Removing High-Frequency Noise from an ECG Signal
Lowpass filter an ECG signal that contains high frequency noise.
Modeling a Fault-Tolerant Fuel Control System
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
Build a Digital Voltmeter
Build a digital voltmeter using MATLAB® Support Package for Raspberry Pi® Hardware.
ANOVA with Random Effects
Use anovan to fit models where a factor's levels represent a random selection from a larger (infinite) set of possible levels.
Introduction to MIMO Systems
Multiple-Input-Multiple-Output (MIMO) systems, which use multiple antennas at the transmitter and receiver ends of a wireless communication system. MIMO systems are increasingly
The Critical flutter velocity is computed for 2 single-span suspension bridges: One with a main span of 1.2 km and the other one with the main span of 0.45 km. The coupling of the lateral,
The data is a measurement from a class room The documentation of the measurement is found at http://legacy.spa.aalto.fi/projects/poririrs/
The data are room impulse responses measured in a control room type space in home environment.
The data are room impulse responses from left and right channel of a a home theater system.
The data are room impulse responses measured in a living room. Sakari Tervo & Jukka Pätynen, Aalto University, 2016 Sakari.Tervo@aalto.fi and Jukka.Patynen@aalto.fi Copyleft
Basic Matrix Operations
Basic techniques and functions for working with matrices in the MATLAB® language.
Anti-Windup Control Using a PID Controller
Use anti-windup schemes to prevent integration wind-up in PID controllers when the actuators are saturated. We use the PID Controller block in Simulink® which features two built-in
Approximating Nonlinear Relationships: Type S Thermocouple
Approximate nonlinear relationships of a type S thermocouple.
Designing a Guidance System in MATLAB and Simulink
Use the model of the missile airframe presented in a number of published papers (References ,  and ) on the use of advanced control methods applied to missile autopilot design. The