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Download Real Time Aircraft Dynamic Models Datasheet (pdf)
View Real Time Aircraft Dynamic Models Datasheet Online 
Overview
The FLIGHTLAB Development System is capable of supporting both fixed and rotary wing flight dynamics simulation but the emphasis to-date has been on supporting the more challenging area of rotorcraft simulation. Under a CRADA between ART and the Army's Aeroflightdynamics Directorate (AFDD), the Army has agreed to support ART in developing a library of Army rotorcraft models that can be run under the FLIGHTLAB Development System. In connection with this CRADA, The Aviation Engineering Division (AED) at the Army's Redstone Arsenal has worked with ART to create a library of Army rotorcraft models and ART has transitioned these models into Army training simulators. ART has provided flight dynamics models of the UH-60A/L, AH-64A/D, and OH-58D for the Army's Aviation Combined Arms Tactical Training (AVCATT) Program. Other models developed jointly with AED include the RAH-66 Comanche and the CH-47D Chinook. ART has also modeled the AH-1, UH-1 and OH-6 helicopters..
With the support of the Navy's Manned Flight Simulator (MFS) at the Naval Air Warfare Center Aircraft Division, Patuxent River, MD, ART has developed a blade element model of the V-22 and ART is integrating it with a HeliFlight-R simulator to be delivered to the Navy for support of flight test applications, including shipboard operations testing. ART has also developed SH-60 and AH-1W models for Navy applications. Under the Army's LSHIP program, ART has integrated a UH-60L model with shipboard landing capability into the Army's UH-60 Operational Flight Trainer (OFT) at Ft. Campbell to demonstrate the training potential.
ART has also developed a Level D version of our OH-58D helicopter model and has successfully supported its integration and testing with two Operational Flight Trainers (OFTs) that a now currently being used in the Army's Flight School XXI Program at Ft. Rucker.
Flight Dynamics Models Key Features
- Blade Element Main and Tail Rotor
- Three State Dynamic Inflow
- Fuselage and Empennage
- Aerodynamic Interference
- Nonlinear Engine and Drive-train
- Nonlinear Control System
- Landing Gear
- Weight and Balance
- Atmospheric Environment
- Custom Interface
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