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Dissertations / Theses on the topic 'Automated flight'

Author: Grafiati

Published: 5 June 2025

Last updated: 15 July 2025

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1

Chen, Haijian. "Automated peak identification for time -of -flight mass spectroscopy." W&M ScholarWorks, 2006. https://scholarworks.wm.edu/etd/1539623489.

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The high throughput capabilities of protein mass fingerprints measurements have made mass spectrometry one of the standard tools for proteomic research, such as biomarker discovery. However, the analysis of large raw data sets produced by the time-of-flight (TOF) spectrometers creates a bottleneck in the discovery process. One specific challenge is the preprocessing and identification of mass peaks corresponding to important biological molecules. The accuracy of mass assignment is another limitation when comparing mass fingerprints with databases.;We have developed an automated peak picking al

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2

Rothman, Keith Eric. "Validation of Linearized Flight Models using Automated System-Identification." DigitalCommons@CalPoly, 2009. https://digitalcommons.calpoly.edu/theses/81.

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Optimization based flight control design tools depend on automatic linearization tools, such as Simulink®’s LINMOD, to extract linear models. In order to ensure the usefulness and correctness of the generated linear model, this linearization must be accurate. So a method of independently verifying the linearized model is needed. This thesis covers the automation of a system identification tool, CIFER®, for use as a verification tool integrated with CONDUIT®, an optimization based design tool. Several test cases are built up to demonstrate the accuracy of the verification tool with respect

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3

Jang, Jinho S. M. Massachusetts Institute of Technology. "Trust and human performance in automated formation flight station-keeping." Thesis, Massachusetts Institute of Technology, 2005. http://hdl.handle.net/1721.1/34139.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2005.<br>Includes bibliographical references (p. 81-84).<br>This thesis primarily describes performance and decision heuristics of human operators intervention with an autonomous formation flight (AFF) system during monitoring of a station-keeping display. Due to mental and physical workloads, automation technologies have been applied to formation flight for precise station-keeping and resultant fuel reduction, shifting control authority from humans to machines. Accordingly, the human is not directly i

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4

Winet, Martin. "Development of an Automated Testing Tool for Flight Dynamic Models." Thesis, KTH, Flygdynamik, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-203808.

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5

Kurylovych, Oleksandr Yuriyovich. "Flight information service in Ukraine." Thesis, Національний авіаційний університет, 2020. http://er.nau.edu.ua/handle/NAU/41877.

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Робота публікується згідно наказу ректора від 21.01.2020 р. №008/од "Про перевірку кваліфікаційних робіт на академічний плагіат 2019-2020р.р. навчальному році" . Керівник проекту: доцент, Луппо Олександр Євгенійович<br>Flight information region (FIR) is a specified region of airspace in which a flight information service and an alerting service are provided. It is the largest regular division of airspace in use in the world today. Flight information regions established throughout all territory of the country. That why it is very important to provide flight information service in the best way.

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6

Miotto, Piero. "Fixed structure methods for flight control analysis and automated gain scheduleing." Thesis, Massachusetts Institute of Technology, 1997. http://hdl.handle.net/1721.1/10469.

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7

Bradley, Alexandre. "A comparison of whole life cycle costs of robotic, semi-automated, and manual build airport baggage handling systems." Thesis, Cranfield University, 2013. http://dspace.lib.cranfield.ac.uk/handle/1826/9311.

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This thesis proposes that a baggage handling system (BHS) environment can be defined and coupled to a whole life cycle cost (WLCC NPV) model. The results from specific experiments using the model can be used as the basis by which to commercially compare BHS flight build types of any capacity, and BHS geographical location. The model examined the three flight build types(i): Fully automatic build2; (ii) Semi-automatic build, and(iii); Manual build. The model has the ability to calculate a bag flow busy hour rate, and to replicate the baggage flow characteristics observed within real BHS opera

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8

Barrows, Andrew Kevin. "Development and inflight validation of an automated flight planning system using multiple-sensor windfield estimation." Thesis, Massachusetts Institute of Technology, 1993. http://hdl.handle.net/1721.1/46422.

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9

Watts, Robert Michael. "Development and evaluation of an automated path planning aid." Thesis, Georgia Institute of Technology, 2010. http://hdl.handle.net/1853/33839.

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In the event of an onboard emergency, air transport pilots are remarkably adept at safely landing their aircraft. However, the tasks of selecting an alternate landing site and developing a safe path to land are very difficult in the high workload, high stress environment of a cockpit during an emergency. The purpose of this research was to develop an automated path planning aid which would assist the pilot in the completion of these tasks. A prototype was developed to test this concept experimentally. The experiment was also intended to gather further information about how pilots think abo

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10

Efstathiou, Teresia. "AUTOMATISERADE FLYGPLAN: EN EMPIRISK STUDIE OM FLYGPASSAGERARES INSTÄLLNING." Thesis, Mälardalens högskola, Akademin för innovation, design och teknik, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-44677.

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Automatiska flygningssystem och kontrollpresentationsenheter utvecklas hela tiden inom flygteknik. Avionik företag skapar datoriserade system som ska kunna automatisera ytterligare aspekter av de operationer som sker i cockpit. Att flyga ska inte bedömas vara något riskfyllt och för att säkerställa säkerhetssynen är det betydelsefullt att ta reda på om människor uppfattar teknikens framgång som positiv. Syftet är att ta reda på människans uppfattning och inställning till automatiserade flygplan. Frågeställningen besvaras genom en empirisk studie där först en noggrann bakgrundsundersökning gjor

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11

Zaludin, Zairil A. "Flight dynamics and automatic flight control system of an hypersonic transport aircraft." Thesis, University of Southampton, 1999. https://eprints.soton.ac.uk/47120/.

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12

Peddle, Iain Kenneth. "Autonomous flight of a model aircraft /." Link to the online version, 2005. http://hdl.handle.net/10019/1155.

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13

Gunbatar, Yakup Rokhsaz Kamran. "Automatic airspace avoidance using advanced flight control system." Diss., A link to full text of this thesis in SOAR, 2006. http://soar.wichita.edu/dspace/handle/10057/648.

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Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.<br>"December 2006." Title from PDF title page (viewed on Oct 31, 2007). Thesis adviser: Kamran Rokhsaz. Includes bibliographic references (leaves 92-94).

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14

Wolfe, Douglas E. "Airplane dynamic modeling and automatic flight control design." Master's thesis, This resource online, 1990. http://scholar.lib.vt.edu/theses/available/etd-01202010-020132/.

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15

Buchner, Denzil. "Automatic control of commercial airliners in formation flight." Thesis, Stellenbosch : Stellenbosch University, 2015. http://hdl.handle.net/10019.1/96963.

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Thesis (MEng)--Stellenbosch University, 2015.<br>ENGLISH ABSTRACT: This thesis presents research contributing towards the automatic control of formation flight for commercial airliners. The motivation behind this research is to ultimately reduce fuel consumption of the trailing airliner through the utilisation of the aerodynamic coupling interactions between the trailing airliner and the wake vortices of the leading airliner. A traditional model for an airliner in isolated flight is developed and expanded to include formation flight interactions as functions of the vertical and late

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16

Bodin, Camilla. "Automatic Flight Maneuver Identification Using Machine Learning Methods." Thesis, Linköpings universitet, Reglerteknik, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-165844.

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This thesis proposes a general approach to solve the offline flight-maneuver identification problem using machine learning methods. The purpose of the study was to provide means for the aircraft professionals at the flight test and verification department of Saab Aeronautics to automate the procedure of analyzing flight test data. The suggested approach succeeded in generating binary classifiers and multiclass classifiers that identified six flight maneuvers of different complexity from real flight test data. The binary classifiers solved the problem of identifying one maneuver from flight tes

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17

Torralbo, Pilar Vicaria. "Optimized Automatic Calibration Tool for Flight Test Analogue Parameters." International Foundation for Telemetering, 2015. http://hdl.handle.net/10150/596389.

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ITC/USA 2015 Conference Proceedings / The Fifty-First Annual International Telemetering Conference and Technical Exhibition / October 26-29, 2015 / Bally's Hotel & Convention Center, Las Vegas, NV<br>The calibration processes consume a big quantity of resources: equipment and people, time and cost. As the number of calibration points increase the resources increase in the same extent. This automatic tool, aimed to reduce these resources, has been designed for commanding, managing and analyzing in real time a large number of acquired data points coming from the specimen under calibration and th

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18

Tang, Yi Rui. "Development, dynamic modeling, and autonomous flight control of small UAV helicopters." Thesis, University of Macau, 2017. http://umaclib3.umac.mo/record=b3691051.

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19

Peddle, Iain K. "Autonomous flight of a model aircraft." Thesis, Stellenbosch : Stellenbosch University, 2005. http://hdl.handle.net/10019.1/2711.

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Thesis (MScEng (Electrical and Electronic Engineering))--Stellenbosch University, 2005.<br>The successful development of a conventional flight autopilot for a model aircraft is presented. All aspects of the autopilot design are considered, from modeling to flight tests. A mathematical aircraft model, as a function of the aircraft’s physical parameters alone, is presented. A controller architecture capable of regulating the motion variables required for conventional flight using only low cost, off-the-shelf sensors is developed. The controller design complements the aircraft model developm

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20

Fitzsimons, Philip Matthew. "Design of a helicopter automatic flight control system using adaptive control." Diss., Georgia Institute of Technology, 1989. http://hdl.handle.net/1853/16641.

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21

Gee, Alan David. "Digital automatic flight control systems for advanced rotorcraft : an analysis framework." Thesis, University of York, 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.341474.

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22

Ehrman, Lisa M. "Automatic target recognition using passive radar and a coordinated flight model." Thesis, Available online, Georgia Institute of Technology, 2004:, 2004. http://etd.gatech.edu/theses/available/etd-06072004-131128/unrestricted/ehrman%5Flisa%5Fm%5F200405%5Fms.pdf.

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23

Holdsworth, Robert, and roberth@gil com au. "Autonomous in-flight path planning to replace pure collision avoidance for free flight aircraft using automatic depedent surveillance broadcast." Swinburne University of Technology, 2003. http://adt.lib.swin.edu.au./public/adt-VSWT20060608.141036.

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By the year 2020 the number of aircraft will have increased substantially and will be in �Free Flight�(that is, ATC will be devolved to the aircraft rather than being ground based). As an aid to navigation a more advanced form of collision avoidance will be required. This thesis proposes a method of collision avoidance planning using Automatic Dependent Surveillance-Broadcast (ADS-B) and Dynamic Programming (DP). It in essence enables Air Traffic Control (ATC) from within the cockpit for remote or uncontrolled airspace and is a step toward Free Flight. Free Flight requires quite different stra

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24

Minaud, Étienne. "Écologie hivernale des abeilles mellifères : contribution des traits d'histoire de vie des individus et des colonies au succès d'hivernation." Electronic Thesis or Diss., université Paris-Saclay, 2024. http://www.theses.fr/2024UPASB024.

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Dans les régions tempérées, les basses températures et le manque de ressources florales font de l'hiver une période critique pour la survie des abeilles mellifères, Apis mellifera, qui hivernent grâce à un ensemble d'adaptations à l'échelle des individus et à l'échelle des colonies. Mais depuis plus de 30 ans, de forts taux de mortalité hivernale sont observés mondialement, questionnant la durabilité du secteur apicole et celui de nombreux systèmes agricoles dépendant du service de pollinisation. Ces mortalités sont induites par de multiples facteurs de stress biotiques et abiotiques agissant

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25

Westberg, Michael. "Time of Flight Based Teat Detection." Thesis, Linköping University, Department of Electrical Engineering, 2009. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-19292.

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<p>Time of flight is an imaging technique with uses depth information to capture 3D information in a scene. Recent developments in the technology have made ToF cameras more widely available and practical to work with. The cameras now enable real time 3D imaging and positioning in a compact unit, making the technology suitable for variety of object recognition tasks</p><p>An object recognition system for locating teats is at the center of the DeLaval VMS, which is a fully automated system for milking cows. By implementing ToF technology as part of the visual detection procedure, it would be pos

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26

Benkhedda, Hassen. "Design of a transport aircraft automatic flight control system with analytical redundancy." Thesis, University of Southampton, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.241599.

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27

Alkhatib, K. Y. "Analytical redundancy scheme for improving reliability of automatic flight control systems for aircraft." Thesis, Loughborough University, 1985. https://dspace.lboro.ac.uk/2134/31989.

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Any redundancy scheme in aircraft control systems is usually considered separately from the control algorithms involved. All feedback control systems are usually designed under the assumption that their sensors will not fail. When the integrity requirements demand it, then a redundancy scheme must be designed to provide any required measurements with only extremely short interruptions to normal service being caused by failures of individual sensors.

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28

Lim, Bock-Aeng. "Design and rapid prototyping of flight control and navigation system for an unmanned aerial vehicle." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2002. http://sirsi.nps.navy.mil/uhtbin/hyperion-image/02Mar%5FLimBA.pdf.

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29

Fredman, Kristin, and Anna Freiholtz. "Use of Simulation Optimization for Clearance of Flight Control Laws." Thesis, Linköping University, Department of Electrical Engineering, 2006. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-5595.

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<p>Before a new flight control system is released for flight, a huge number of simulations are evaluated to find weaknesses of the system. This process is called flight clearance. Flight clearance is a very important but time consuming process. There is a need of better flight clearance methods and one of the most promising methods is the use of optimization. In this thesis the flight clearance of a simulation model of JAS 39 Gripen is examined. Two flight clearance algorithms using two different optimization methods are evaluated and compared to each other and to a traditional flight clearanc

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Al-Ataby, Ali. "Automatic detection, sizing and characterisation of weld defects using ultrasonic time-of-flight diffraction." Thesis, University of Liverpool, 2012. http://livrepository.liverpool.ac.uk/6413/.

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Ultrasonic time-of-flight diffraction (TOFD) is known as a reliable non-destructive testing technique for weld inspection in steel structures, providing accurate aw positioning and sizing. Despite all its good features, TOFD data interpretation and reporting are still performed manually by skilled inspectors and interpretation software operators. This is a cumbersome and error-prone process, leading to inevitable delay and inconsistency. The quality of the collected TOFD data is another issue that may introduce a host of error to the overall interpretation process. Manual interpretation focuse

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31

RINALDI, FILIPPO. "Automatic control of a multirotor." Doctoral thesis, Politecnico di Torino, 2014. http://hdl.handle.net/11583/2539287.

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Objective of this thesis is to describe the design and realisation phases of a multirotor to be used for low risk and cost aerial observation. Starting point of this activity was a wide literature study related to the technological evolution of multirotors design and to the state of the art. Firstly the most common multirotor configurations were defined and, according to a size and performance based evaluation, the most suitable one was chosen. A detailed computer aided design model was drawn as basis for the realisation of two prototypes. The realised multirotors were “X-shaped” octorotors wi

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32

Wu, Xiaofei. "A nonlinear flight controller design for an advanced flight control test bed by trajectory linearization method." Ohio : Ohio University, 2004. http://www.ohiolink.edu/etd/view.cgi?ohiou1177093858.

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33

Kutluay, Umit. "Aerodynamic Parameter Estimation Using Flight Test Data." Phd thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12613786/index.pdf.

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This doctoral study aims to develop a methodology for use in determining aerodynamic models and parameters from actual flight test data for different types of autonomous flight vehicles. The stepwise regression method and equation error method are utilized for the aerodynamic model identification and parameter estimation. A closed loop aerodynamic parameter estimation approach is also applied in this study which can be used to fine tune the model parameters. Genetic algorithm is used as the optimization kernel for this purpose. In the optimization scheme, an input error cost function is used

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34

Wise, Richard. "UAV guidance control laws for autonomous coordinated tracking of a moving ground target /." Thesis, Connect to this title online; UW restricted, 2007. http://hdl.handle.net/1773/9959.

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35

Isik, Sinem. "Flight Control System Design For An Over Actuated Uav Against Actuator Failures." Master's thesis, METU, 2010. http://etd.lib.metu.edu.tr/upload/3/12611652/index.pdf.

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This thesis describes the automatic flight control systems designed for a conventional and an over actuated unmanned air vehicle (UAV). A nonlinear simulation model including the flight mechanics equations together with the interpolated nonlinear aerodynamics, environmental effects, mass-inertia properties, thrust calculations and actuator dynamics is created<br>trim and linearization codes are developed. Automatic flight control system of the conventional UAV is designed by using both classical and robust control methods. Performances of the designs for full autonomous flight are tested throu

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36

Hansson, Jörgen. "Using Linear Fractional Transformations for Clearance of Flight Control Laws." Thesis, Linköping University, Department of Electrical Engineering, 2003. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-2041.

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<p>Flight Control Systems are often designed in linearization points over a flight envelope and it must be proven to clearance authorities that the system works for different parameter variations and failures all over this envelope. </p><p>In this thesis µ-analysis is tried as a complement for linear analysis in the frequency plane. Using this method stability can be guaranteed for all static parameter combinations modelled and linear criteria such as phase and gain margins and most unstable eigenvalue can be included in the analysis. A way of including bounds on the parameter variations using

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37

Ehrman, Lisa M. "An Algorithm for Automatic Target Recognition Using Passive Radar and an EKF for Estimating Aircraft Orientation." Diss., Georgia Institute of Technology, 2005. http://hdl.handle.net/1853/7510.

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Rather than emitting pulses, passive radar systems rely on illuminators of opportunity, such as TV and FM radio, to illuminate potential targets. These systems are attractive since they allow receivers to operate without emitting energy, rendering them covert. Until recently, most of the research regarding passive radar has focused on detecting and tracking targets. This dissertation focuses on extending the capabilities of passive radar systems to include automatic target recognition. The target recognition algorithm described in this dissertation uses the radar cross section (RCS) of pote

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38

Hedman, Robert. "Robust control system development forVTOL-to-fixed wing flight transition withthe EcoSoar UAV : A masters thesis in Automatic Control." Thesis, Luleå tekniska universitet, Institutionen för system- och rymdteknik, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-81000.

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A non switching, non linear, quaternion based attitude P2 controller, together with a sensitivitynormalizing function for the control surfaces has been simulated and implemented on a flying fixedwing with non vectored engines. In simulations the controller worked well in all flight modes,hovering, transition and flying, and also rejected a simple wind disturbance in all modes. Thefirst implementation on hardware did not work due to programming errors causing crashes withunrepairable damages. The second aircraft was built out of a piece of plywood to further simplifythe testing and tolerate mor

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Hartley, Edward Nicholas. "Model predictive control for spacecraft rendezvous." Thesis, University of Cambridge, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.609090.

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40

Duan, Pengfei. "Automatic Dependent Surveillance-Broadcast (ADS-B) Space-Oriented Message Set Design." Ohio University / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1305656769.

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41

Riviello, Luca. "Rotorcraft trim by a neural model-predictive auto-pilot." Thesis, Available online, Georgia Institute of Technology, 2005, 2005. http://etd.gatech.edu/theses/available/etd-04142005-203616/unrestricted/riviello%5Fluca%5F200505%5Fmast.pdf.

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Thesis (M. S.)--Aerospace Engineering, Georgia Institute of Technology, 2005.<br>Bottasso, Carlo, Committee Chair ; Hodges, Dewey, Committee Member ; Bauchau, Olivier, Committee Member. Includes bibliographical references.

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Uhlíř, Zdeněk. "Návrh a porovnání klasického a fuzzy regulátoru pro automatické udržení výšky letu." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2009. http://www.nusl.cz/ntk/nusl-228865.

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Účelem této práce je navrhnout zjednodušené modely klasického a fuzzy regulátoru pro automatické udržení výšky letu a porovnat jejich vlastnosti. Cílem je vyšetřit, zda fuzzy regulátor neprojeví lepší chování než klasický. Prostředkem pro návrh a srovnání vlastností obou regulátorů je posouzení odezev modelu systému letadlo-regulátor na požadavek změny výšky a modelu turbulence. Simulace jsou realizovány s pomocí prostředí MATLAB SIMULINK.

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Zhong, Lunlong. "Contribution to Fault Tolerant Flight Control under Actuator Failures." Phd thesis, INSA de Toulouse, 2014. http://tel.archives-ouvertes.fr/tel-00951340.

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L'objectif de cette thèse est d'optimiser l'utilisation d'actionneurs redondants pour un avion de transport lorsqu'une défaillance des actionneurs arrive en vol. La tolérance aux pannes résulte ici de la redondance des actionneurs présents sur l'avion. Différents concepts et méthodes classiques liés aux chaînes de commande de vol tolérantes aux pannes sont d'abord examinés et de nouveaux concepts utiles pour l'analyse requise sont introduits. Le problème qui est abordé ici est de développer une méthode de gestion des pannes des commandes de vol dans le cas d'une défaillance partielle des actio

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Sharma, Manu. "A neuro-adaptive autopilot design for guided munitions." Diss., Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/12470.

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45

Tagebrand, Emil, and Ek Emil Gustafsson. "Dataset Generation in a Simulated Environment Using Real Flight Data for Reliable Runway Detection Capabilities." Thesis, Mälardalens högskola, Akademin för innovation, design och teknik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-54974.

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Implementing object detection methods for runway detection during landing approaches is limited in the safety-critical aircraft domain. This limitation is due to the difficulty that comes with verification of the design and the ability to understand how the object detection behaves during operation. During operation, object detection needs to consider the aircraft's position, environmental factors, different runways and aircraft attitudes. Training such an object detection model requires a comprehensive dataset that defines the features mentioned above. The feature's impact on the detection ca

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46

Zhao, Yue. "Automatic Prevention and Recovery of Aircraft Loss-of-Control by a Hybrid Control Approach." Ohio University / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1458728101.

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47

Zhou, Yan. "Development of a data collection system for small Unmanned Aerial Vehicles (UAVs)." Thesis, Cape Peninsula University of Technology, 2011. http://hdl.handle.net/20.500.11838/1299.

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Dissertation (MTech (Mechanical Engineering))--Cape Peninsula University of Technology, 2011<br>This paper presents the development of a data collection system for a small unmanned Aerial Vehicle (UAV) flight. The following three facets comprise of a UAV system: (1) a UAV aircraft; (2) onboard avionics; and (3) a ground control station subsystem (Taha et al., 2010:1). In this project, the UAV aircraft is based on the low-cost autonomous quad-rotator system named “Arducopter Quad”, where the onboard avionic system utilizes both an ArduPilot Mega (APM) on-board controller and IMU sensor shi

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Dijkstra, Gabriel. "Beväpning av flygtekniker." Thesis, Försvarshögskolan, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:fhs:diva-8533.

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The AK5C has reached the edge of life and is due for replacement. Studies have been investigating a new small arm but focus of these studies has been the army and its personnel. For flight maintenance personnel the AK5C was too heavy and when working on an aircraft the technicians had to lay the weapon aside. The question this study aims to answer is how the future small arms for flight maintenance personnel might look like. To illustrate when a flight technician might use their weapon three scenarios where created. The scenarios where all originated from reglemente flygbassystem and focused o

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Fuggetti, Giuseppe. "Parameter Identification of a QuadPlane VTOL Drone Model by means of Reverse Engineering Techniques for Flight Control System Purposes." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2019.

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The aim of this thesis work is to identify the model parameters, both the inertial terms and the aerodynamic ones, of a new drone concept. Based on reverse engineering philosophy, the proposed techniques represents the new way the aerospace industry of drones is going to meet. All over the world the application of drones for the most disparate purposes is advancing exponentially and the need to bring new effective and efficient solutions to the market cannot ignore considering what has been done up to now for the drone industry. In this sense one wants to include reverse engineering in the pro

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Lombardi, Paolo. "Generic wind estimation and compensation based on residual generators and higher-order sliding mode schemes." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2016. http://amslaurea.unibo.it/10662/.

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This master thesis proposes a solution to the approach problem in case of unknown severe microburst wind shear for a fixed-wing aircraft, accounting for both longitudinal and lateral dynamics. The adaptive controller design for wind rejection is also addressed, exploiting the wind estimation provided by suitable estimators. It is able to successfully complete the final approach phase even in presence of wind shear, and at the same time aerodynamic envelope protection is retained. The adaptive controller for wind compensation has been designed by a backstepping approach and feedback linearizati

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