Videos and Webinars
Arkadiy Turevskiy, MathWorks
Trim and linearize a nonlinear aircraft model and use the resulting linear model to design a pitch rate damper controller using Simulink Control DesignTM.
Recorded: 3 Mar 2016
Batch Mode Trimming and Linearization
Simulink Control Design Overview
PID Controller Design for a DC Motor
Automatic Tuning of a Helicopter Flight Control System
Simulating a Multi-Stage Rolling Mill Process, Part 3:...
PID Control Made Easy
Design and Optimize MEMS Devices with Coventor MEMS+ and...
Time-Delay Systems: Analysis and Design with MATLAB and...
PID Controller Tuning for a Model with Discontinuities
Trim, Linearization, and Control Design for an Aircraft
Modeling, Simulation, and Flight Control Design of an...
Linking Requirements and Design for Aircraft
BAE Systems Designs Next-Generation Aircraft Control Systems
Aircraft Power Network Development with Model-Based Design
Presentation of a Platform for the Development of Aircraft...
Automatic Report Generation for Aircraft Power Network
Model-Based Design for Control Systems
Effects of CAN Bus Communications for Distributed Control...
Model-Based Control Design and Calibration Toolset for...
Desktop Real-Time Flight Simulator for Control Design
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