Linear KF • Extended KF (EKF) • Unscented KF (UKF) • Sensor Fusion • 100% Original Code
Get expert guidance on designing and implementing Kalman filters in MATLAB for state estimation, sensor fusion, and control systems.
Every state estimation model is engineered from scratch by certified aerospace and control systems specialists.
Clean .m scripts and Simulink model test harnesses
implementing Discrete KF, EKF, or UKF blocks.
100% custom-derived state-space models, Jacobian calculations, and technical reports with 0% Turnitin similarity.
Tight deadline? We fast-track covariance tuning, non-linear Jacobians, and state estimation reports on-time.
High-resolution plots of state tracking error, error covariance bounds (±3σ), and innovation residual whiteness.
Unlimited adjustments to noise covariance ratios (Q/R), initial states (x0, P0), or documentation until full approval.
Your experimental flight datasets, proprietary robot kinematics, and student identity remain strictly confidential and encrypted.
How our control engineers deliver 100% verified, non-diverging Kalman filter state estimators.
Deriving continuous-to-discrete state transition matrices (A, B, C, D) or non-linear functions f(x, u) and h(x).
Computing analytical Jacobians (Fk, Hk) for EKF, or selecting optimal sigma points (α, β, κ) for UKF.
Tuning process noise (Q) and measurement noise (R) covariance matrices to ensure stability and zero innovation bias.
Delivery of .m scripts, .slx models, ±3σ error bound
plots, technical documentation, and 0% Turnitin similarity verification.
Copy and run this self-contained 1D tracking Kalman filter in any base MATLAB release without requiring the Control System or Sensor Fusion toolboxes.
x̂k|k-1 = A × x̂k-1 + B × ukPk|k-1 = A × Pk-1 × AT + QKk = Pk|k-1 × HT / (H × Pk|k-1 × HT + R)x̂k = x̂k|k-1 + Kk × (zk - H × x̂k|k-1)Pk = (I - Kk × H) × Pk|k-1% =========================================================================
% STANDALONE DISCRETE KALMAN FILTER IN MATLAB (1D KINEMATIC TRACKING)
% Zero Toolbox Required - Compatible with base MATLAB (R2018a - R2026b)
% Prepared by: MATLABSolutions State Estimation Team
% =========================================================================
clear; clc; close all;
%% 1. Simulation Parameters & Ground Truth Setup
N = 60; % Total simulation discrete time steps
dt = 0.5; % Sampling time interval (seconds)
true_accel = 0.15; % Constant acceleration (m/s^2)
t = (0:N-1) * dt; % Time vector
% True physics-based trajectory (constant acceleration)
true_pos = 0.5 * true_accel * t.^2;
true_vel = true_accel * t;
% Sensor Noise Simulation (Gaussian white noise)
meas_noise_var = 9.0; % Measurement variance R (sigma^2 = 9 m^2)
measurements = true_pos + sqrt(meas_noise_var) * randn(1, N);
%% 2. Discrete State-Space Model Formulation
% State vector x = [Position; Velocity]
A = [1, dt; % State transition matrix
0, 1];
H = [1, 0]; % Measurement observation matrix (position only)
% Noise Covariance Matrices
Q = [0.05, 0.00; % Process noise covariance matrix (model uncertainty)
0.00, 0.05];
R = meas_noise_var; % Measurement noise covariance (scalar)
%% 3. Kalman Filter Initialization
x_est = [0; 0]; % Initial state estimate [pos_0; vel_0]
P_est = [10, 0; % Initial state error covariance uncertainty
0, 10];
I = eye(2); % 2x2 Identity matrix
% Preallocate memory for logging
est_pos = zeros(1, N);
est_vel = zeros(1, N);
sigma_pos = zeros(1, N);
%% 4. Recursive Predict & Correct Loop
for k = 1:N
% --- STEP 1: TIME UPDATE (PREDICT) ---
x_pred = A * x_est;
P_pred = A * P_est * A' + Q;
% --- STEP 2: MEASUREMENT UPDATE (CORRECT) ---
z_k = measurements(k); % Current sensor reading
y_k = z_k - H * x_pred; % Innovation residual
S_k = H * P_pred * H' + R; % Residual covariance
K_k = P_pred * H' / S_k; % Optimal Kalman Gain
x_est = x_pred + K_k * y_k; % Corrected state estimate
P_est = (I - K_k * H) * P_pred; % Corrected error covariance
% Store history
est_pos(k) = x_est(1);
est_vel(k) = x_est(2);
sigma_pos(k) = sqrt(P_est(1, 1)); % Standard deviation bound
end
%% 5. Performance Metrics & Visualization
rmse_pos = sqrt(mean((true_pos - est_pos).^2));
rmse_raw = sqrt(mean((true_pos - measurements).^2));
noise_reduction_pct = (1 - rmse_pos / rmse_raw) * 100;
fprintf('--- Kalman Filter Tracking Results ---
');
fprintf('Raw Sensor Measurement RMSE : %.3f meters
', rmse_raw);
fprintf('Kalman Filter Estimate RMSE : %.3f meters
', rmse_pos);
fprintf('Noise Attenuation Percentage : %.1f%%
', noise_reduction_pct);
% Generate Plots
figure('Color', 'w', 'Position', [100, 100, 800, 500]);
subplot(2, 1, 1);
plot(t, measurements, 'r.', 'MarkerSize', 8, 'DisplayName', 'Noisy Sensor (R)');
hold on;
plot(t, true_pos, 'k-', 'LineWidth', 1.8, 'DisplayName', 'True Trajectory');
plot(t, est_pos, 'b-', 'LineWidth', 2.0, 'DisplayName', 'Kalman Estimate');
fill([t, fliplr(t)], [est_pos + 3*sigma_pos, fliplr(est_pos - 3*sigma_pos)], ...
'b', 'FaceAlpha', 0.15, 'EdgeColor', 'none', 'DisplayName', '\pm3\sigma Covariance Bound');
grid on; xlabel('Time (s)'); ylabel('Position (m)');
title(sprintf('1D Kalman Filter Tracking (RMSE: %.2f m | %.1f%% Noise Reduction)', ...
rmse_pos, noise_reduction_pct));
legend('Location', 'NorthWest');
subplot(2, 1, 2);
estimation_error = true_pos - est_pos;
plot(t, estimation_error, 'm-', 'LineWidth', 1.5, 'DisplayName', 'Estimation Error');
hold on;
plot(t, 3*sigma_pos, 'k--', 'LineWidth', 1.2, 'DisplayName', '+3\sigma Bound');
plot(t, -3*sigma_pos, 'k--', 'LineWidth', 1.2, 'DisplayName', '-3\sigma Bound');
grid on; xlabel('Time (s)'); ylabel('Error (m)');
title('Tracking Error within \pm3\sigma Confidence Envelope');
legend('Location', 'NorthWest');
The ratio Q / R controls the balance of the filter. Tuning this prevents divergence and minimizes state lag:
Linear Kalman filters require linear dynamics x = A x + B u. Real-world applications require advanced nonlinear variants:
f(x, u) and h(x) using first-order Taylor series Jacobians. Ideal for GPS/IMU attitude fusion & EV battery SOC.
Our PhD control systems specialists formulate exact Jacobians, tune positive-definite covariance matrices, and build verified MATLAB & Simulink models within 3 to 24 hours.
Explore actual aerospace navigation, EV battery estimation, and autonomous tracking assignments solved by our team.
Task: Implement 2nd-order RC equivalent circuit model (ECM), define non-linear OCV-SOC polynomial relationship, implement Dual-EKF (slow timescale for capacity/R0, fast timescale for SOC), and test on dynamic UDDS drive cycles.
dual_ekf_bms_soc.slx,
bms_ekf.m, SOC error plots.
Task: Track a high-speed maneuvering aircraft in Cartesian coordinates using non-linear range-bearing polar radar observations (r = √(x2 + y2), θ = arctan(y/x)), formulate scaled unscented transform sigma points.
ukf_radar_tracker.m, Cartesian
tracking trajectory, error ellipses plot.
Task: Implement 2,000-particle SIR filter for non-linear growth model with bimodal non-Gaussian measurement noise, implement systematic resampling to mitigate particle degeneracy (Neff < N/2).
sir_particle_filter.m,
particle distribution evolution plot, MSE comparison.
Why control systems professors immediately spot raw AI code and how verified state estimation models protect your grade.
| Evaluation Criteria | MATLABSolutions | Raw AI (ChatGPT) | Generic Freelancers |
|---|---|---|---|
| Analytical Jacobian Matrix Formulations | 100% Exact Analytical Jacobians | Partial Derivative Sign Errors | Dimension Mismatch Errors |
Covariance Tuning
(Q & R Positive Definite) |
Stable & Non-Diverging Matrices | Covariance Divergence / NaNs | Arbitrary Identity Matrices |
| Turnitin Plagiarism Certificate | 0% Plagiarism Report Attached | Flagged by AI Detectors | Copied from GitHub Repos |
| ±3σ Covariance Bounds & Residual Whiteness | Complete Statistical Figures | No Figures Generated | Extra Charge for Figures |
| Free Revisions & WhatsApp Support | 7 Days Free + Direct Hotline | No Human Follow-Up | Slow / Disappearing Sellers |
Pricing is based purely on state dimension, non-linear filter architecture, and turnaround urgency.
1D/2D Discrete Kalman filter, constant velocity tracking & sensor noise filtering.
.m script
Non-linear EKF/UKF, GPS/IMU fusion, EV battery SOC & Simulink integration.
.slx)Quaternion Error-State EKF, Particle Filter & Master's / PhD Dissertation.
Everything aerospace, robotics, electrical, and autonomous systems students ask before getting started with our Kalman Filter service.
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