Framework for Estimating Performance and Associated Uncertainty for Modified Aircraft Configurations

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

Flight testing has been the historical standard for determining aircraft airworthiness. However, increases in the cost of flight testing and the accuracy of inexpensive CFD encourage the adoption of certification by analysis to reduce or replace flight testing. A framework is introduced to predict the performance in the special case of a modification to an existing, previously certified aircraft. This framework uses a combination of existing flight tests or high fidelity data of the original aircraft as well as lower fidelity data from CFD or wind tunnel testing of the original and modified configurations to create 6-DOF flight dynamics models. Two methods are presented which generate an updated flight dynamics model and estimate the model form uncertainty for the modified aircraft configuration using knowledge of the original aircraft. This updated dynamics model and uncertainty estimate are then used to conduct non-deterministic simulations with wind turbulence included. The framework is applied to an example aircraft system to demonstrate the ability to predict the performance and associated model from the uncertainty of modified aircraft configurations.

Authors

• Casey L. Denham Langley Research Center
• Mayuresh Patil Georgia Institute of Technology
• Christopher J. Roy Virginia Tech
• Natalia Alexandrov Langley Research Center

Keywords

• uncertainty quantification
• modeling and simulation
• flight dynamics