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SDRE Based Guidance and Flight Control of Aircraft Formations
Date
2015-01-05
Author
Tekinalp, Ozan
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In this paper, a nonlinear guidance algorithm to control unmanned aircraft formationsis presented. This algorithm is based on State Dependent Riccati Equation (SDRE) ap-proach. Guidance equations are developed for leader-follower formation configurations.Flight control algorithms use SDRE based controllers as well, in the longitudinal and lat-eral dynamic channels of the aircraft. Leader aircraft follows the given speed, heading andaltitude commands and follower aircraft follows the leader using the commands generatedby SDRE based guidance algorithm. The effectiveness of the algorithms are demonstratedthrough simulations
URI
www.aiaa.org
https://hdl.handle.net/11511/80699
https://www.researchgate.net/publication/306260201_SDRE_Based_Guidance_and_Flight_Control_of_Aircraft_Formations
DOI
https://doi.org/10.2514/6.2015-0601
Conference Name
AIAA ScitTech 2015 Konferansı, 5 - 09 Ocak 2015
Collections
Department of Aerospace Engineering, Conference / Seminar
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O. Tekinalp, “SDRE Based Guidance and Flight Control of Aircraft Formations,” Orlando, Florida, Amerika Birleşik Devletleri, 2015, p. 1, Accessed: 00, 2021. [Online]. Available: www.aiaa.org.