Port-Hamiltonian Flight Control of a Fixed-Wing Aircraft
dc.contributor.author | Fahmi, Jean-Michel W. | en |
dc.contributor.author | Woolsey, Craig A. | en |
dc.date.accessioned | 2024-11-06T15:07:45Z | en |
dc.date.available | 2024-11-06T15:07:45Z | en |
dc.date.issued | 2022-01 | en |
dc.description.abstract | This brief addresses the problem of stabilizing steady, wing level flight of a fixed-wing aircraft to a specified inertial velocity (speed, course, and climb angle). The aircraft is modeled as a port-Hamiltonian system and the passivity of this system is leveraged in devising the nonlinear control law. The aerodynamic force model in the port-Hamiltonian formulation is quite general; the static, state feedback control scheme requires only basic assumptions concerning lift, side force, and drag. Following an energy-shaping approach, the static state feedback control law is designed to leverage the open-loop system’s port-Hamiltonian structure in order to construct a control Lyapunov function. Asymptotic stability of the desired flight condition is guaranteed within a large region of attraction. Simulations comparing the proposed flight controller with dynamic inversion suggest it is more robust to uncertainty in aerodynamics. | en |
dc.description.sponsorship | This work was supported in part by the National Science Foundation under Grant CNS-1650465 and in part by the National Aeronautics and Space Administration (NASA) under Grant 80NSSC20M0162. | en |
dc.description.version | Accepted version | en |
dc.format.extent | pp. 408-415 | en |
dc.format.mimetype | application/pdf | en |
dc.identifier.doi | https://doi.org/10.1109/TCST.2021.3059928 | en |
dc.identifier.issue | 1 | en |
dc.identifier.orcid | Woolsey, Craig A. [0000-0003-3483-7135] | en |
dc.identifier.uri | https://hdl.handle.net/10919/121573 | en |
dc.identifier.volume | 30 | en |
dc.language.iso | en | en |
dc.publisher | IEEE | en |
dc.rights | In Copyright | en |
dc.rights.uri | http://rightsstatements.org/vocab/InC/1.0/ | en |
dc.title | Port-Hamiltonian Flight Control of a Fixed-Wing Aircraft | en |
dc.title.serial | IEEE Transactions on Control Systems Technology | en |
dc.type | Article - Refereed | en |
dc.type.dcmitype | Text | en |
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