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Design of a full state SDRE tracking controller for an unmanned aircraft
Date
2014-02-28
Author
PRACH, ANNA
Tekinalp, Ozan
Metadata
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This paper addresses the design of a nonlinear tracking controller for an unmanned aircraft. A State Dependent Riccati Equation (SDRE) method is utilized in a parallel-loop controller structure. We consider a classical approach of separating dynamics of a fixed- wing aircraft into longitudinal and lateral. SDRE controllers are designed for each of these control channels. The coupling effects, and nonlinearities are reected in the extended parametrization models of the channels. A nonlinear simulation model of an aircraft is used to validate the performance of the proposed control algorithm. Simulation results show the effectiveness of the algorithm for a coordinated turn maneuver.
URI
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=84894411979&origin=inward
https://hdl.handle.net/11511/106687
DOI
https://doi.org/10.2514/6.2014-1302
Conference Name
AIAA Guidance, Navigation, and Control Conference 2014 - SciTech Forum and Exposition 2014
Collections
Department of Aerospace Engineering, Conference / Seminar
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BibTeX
A. PRACH and O. Tekinalp, “Design of a full state SDRE tracking controller for an unmanned aircraft,” presented at the AIAA Guidance, Navigation, and Control Conference 2014 - SciTech Forum and Exposition 2014, National Harbor, MD, Amerika Birleşik Devletleri, 2014, Accessed: 00, 2023. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=84894411979&origin=inward.
