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@article{pflimlin_modeling_2010,
title = {Modeling and attitude control analysis of a ducted-fan micro aerial vehicle},
volume = {18},
issn = {09670661},
url = {https://linkinghub.elsevier.com/retrieve/pii/S0967066109001828},
doi = {10.1016/j.conengprac.2009.09.009},
pages = {209--218},
number = {3},
journaltitle = {Control Engineering Practice},
shortjournal = {Control Engineering Practice},
author = {Pflimlin, J.-M. and Binetti, P. and Souères, P. and Hamel, T. and Trouchet, D.},
urldate = {2024-03-25},
date = {2010-03},
langid = {english},
file = {Pflimlin et al. - 2010 - Modeling and attitude control analysis of a ducted.pdf:/Users/npross/Zotero/storage/NYXNQRF2/Pflimlin et al. - 2010 - Modeling and attitude control analysis of a ducted.pdf:application/pdf},
}
@inproceedings{pflimlin_hovering_2004,
location = {Nassau, Bahamas},
title = {Hovering flight stabilization in wind gusts for ducted fan {UAV}},
isbn = {978-0-7803-8682-2},
url = {http://ieeexplore.ieee.org/document/1429251/},
doi = {10.1109/CDC.2004.1429251},
eventtitle = {2004 43rd {IEEE} Conference on Decision and Control ({CDC}) ({IEEE} Cat. No.04CH37601)},
pages = {3491--3496 Vol.4},
booktitle = {2004 43rd {IEEE} Conference on Decision and Control ({CDC}) ({IEEE} Cat. No.04CH37601)},
publisher = {{IEEE}},
author = {Pflimlin, J.M. and Soueres, P. and Hamel, T.},
urldate = {2024-03-25},
date = {2004},
file = {Pflimlin et al. - 2004 - Hovering flight stabilization in wind gusts for du.pdf:/Users/npross/Zotero/storage/K5XIP2TS/Pflimlin et al. - 2004 - Hovering flight stabilization in wind gusts for du.pdf:application/pdf},
}
@inproceedings{pflimlin_aerodynamic_2007,
location = {Kos, Greece},
title = {Aerodynamic modeling and practical attitude stabilization of a ducted fan {UAV}},
isbn = {978-3-9524173-8-6},
url = {https://ieeexplore.ieee.org/document/7068497/},
doi = {10.23919/ECC.2007.7068497},
eventtitle = {2007 European Control Conference ({ECC})},
pages = {4023--4029},
booktitle = {2007 European Control Conference ({ECC})},
publisher = {{IEEE}},
author = {Pflimlin, Jean Michel and Binetti, Paolo and Trouchet, Daniel and Soueres, Philippe and Hamel, Tarek},
urldate = {2024-03-25},
date = {2007-07},
}
@article{naldi_design_2010,
title = {Design and experimental validation of a nonlinear control law for a ducted-fan miniature aerial vehicle},
volume = {18},
issn = {09670661},
url = {https://linkinghub.elsevier.com/retrieve/pii/S0967066110000444},
doi = {10.1016/j.conengprac.2010.02.007},
pages = {747--760},
number = {7},
journaltitle = {Control Engineering Practice},
shortjournal = {Control Engineering Practice},
author = {Naldi, Roberto and Gentili, Luca and Marconi, Lorenzo and Sala, Andrea},
date = {2010-07},
langid = {english},
file = {Naldi et al. - 2010 - Design and experimental validation of a nonlinear .pdf:/Users/npross/Zotero/storage/PINX95Y4/Naldi et al. - 2010 - Design and experimental validation of a nonlinear .pdf:application/pdf},
}
@inproceedings{ko_ducted_2007,
location = {Hilton Head, South Carolina},
title = {Ducted Fan {UAV} Modeling and Simulation in Preliminary Design},
isbn = {978-1-62410-160-1},
url = {https://arc.aiaa.org/doi/10.2514/6.2007-6375},
doi = {10.2514/6.2007-6375},
eventtitle = {{AIAA} Modeling and Simulation Technologies Conference and Exhibit},
booktitle = {{AIAA} Modeling and Simulation Technologies Conference and Exhibit},
publisher = {American Institute of Aeronautics and Astronautics},
author = {Ko, Andy and Ohanian, Osgar and Gelhausen, Paul},
date = {2007-08-20},
langid = {english},
file = {Ko et al. - 2007 - Ducted Fan UAV Modeling and Simulation in Prelimin.pdf:/Users/npross/Zotero/storage/9VB5WUZT/Ko et al. - 2007 - Ducted Fan UAV Modeling and Simulation in Prelimin.pdf:application/pdf},
}
@thesis{rothlin_flight_2021,
location = {Rapperswil, Switzerland},
title = {Flight control system for hovering a 'Ducted-Fan' prototype},
url = {https://www.ost.ch/de/details/abstracts/ducted-fan-prototype-17443},
pagetotal = {114},
institution = {{OST} {RJ} University of Applied Sciences},
type = {Bachelor Thesis},
author = {Rothlin, Tobias and Tönz, Tim},
date = {2021},
file = {Rothlin and Tönz - 2021 - Flight control system for hovering a 'Ducted-Fan' .pdf:/Users/npross/Zotero/storage/6E434P4J/Rothlin and Tönz - 2021 - Flight control system for hovering a 'Ducted-Fan' .pdf:application/pdf},
}
@inproceedings{koo_output_1998,
location = {Tampa, {FL}, {USA}},
title = {Output tracking control design of a helicopter model based on approximate linearization},
volume = {4},
isbn = {978-0-7803-4394-8},
url = {http://ieeexplore.ieee.org/document/761745/},
doi = {10.1109/CDC.1998.761745},
eventtitle = {37th {IEEE} Conference on Decision and Control},
pages = {3635--3640},
booktitle = {Proceedings of the 37th {IEEE} Conference on Decision and Control (Cat. No.98CH36171)},
publisher = {{IEEE}},
author = {Koo, T.J. and Sastry, S.},
date = {1998},
file = {Koo and Sastry - 1998 - Output tracking control design of a helicopter mod.pdf:/Users/npross/Zotero/storage/KDPUPDMP/Koo and Sastry - 1998 - Output tracking control design of a helicopter mod.pdf:application/pdf},
}
@book{stengel_flight_2022,
location = {Princeton Oxford},
edition = {Second edition},
title = {Flight dynamics},
isbn = {978-0-691-22025-3},
pagetotal = {894},
publisher = {Princeton University Press},
author = {Stengel, Robert F.},
date = {2022},
file = {Table of Contents PDF:/Users/npross/Zotero/storage/2TBQDVR6/Stengel - 2022 - Flight dynamics.pdf:application/pdf},
}
@article{packard_complex_1993,
title = {The complex structured singular value},
volume = {29},
rights = {https://www.elsevier.com/tdm/userlicense/1.0/},
issn = {00051098},
url = {https://linkinghub.elsevier.com/retrieve/pii/000510989390175S},
doi = {10.1016/0005-1098(93)90175-S},
pages = {71--109},
number = {1},
journaltitle = {Automatica},
shortjournal = {Automatica},
author = {Packard, A. and Doyle, J.},
date = {1993-01},
langid = {english},
file = {Accepted Version:/Users/npross/Zotero/storage/F6DIYFGM/Packard and Doyle - 1993 - The complex structured singular value.pdf:application/pdf},
}
@article{martini_dynamic_2009,
title = {Dynamic Modelling and Stability Analysis of Model-Scale Helicopters Under Wind Gust},
volume = {54},
rights = {http://www.springer.com/tdm},
issn = {0921-0296, 1573-0409},
url = {http://link.springer.com/10.1007/s10846-008-9280-z},
doi = {10.1007/s10846-008-9280-z},
pages = {647--686},
number = {4},
journaltitle = {Journal of Intelligent and Robotic Systems},
shortjournal = {J Intell Robot Syst},
author = {Martini, Adnan and Léonard, François and Abba, Gabriel},
date = {2009-04},
langid = {english},
file = {Martini et al. - 2009 - Dynamic Modelling and Stability Analysis of Model-.pdf:/Users/npross/Zotero/storage/2SPK4W3M/Martini et al. - 2009 - Dynamic Modelling and Stability Analysis of Model-.pdf:application/pdf},
}
@article{chirarattananon_dynamics_2017,
title = {Dynamics and flight control of a flapping-wing robotic insect in the presence of wind gusts},
volume = {7},
issn = {2042-8898, 2042-8901},
url = {https://royalsocietypublishing.org/doi/10.1098/rsfs.2016.0080},
doi = {10.1098/rsfs.2016.0080},
abstract = {With the goal of operating a biologically inspired robot autonomously outside of laboratory conditions, in this paper, we simulated wind disturbances in a laboratory setting and investigated the effects of gusts on the flight dynamics of a millimetre-scale flapping-wing robot. Simplified models describing the disturbance effects on the robot's dynamics are proposed, together with two disturbance rejection schemes capable of estimating and compensating for the disturbances. The proposed methods are experimentally verified. The results show that these strategies reduced the root-mean-square position errors by more than 50\% when the robot was subject to 80 cm s
−1
horizontal wind. The analysis of flight data suggests that modulation of wing kinematics to stabilize the flight in the presence of wind gusts may indirectly contribute an additional stabilizing effect, reducing the time-averaged aerodynamic drag experienced by the robot. A benchtop experiment was performed to provide further support for this observed phenomenon.},
pages = {20160080},
number = {1},
journaltitle = {Interface Focus},
shortjournal = {Interface Focus.},
author = {Chirarattananon, Pakpong and Chen, Yufeng and Helbling, E. Farrell and Ma, Kevin Y. and Cheng, Richard and Wood, Robert J.},
date = {2017-02-06},
langid = {english},
file = {Full Text:/Users/npross/Zotero/storage/UKKFL5SQ/Chirarattananon et al. - 2017 - Dynamics and flight control of a flapping-wing rob.pdf:application/pdf},
}
@thesis{pereira_hover_2008,
title = {Hover and Wind-Tunnel Testing of Shrouded Rotors for Improved Micro Air Vehicle Design},
url = {http://hdl.handle.net/1903/8752},
abstract = {This dissertation describes an experimental investigation of the effects of varying the shroud profile shape on the performance of {MAV} (Micro Air Vehicle) -scale shrouded rotors. Hover tests were performed on seventeen models with a rotor diameter of 16 cm (6.3 in) and various values of diffuser expansion angle, diffuser length, inlet lip radius and blade tip clearance, at various rotor collective angles. Compared to the baseline open rotor, the shrouded rotors showed increases in thrust by up to 94\%, at the same power consumption, or reductions in power by up to 62\% at the same thrust. These improvements surpass those predicted by momentum theory, due to the additional effect of the shrouds in reducing the non-ideal power losses of the rotor. The uniformity of the rotor wake was improved by the presence of the shrouds and by decreasing the blade tip clearance, resulting in lower induced power losses. Strong suction pressures were observed on the shroud inlet surface, at the blade passage region; taking advantage of this phenomenon could enable further increases in thrust. However, trade studies showed that, for a given overall aircraft size limitation, and ignoring considerations of the safety benefits of a shroud, a larger-diameter open rotor is more likely to give better performance than a smaller-diameter shrouded rotor. A single shrouded-rotor model was subsequently tested in translational flight at various angles of attack. In axial flow, at the same collective, the net thrust and the power consumption of the shrouded rotor were lower than those of the open rotor; in edgewise flow, the shrouded rotor produced greater thrust than the open rotor, while consuming less power. Measurements of the shroud surface pressure distributions illustrated the extreme asymmetry of the flow around the shroud, with consequent pitch moments much greater than those experienced by the open rotor. Except at low airspeeds and high angles of attack, the static pressure in the wake did not reach ambient atmospheric values at the diffuser exit plane; this challenges the validity of the fundamental assumption of the simple-momentum-theory flow model for short-chord shrouds in translational flight.},
institution = {University of Maryland (College Park, Md.)},
type = {phdthesis},
author = {Pereira, Jason Louie},
urldate = {2024-03-31},
date = {2008-08-29},
langid = {american},
file = {Full Text PDF:/Users/npross/Zotero/storage/L7WYTRQK/Pereira - 2008 - Hover and Wind-Tunnel Testing of Shrouded Rotors f.pdf:application/pdf},
}
@book{skogestad_multivariable_2010,
location = {Chichester},
edition = {2. ed., repr},
title = {Multivariable feedback control: analysis and design},
isbn = {978-0-470-01168-3 978-0-470-01167-6},
shorttitle = {Multivariable feedback control},
pagetotal = {574},
publisher = {Wiley},
author = {Skogestad, Sigurd and Postlethwaite, Ian},
date = {2010},
}
@thesis{rothlin_optimization_2024,
location = {Rapperswil, Switzerland},
title = {Optimization of a ducted fan prototype},
url = {https://www.ost.ch/de/details/abstracts/optimization-of-a-ducted-fan-prototype-18926},
institution = {{OST} {RJ} University of Applied Sciences},
type = {Semester Project},
author = {Rothlin, Tobias},
date = {2024},
}
|
