Optimal Input Design for Aircraft Stability and Control Flight Testing

Author:

Morelli Eugene A.ORCID

Funder

NASA Aeronautics Research Mission Directorate (ARMD) Transformational Tools and Technologies (TTT) project

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Management Science and Operations Research,Control and Optimization

Reference42 articles.

1. Brandon, J.M., Morelli, E.A.: Real-time Global Nonlinear Aerodynamic Modeling from Flight Data. J. Aircraft 53(5), 1261–1297 (2016)

2. Chen, R.T.N.: Input Design for Aircraft Parameter Identification Using Time-Optimal Control Formulation. Methods for Aircraft and Parameter Identification AGARD-CP-172, 13 (1975)

3. Cobleigh, B.R.: Design of Optimal Inputs for Parameter Estimation Flight Experiments with Application to the X-31 Drop Model. M.S. Thesis, The George Washington University, Washington, DC (1991)

4. Grauer, J.A.: Dynamic Modeling using Output-Error Parameter Estimation based on Frequency Responses Estimated with Multisine Inputs. NASA/TM 2018–220108 (2018)

5. Grauer, J.A., Boucher, M.J.: Real-Time Parameter Estimation for Flexible Aircraft. AIAA-2018-3155, AIAA Aviation Forum, Atlanta, GA (2018)

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