Fixed-Wing Aircraft Creation with Objects
Use fully realized fixed-wing solutions for aircraft analysis, including static
stability and linearization. To analyze fixed-wing aircraft, use the Aero.FixedWing class and its supporting classes.
Classes
Aero.FixedWing | Define fixed-wing aircraft |
Aero.FixedWing.State | Define condition of Aero.FixedWing aircraft at time
instant |
Aero.FixedWing.Coefficient | Create Aero.FixedWing aircraft coefficient set |
Aero.Aircraft.CompositeCoefficient | Create composite aerodynamic coefficient (Since R2023b) |
Aero.FixedWing.Surface | Define aerodynamic and control surfaces on Aero.FixedWing
aircraft |
Aero.FixedWing.Thrust | Define thrust vector on fixed-wing aircraft |
Aero.Aircraft.Environment | Properties defining and managing aircraft environment |
Aero.Aircraft.Properties | Properties defining and managing aircraft |
Aero.Aircraft.ControlState | Define control states of fixed-wing aircraft |
Topics
- Analyze Fixed-Wing Aircraft with Objects
Use fully realized fixed-wing solutions for aircraft analysis, including static stability and linearization.
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.
Customize Fixed-Wing Aircraft with the Object Interface
Get started using fixed-wing aircraft in MATLAB.
Aircraft Design Optimization with the Fixed-Wing Object
Optimize aircraft size and geometry using the Aero.FixedWing object to enforce static stability constraints.
