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Flatness-based aircraft trajectory optimization and tracking using pseudospectral method
, R Sandeepkumar
Published in American Institute of Aeronautics and Astronautics

In this paper, we use a flatness-based approach for computing constrained trajectories while optimizing an objective function for a six degree of freedom aircraft. The resulting optimal control problem in flat output space is numerically solved using Legendre-Gauss-Lobatto pseudospectral method. A real-time linear optimal controller based on flatness is designed and successfully applied to time-varying trajectory tracking.

About the journal
PublisherData powered by TypesetAmerican Institute of Aeronautics and Astronautics
Impact Factor1.868
Open AccessNo
Citation Styleunsrt
Sherpa RoMEO Archiving PolicyGreen