Control and Stability Analysis
Define aircraft configuration and dynamics to perform control design and flying
qualities analysis
Quickly create fixed-wing aircraft using the fixedWingAircraft function and its supporting functions. Then use fully
realized fixed-wing solutions for aircraft analysis, including static stability and
linearization.
Categories
- Fixed-Wing Aircraft Applications
Use fully realized fixed-wing solutions using functions and objects
- Flight Control Analysis
Analyze the motion and dynamics of aerospace vehicles with short-period requirements, boundary line, altitude contour plots, and entire flight envelopes
Featured Examples
Determine Static Stability of Fixed-Wing Aircraft
Create and analyze a fixed-wing aircraft in MATLAB® using Cessna C182 geometry and coefficient data.
Analyze State-Space Model for Linear Control and Static Stability Analysis
Convert a fixed-wing aircraft to a linear time invariant (LTI) state-space model for linear analysis.
Customize Fixed-Wing Aircraft with Additional Aircraft States
Construct and define a custom state for a fixed-wing aircraft.
