forked from ZhanLi/UWBIns
155 lines
3.7 KiB
Matlab
155 lines
3.7 KiB
Matlab
clear
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clc
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close all
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load('data1.mat');
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nn = size(imuPosX,1);
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%% lightHouse坐标系转换
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x = lightHousePosX * 100;
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y = -lightHousePosZ * 100;
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% 定义误差函数，即均方根误差
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errorFunction = @(params) sqrt(mean((x(1:500) * cos(params(1)) - y(1:500) * sin(params(1)) + params(2) - imuPosX(1:500)).^2 + (x(1:500) * sin(params(1)) + y(1:500) * cos(params(1)) + params(3) - imuPosY(1:500)).^2));
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% 使用 fminsearch 优化误差函数，找到使误差最小的旋转角和位移
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initialGuess = [0, 10, 10]; % 初始猜测值，[旋转角, 位移]
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optimizedParams = fminsearch(errorFunction, initialGuess);
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% 输出优化后的旋转角和位移
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rotationAngle = optimizedParams(1);
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xOffset = optimizedParams(2);
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yOffset = optimizedParams(3);
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% 旋转坐标
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xt = x * cos(rotationAngle) - y * sin(rotationAngle) + xOffset;
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yt = x * sin(rotationAngle) + y * cos(rotationAngle) + yOffset;
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%%
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tagN = 4;
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%标签坐标
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XN(:,1)=[-300;-300];
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XN(:,2)=[-300;300];
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XN(:,3)=[300;300];
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XN(:,4)=[300;-300];
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sim2=6;
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Q=diag(repmat(sim2,1,2*tagN));%协方差矩阵
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measure_AOA = zeros(4,nn);
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measure_d = zeros(4,nn);
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measure_AOA(1,:) = aoa1';
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measure_AOA(2,:) = aoa2';
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measure_AOA(3,:) = aoa3';
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measure_AOA(4,:) = aoa4';
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measure_d(1,:) = d1';
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measure_d(2,:) = d2';
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measure_d(3,:) = d3';
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measure_d(4,:) = d4';
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%% uwb解算
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x_uwb(1) = 0;
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y_uwb(1) = 0;
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theta_uwb=zeros(nn,1);
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for i=2:nn
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if measure_d(1,i) == 0
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x_uwb(i) = x_uwb(i-1);
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y_uwb(i) = y_uwb(i-1);
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continue;
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end
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[t1,theta] = WLS(XN,measure_AOA(:,i),measure_d(:,i),Q);
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x_uwb(i) = t1(1);
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y_uwb(i) = t1(2);
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theta_uwb(i) = 90-theta;
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theta_uwb(i) = mod(theta_uwb(i)+180,360)-180;
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derr_WLS(i)=norm(t1-[xt(i);yt(i)]);
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end
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thetat=zeros(nn,1);
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for i=2:nn
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detx=xt(i)-xt(i-1);
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dety=yt(i)-yt(i-1);
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thetat(i)=atan2d(detx,dety);
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end
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% Uwb.x=x_uwb;
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% Uwb.y=y_uwb;
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% Uwb.alpha=theta_uwb;
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% 角速度校准
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detW = mean(wZ(1:200));
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wZ = wZ - detW;
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x_imu(1) = 0;
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y_imu(1) = 0;
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Z=zeros(3,1);
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WW = 0.05;
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theta_imu(1) = 0;
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%
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% Imu.x=x_imu;
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% Imu.y=y_imu;
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% Imu.v=v_imu;
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% Imu.alpha=alpha_imu;
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% Imu.omega=omega_imu;
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%% KF
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R = diag([1 1 1]);
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% qq = 1;
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qq = 0.005;
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Q1 = diag([qq qq qq qq qq]);
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P0 = diag([0 0 0 0 0]);
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H = [1 0 0 0 0;
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0 1 0 0 0;
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0 0 0 1 0];
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I = eye(5);
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JF = zeros(5,5);
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X_pre = zeros(5,nn);
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X_kf(:,1) = [imuPosX(1);imuPosY(1);vXY(1)*100;0;wZ(1)];
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for i=2:nn
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% 计算IMU和里程计的时间差值
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detImuTime = imuDataRxTime(i) - imuDataRxTime(i-1);
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detOdomTime = odomDataRxTime(i)-odomDataRxTime(i-1);
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% 获得此时Z轴角速度
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w = wZ(i);
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% 获得小车的水平速度
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v = vXY(i)*100;
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% 计算速度增量
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detV=(vXY(i)-vXY(i-1))*100;
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% 计算位置增量
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detD = v*detImuTime;
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% 计算角度增量
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detTheta = w*180/pi*detImuTime;
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% 计算角速度的变化量
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detW = w-wZ(i-1);
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% 积分计算IMU的航位角
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theta_imu(i) = theta_imu(i-1)+detTheta;
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% 航向约束
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theta_imu(i) = mod(theta_imu(i)+180,360)-180;
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% 状态更新方程
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F = [1 0 detImuTime*cosd(X_kf(4,i-1)) 0 0;
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0 1 detImuTime*sind(X_kf(4,i-1)) 0 0;
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0 0 0 0 0;
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0 0 0 0 0;
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0 0 0 0 0;];
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% 获得水平和垂直方向的位置增量
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vtx = detD*cosd(theta_imu(i));
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vty = detD*sind(theta_imu(i));
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x_imu(i) = x_imu(i-1)+vtx;
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y_imu(i) = y_imu(i-1)+vty;
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X_next = [vtx;vty;detV;detTheta;detW];
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if (x_uwb(i) == x_uwb(i-1))&&(y_uwb(i) == y_uwb(i-1))
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X_kf(:,i) = X_kf(:,i-1)+X_next;
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errKf(i) = norm(X_kf(1:2,i)-[xt(i);yt(i)]);
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theta_kf(i) = X_kf(4,i);
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continue
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end
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X_pre(:,i) = X_kf(:,i-1)+X_next;
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% 观测矩阵: UWB的位置、UWB的航向角
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Z = [x_uwb(i);y_uwb(i);theta_uwb(i)];
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P = F*P0*F'+Q1;
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Kg_kf = P*H'*inv(H*P*H'+R);
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X_kf(:,i) = X_pre(:,i)+Kg_kf*(Z-H*X_pre(:,i));
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P0 = (I-Kg_kf*H)*P;
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errKf(i) = norm(X_kf(1:2,i)-[xt(i);yt(i)]);
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theta_kf(i) = X_kf(4,i);
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end
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plot(errKf);
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mean(errKf) |