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객체를 사용한 고정익 항공기 생성
객체를 활용하여 완전 구현된 고정익 솔루션 사용
정적 안정성 및 선형화를 비롯하여 항공기 분석을 위한 완전 구현된 고정익 솔루션을 사용합니다. 고정익 항공기를 분석하려면 Aero.FixedWing 클래스와 그 지원 클래스를 사용하십시오.
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.Specification | Define Aero.FixedWing specification set (R2025a 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.
