Nonlinear Guidance of Aircraft Formations

Date

2015-01-05

Author

Tekinalp, Ozan

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Nonlinear formation flight control algorithm for a pair of unmanned aerial vehicles (UAV) is proposed. The leader-follower approach to formation flight is adopted. The leader maintains a prescribed trajectory while the follower is controlled to track and maintain a fixed relative distance from its leader. Two nonlinear guidance algorithms, Lyapunov and State Dependent Ricatti Equation, (SDRE) based are proposed for the relative guidance of the follower UAV. The resulting formation control systems are tested through simulations and their effectiveness are demonstrated. © 2015, E-flow American Institute of Aeronautics and Astronautics (AIAA). All rights reserved.

URI

www.aiaa.org
https://hdl.handle.net/11511/79061

Conference Name

AIAA Guidance, Navigation, and Control Conference, 2015

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

O. Tekinalp, “Nonlinear Guidance of Aircraft Formations,” presented at the AIAA Guidance, Navigation, and Control Conference, 2015, Kissimmee; United States, 2015, Accessed: 00, 2021. [Online]. Available: www.aiaa.org.