sin

4、(z4);%非歸一化的陣因子K2K2=abs(W2);%-W=a+(beta.*d.*cos(t);z5=(N3/2).*(W);z6=(1/2).*(W);W3=sin(z5)./(N3.*sin(z6);%非歸一化的陣因子K3K3=abs(W3);%-繪圖函數(shù)figure(2)subplot(131);polar(t,K1);xlabel(f=3GHz,N=4,d=1/2波長(zhǎng),a=/2);subplot(132);polar(t,K2);xlabel(f=3GHz,N=8,d=1/2波長(zhǎng),a=/2);subplot(133);polar(t,K3);xlabel(f=3GHz,N=12,d

5、=1/2波長(zhǎng),a=/2);%-%只有陣列單元方向角a改變的天線方向圖N4=10;d1=lambda/4;a1=0;a2=pi/2;a3=pi/2+pi/10;A=a1+(beta.*d1.*cos(t);x1=(N4/2).*(A);x2=(1/2).*(A);A1=sin(x1)./(N4.*sin(x2);%非歸一化的陣因子K4K4=abs(A1);%-B=a2+(beta.*d1.*cos(t);y_1=(N4/2).*(B);y_2=(1/2).*(B);B1=sin(y_1)./(N4.*sin(y_2);%非歸一化的陣因子K5K5=abs(B1);%-C=a3+(beta.*d1.

6、*cos(t);v1=(N4/2).*(C);v2=(1/2).*(C);C1=sin(v1)./(N4.*sin(v2);%非歸一化的陣因子K6K6=abs(C1);%-繪圖函數(shù)figure(3)subplot(131);polar(t,K4);xlabel(f=3GHz,N=10,d=1/4波長(zhǎng),a=0);subplot(132);polar(t,K5);xlabel(f=3GHz,N=10,d=1/4波長(zhǎng),a=/2);subplot(133);polar(t,K6);xlabel(f=3GHz,N=10,d=1/4波長(zhǎng),a=/2+/10);%-%只有陣列單元間隔d改變的天線方向圖N5=2

7、0;d2=lambda/4;d3=lambda/2;d4=0.7*lambda;a4=pi/2;D=a4+(beta.*d2.*cos(t);p1=(N5/2).*(D);p2=(1/2).*(D);D1=sin(p1)./(N5.*sin(p2);%非歸一化的陣因子K7K7=abs(D1);%-E=a4+(beta.*d3.*cos(t);q1=(N5/2).*(E);q2=(1/2).*(E);E1=sin(q1)./(N5.*sin(q2);%非歸一化的陣因子K8K8=abs(E1);%-F=a4+(beta.*d4.*cos(t);r_1=(N5/2).*(F);r_2=(1/2).*

8、(F);F1=sin(r_1)./(N5.*sin(r_2);%非歸一化的陣因子K9K9=abs(F1);%-繪圖函數(shù)figure(4)subplot(131);polar(t,K7);xlabel(f=3GHz,N=20,d=1/4波長(zhǎng),a=/2);subplot(132);polar(t,K8);xlabel(f=3GHz,N=20,d=1/2波長(zhǎng),a=/2);subplot(133);polar(t,K9);xlabel(f=3GHz,N=20,d=0.7波長(zhǎng),a=/2);%-%-3D-天線方向圖n_tehta=130;%-采樣視角點(diǎn)的仰角n_phi=130;%-采樣點(diǎn)的方向角tehta

9、,phi=meshgrid(eps:pi./(n_tehta-1):pi,.%meshgrid函數(shù)為矩形區(qū)域的設(shè)定范圍是epftehta0phi20:2*pi./(n_phi-1):2*pi);t3=tehta;%-只有參數(shù)N改變的天線方向3D圖M=a+(beta.*d.*cos(t3);%-N1=4;N2=8;N3=12;z_1=(N1/2).*(M);z_2=(1/2).*(M);M1=sin(z_1)./(N1.*sin(z_2);%非歸一化的陣因子K1K_1=abs(M1);radio_1=K_1;X1=radio_1.*sin(tehta).*cos(phi);Y1=radio_1.

10、*sin(tehta).*sin(phi);Z1=radio_1.*cos(tehta);%-M=a+(beta.*d.*cos(t3);z_3=(N2/2).*(M);z_4=(1/2).*(M);M2=sin(z_3)./(N2.*sin(z_4);%非歸一化的陣因子K2K_2=abs(M2);radio_2=K_2;X2=radio_2.*sin(tehta).*cos(phi);Y2=radio_2.*sin(tehta).*sin(phi);Z2=radio_2.*cos(tehta);%-M=a+(beta.*d.*cos(t3);z_5=(N3/2).*(M);z_6=(1/2)

11、.*(M);M3=sin(z_5)./(N3.*sin(z_6);%非歸一化的陣因子K3K_3=abs(M3);radio_3=K_3;X3=radio_3.*sin(tehta).*cos(phi);Y3=radio_3.*sin(tehta).*sin(phi);Z3=radio_3.*cos(tehta);%-3D繪圖函數(shù)figure(5)surf(X1,Y1,Z1);%三維繪圖函數(shù)surf，采用偽彩色表示曲面的高度camlightrightlightcolorbaraxisimagerotate3Dontitle(f=3GHz,N=4,d=1/2波長(zhǎng),a=/2);figure(6)su

12、rf(X2,Y2,Z2);camlightrightlightcolorbaraxisimagerotate3Dontitle(f=3GHz,N=8,d=1/2波長(zhǎng),a=/2);figure(7)surf(X3,Y3,Z3)camlightrightlightcolorbaraxisimagerotate3Dontitle(f=3GHz,N=12,d=1/2波長(zhǎng),a=/2);%-%-只有陣列單元方向角a改變的天線方向圖N4=10;d1=lambda/4;a1=0;a2=pi/2;a3=pi/2+pi/10;A_3d=a1+(beta.*d1.*cos(t3);x_1=(N4/2).*(A_3d

13、);x_2=(1/2).*(A_3d);A_1=sin(x_1)./(N4.*sin(x_2);%非歸一化的陣因子K4K_4=abs(A_1);radio_4=K_4;X4=radio_4.*sin(tehta).*cos(phi);Y4=radio_4.*sin(tehta).*sin(phi);Z4=radio_4.*cos(tehta);%-B_3d=a2+(beta.*d1.*cos(t3);y_1_3d=(N4/2).*(B_3d);y_2_3d=(1/2).*(B_3d);B_1=sin(y_1_3d)./(N4.*sin(y_2_3d);%非歸一化的陣因子K5K_5=abs(B_

14、1);radio_5=K_5;X5=radio_5.*sin(tehta).*cos(phi);Y5=radio_5.*sin(tehta).*sin(phi);Z5=radio_5.*cos(tehta);%-C_3d=a3+(beta.*d1.*cos(t3);v_1=(N4/2).*(C_3d);v_2=(1/2).*(C_3d);C_1=sin(v_1)./(N4.*sin(v_2);%非歸一化的陣因子K6K_6=abs(C_1);radio_6=K_6;X6=radio_6.*sin(tehta).*cos(phi);Y6=radio_6.*sin(tehta).*sin(phi);

15、Z6=radio_6.*cos(tehta);%-figure(8)surf(X4,Y4,Z4);%三維繪圖函數(shù)surf，采用偽彩色表示曲面的高度camlightrightlightcolorbaraxisimagerotate3Dontitle(f=3GHz,N=10,d=1/4波長(zhǎng),a=0);figure(9)surf(X5,Y5,Z5);camlightrightlightcolorbaraxisimagerotate3Dontitle(f=3GHz,N=10,d=1/4波長(zhǎng),a=/2);figure(10)surf(X6,Y6,Z6)camlightrightlightcolorbar

16、axisimagerotate3Dontitle(f=3GHz,N=10,d=1/4波長(zhǎng),a=/2+/10);%-%-只有陣列單元間隔d改變的天線方向3D圖N5=20;d2=lambda/4;d3=lambda/2;d4=0.7*lambda;a4=pi/2;D_3d=a4+(beta.*d2.*cos(t3);p_1=(N5/2).*(D_3d);p_2=(1/2).*(D_3d);D_1=sin(p_1)./(N5.*sin(p_2);%非歸一化的陣因子K7K_7=abs(D_1);radio_7=K_7;X7=radio_7.*sin(tehta).*cos(phi);Y7=radio_

17、7.*sin(tehta).*sin(phi);Z7=radio_7.*cos(tehta);%-E_3d=a4+(beta.*d3.*cos(t3);q_1=(N5/2).*(E_3d);q_2=(1/2).*(E_3d);E_1=sin(q_1)./(N5.*sin(q_2);%非歸一化的陣因子K8K_8=abs(E_1);radio_8=K_8;X8=radio_8.*sin(tehta).*cos(phi);Y8=radio_8.*sin(tehta).*sin(phi);Z8=radio_8.*cos(tehta);%-F_3d=a4+(beta.*d4.*cos(t3);r_1_3

18、d=(N5/2).*(F_3d);r_2_3d=(1/2).*(F_3d);F_1=sin(r_1_3d)./(N5.*sin(r_2_3d);%非歸一化的陣因子K9K_9=abs(F_1);radio_9=K_9;X9=radio_9.*sin(tehta).*cos(phi);Y9=radio_9.*sin(tehta).*sin(phi);Z9=radio_9.*cos(tehta);%-figure(11)surf(X7,Y7,Z7);%三維繪圖函數(shù)surf，采用偽彩色表示曲面的高度camlightrightlightcolorbaraxisimagerotate3Dontitle(f

19、=3GHz,N=20,d=1/4波長(zhǎng),a=/2);figure(12)surf(X8,Y8,Z8);camlightrightlightcolorbaraxisimagerotate3Dontitle(f=3GHz,N=20,d=1/2波長(zhǎng),a=/2);figure(13)surf(X9,Y9,Z9)camlightrightlightcolorbaraxisimagerotate3Dontitle(f=3GHz,N=20,d=0.7波長(zhǎng),a=/2);二、%-均勻直線陣列天線的應(yīng)用之一：邊射陣clcclearallf=3e10;%30GHz,厘米波i=1;%天線電流值lambda=(3e8)/

20、f;%lambda=c/f波長(zhǎng)beta=2.*pi/lambda;N=15;t=0:0.01:2*pi;d1=lambda/4;%沒(méi)有柵瓣效應(yīng)的邊射陣，即間隔d波長(zhǎng)W2=beta.*d2.*cos(t);%定義kdcos(方向角)z3=(N/2).*W2;z4=(1/2).*W2;F2=sin(z3)./(N.*sin(z4);K2=abs(F2);figure(1)subplot(121);polar(t,K1);title(邊射陣f=30GHz,N=15,d=1/4波長(zhǎng));subplot(122);polar(t,K2);title(邊射陣（有柵瓣）f=30GHz,N=15,d=1.5倍波長(zhǎng));三、%-均勻直線陣列天線的應(yīng)用之二：普通端射陣clcclearallf=3e10;%30GHz,厘米波i=1;%天線電流值lambda=(3e8)/f;%lambda=c/f波長(zhǎng)beta=2.*pi/lambda;N=15;t=0:0.01:2*pi;d1=lambda/4;%沒(méi)有柵瓣效應(yīng)的普通端射陣，即間隔d1/2波長(zhǎng)W2=beta.*d2.*cos