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객체를 사용하여 고정익 항공기 생성
객체를 사용하여 완전히 실현된 고정익 솔루션을 사용합니다.
정적 안정성과 선형화를 포함하여 항공기 분석을 위해 완벽하게 구현된 고정익 솔루션을 사용합니다. 고정익 항공기를 분석하려면 Aero.FixedWing 클래스와 지원 클래스를 사용합니다.
클래스
Aero.FixedWing | Define fixed-wing aircraft (R2021a 이후) |
Aero.FixedWing.State | Define condition of Aero.FixedWing aircraft at time
instant (R2021a 이후) |
Aero.FixedWing.Coefficient | Create Aero.FixedWing aircraft coefficient set (R2021a 이후) |
Aero.Aircraft.CompositeCoefficient | Create composite aerodynamic coefficient (R2023b 이후) |
Aero.FixedWing.Surface | Define aerodynamic and control surfaces on Aero.FixedWing
aircraft (R2021a 이후) |
Aero.FixedWing.Thrust | Define thrust vector on fixed-wing aircraft (R2021a 이후) |
Aero.Aircraft.Environment | Properties defining and managing aircraft environment (R2021a 이후) |
Aero.Aircraft.Properties | Properties defining and managing aircraft (R2021a 이후) |
Aero.Aircraft.ControlState | Define control states of fixed-wing state (R2021a 이후) |
도움말 항목
- Analyze Fixed-Wing Aircraft with Objects
Use fully realized fixed-wing solutions for aircraft analysis, including static stability and linearization.
추천 예제
Determine Nonlinear Dynamics and 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.
