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Trim Analysis
Blade Element Model Rotor View
Example generic helicopter model
- UH-60 Blackhawk weight class
- Single main and tail rotor configuration with:
- Turbine Engine
- Landing gears (steerable)
- Variable incidence horizontal stabilizer
- Autopilot
- Fuselage
- Vertical stabilizer
Analysis tools
- Trim analysis (Video)
- Model linearization (Video1 Video2)
- Acceleration analysis (Video)
- Dynamic response analysis (Video)
- Maximum speed analysis (Video)
- Maximum climb rate analysis (Video)
- Multicore support for analysis tools
- All analysis tools are accessible via Matlab functions hence they are scriptable
- Develop helicopter models and control systems with Rotorlib FDM for Matlab and deploy on a simulator powered by RotorLib FDM for C++.
Supported helicopter configurations
- Single main and tail rotor
- Tandem
- Coaxial
- Quadcopter
Normal procedures
- Hover (IGE, OGE)
- Forward flight
- Climb, descend
- Steep approach
- Coordinated turn
- Sideways and backward flight
- Taxi
- Hovering taxi
Simulated aerodynamic effects
- Translational tendency
- Non-uniform inflow
- Translational lift
- Asymmetry of lift
- Effective translational lift
- Compressibility and yawed flow
- Ground effect
- Autorotation
- Interference effects (main rotor downwash effects on surfaces and tail rotor)
Model Library
- Blade element and Momentum theory rotor models for main and tail rotors
- Weight and balance
- Programmable Generic Control System
- Engine and Drive Train (Not supported in Simulink)
- Turbine Engine (add-on)
- Constant RPM Engine
- Freewheeling clutch for engine and drive train
- Multiple Engines
- Engine start-up procedures
- Fuselage and Stabilizers
- Wind and turbulence model
- Slung Loads (add-on) (Not supported in Simulink)
Design Tools
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