Abstract
Knowledge of the safe maneuvering envelope is of vital importance to prevent loss of control aircraft accidents. In this paper, determination of the safe maneuvering envelope is addressed in a reachability framework. The forwards and backwards reachable sets for a set of initial trim conditions are obtained by solving a Hamilton Jacobi partial differential equation through a semi-Lagriangian method. Results obtained using this approach are presented for a nonlinear, high-fidelity, F-16 aircraft model.
Cite
CITATION STYLE
van Oort, E. R., Chu, Q. P., & Mulder, J. A. (2011). Maneuver Envelope Determination through Reachability Analysis. In Advances in Aerospace Guidance, Navigation and Control (pp. 91–102). Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-19817-5_8
Register to see more suggestions
Mendeley helps you to discover research relevant for your work.
