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Flight Dynamic Simulation with Nonlinear Aeroelastic Interaction using the ROM-ROM Procedure

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX11CB68C
Agency Tracking Number: 094184
Amount: $599,998.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: A2.07
Solicitation Number: N/A
Solicitation Year: 2009
Award Year: 2011
Award Start Date (Proposal Award Date): 2011-06-01
Award End Date (Contract End Date): 2013-09-30
Small Business Information
Scottsdale, AZ 85258-4578
United States
DUNS: 182103291
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: Yes
Principal Investigator
 Ping Chih Chen
 Principal Investigator
 (480) 945-9988
Business Contact
 Jennifer Scherr
Title: Business Official
Phone: (480) 480-9988
Research Institution

ZONA Technology, Inc. proposes to develop an integrated flight dynamics simulation capability with nonlinear aeroelastic interactions by combining a flight dynamics model and an add-on nonlinear aeroelastic solver in a Simulink environment. This nonlinear aeroelastic solver is generated by interacting a nonlinear structural Reduced Order Model (ROM) with a Neural-Network-based (NN-based) aerodynamic ROM and a gust ROM to provide the incremental aeroelastic forces and moments of a classical flight dynamics model. In this way, the flight dynamics model is kept with minimum changes so that this integrated flight dynamics simulation remains in the frame work of a 6-degrees-of-freedom simulation environment. The nonlinear structural ROM employs an ELSTEP/FAT procedure that operates on a commercial nonlinear finite element software to construct the nonlinear stiffness matrices. The NN-based and gust aerodynamic ROM is generated using a system identification technique operating on a CFD code to evaluate the weights and biases in a two-layer feed-forward NN system. The end product is called FuNL-DFS that can simulate the key aeroelastic coupling mechanism between nonlinear structural dynamics and nonlinear unsteady aerodynamics with classical rigid body dynamics and can be used for control law development, maneuvering flight simulation, flight loads prediction and handling quality assessment. The FuNL-DFS system will be validated with the flight test data of the Predator B Aircraft.

* Information listed above is at the time of submission. *

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