Use Simulink® to model a quadcopter, based on the PARROT® series of mini-drones.

Use anovan to fit models where a factor's levels represent a random selection from a larger (infinite) set of possible levels.

Lowpass filter an ECG signal that contains high frequency noise.

Simulate the working of an automatic climate control system in a car using Simulink® and Stateflow®. You can enter a temperature value you would like the air in the car to reach by double

Generate a standalone C library from MATLAB code that implements a simple Sobel filter that performs edge detection on images. The example also shows how to generate and test a MEX function in

Combine Stateflow® with Simulink® to efficiently model hybrid systems. This type of modeling is particularly useful for systems that have numerous possible operational modes based on

Perform modal and transient analysis of a tuning fork.

This example was authored by the MathWorks community.

Perform a parameter sweep of material properties to determine the material with minimum deflection caused by a given load. Lastly, for such material we compute a load deflection curve. This

Analyze an idealized 3-D mechanical part under an applied load using Finite Element Analysis (FEA). The objective of the analysis is to determine the maximal deflection caused by the load.

This finite element thermal analysis (FEA) examines the heat tolerance for a robotics component of a commercial youBot.

This example was authored by the MathWorks community.

Approximate nonlinear relationships of a type S thermocouple.

Use the model of the missile airframe presented in a number of published papers (References [1], [2] and [3]) on the use of advanced control methods applied to missile autopilot design. The

Work with arrays having more than two dimensions. Multidimensional arrays can be numeric, character, cell, or structure arrays.

Use an extended Kalman filter with the MATLAB® Function block in Simulink® to estimate an aircraft's position from radar measurements. The filter implementation is found in the MATLAB

Model a conceptual air traffic control (ATC) radar simulation based on the radar range equation.

Use the Control System Toolbox™ and Simulink® Control Design™ to interact with Simulink to design a digital pitch control for the aircraft. In this example, we will design the controller to