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Dissertations / Theses on the topic 'Aerospace law'

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Published: 7 June 2025

Last updated: 2 August 2025

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1

Bunker, Donald H. (Donald Harry) 1940. "The legal aspects of aerospace finance in Canada /." Thesis, McGill University, 1987. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=76526.

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Access to adequate financing for the development of Canada's aerospace industry, which is a significant contributor to the country's gross national product, is controlled by the financial community generally. In order for one to successfully transact with the community, their fears and expectations must be clearly understood and respected. This study begins in Chapter I with an examination of the types of financing available, and Chapter II discusses how these financings may be funded. Chapter III contains a detailed consideration of the types of security required to secure such obligations, w

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2

Hoversten, Michael R. "The law governing aerospace warfare in the twenty-first century /." Thesis, McGill University, 2000. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=33360.

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The world is in the midst of a revolution in the conduct of military operations wherein modern military aerospace information systems, weapons and their associated weapon systems are changing the conduct of warfare. Aerospace power has become the dominant, if not decisive, factor in modern warfare. Yet, there are currently no treaties dealing specifically with the law of armed conflict in the air and space environments. Chapter I describes the evolution to date of the law governing aerospace warfare. Chapter II analyzes the relevance of military interventions in Iraq and Yugoslavia (Bosnia; Ko

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3

Hoverstein, Michael R. "The law governing aerospace warfare in the twenty-first century /." (Requires Adobe Acrobat Reader), 2000. http://stinet.dtic.mil/str/tr4%5Ffields.html.

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4

Fortin, Pierre 1960. "Artificial space debris and international law." Thesis, McGill University, 1990. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=59927.

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In just three decades of human exploration and utilization of outer space, an unwanted legacy of thousands of artificial space debris has been left behind.<br>The purpose of this thesis is to analyse the appropriate technical aspects of the artificial space debris issue and to explore the legal ramifications of the question.<br>The first chapter is devoted to the technical aspects and covers topics such as the origins and location of artificial space debris, the hazards they constitute, the anticipated damage that might be caused by such debris and the likelihood of its occurrence.<br>In the s

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5

Trepczynski, Susan J. "Edge of space : emerging technologies, the 'new' space industry, and the continuing debate on the delimitation of outer space." Thesis, McGill University, 2006. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=101829.

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Nearly fifty years have passed since the beginning of the space age, but international lawmakers have yet to determine where airspace ends and outer space begins. This paper examines the need to settle the boundary dispute, specifically taking into account the effect it has on emerging technologies and the 'new' space industry.<br>The opening chapter examines the fundamental changes that have occurred since the beginning of the space age, both in terms of the technology and the space exploration infrastructure. The background of the delimitation question is then provided, followed by a discuss

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6

Vissepó, Varlin. "Reusable launch vehicles : crossroads between air and space law." Thesis, McGill University, 2003. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=81239.

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Space technology is increasingly becoming part of our everyday life, businesses, governments and private entities rely heavily on satellite communications for their respective dealings and transactions. On the other hand, not all transactions or businesses can be done solely through telecommunications, we often need to get on an airplane and go somewhere else to do our respective businesses and if we are on vacation we definitely need to travel. The problem is that airplane travel, although fast, sometimes is not fast enough. Today's people want convenience and when they want something

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7

Fobe, Jean-Michel. "Legal aspects and insurance of the liability of civil aerospace products manufacturers in the EEC, for damage to third parties." Thesis, McGill University, 1993. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=26198.

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Civil aerospace products manufacturers in the EEC may, as in the USA, be called into litigation as co-defendant following an aircraft accident by the victims or their dependents. As opposed to the airlines, their liability is not limited by international conventions.<br>This thesis examines their liability and insurance in case of damage to third parties after the entry into force of EEC Directive 85/374 on liability for defective products.<br>First, a brief description will be given of the evolution of the aerospace industry in Europe and its governmental regulation through certification. In

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8

Fujizawa, Brian T. "Control Law Design and Validation for a Helicopter In-Flight Simulator." DigitalCommons@CalPoly, 2010. https://digitalcommons.calpoly.edu/theses/240.

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In-flight simulation allows one aircraft to simulate the dynamic response of another aircraft. A control system designed to give RASCAL, a JUH-60A Black Hawk helicopter based at Moffett Field, CA, in-flight simulation capabilities has been designed, optimized and validated in this research. A classical explicit model following control system with a frequency dependent feedback controller was used. The frequency dependent controller allows model following of the attitude in the short term and the velocity in the long term. Controller gains were optimized using a high order, linearized model

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9

Nordlund, Frédéric. "Le régime juridique des activités industrielles et commerciales conduites dans l'espace extra-atmosphérique : nouvelles orientations." Thesis, McGill University, 1989. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=59581.

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Current technology and the planning of ambitious programs for the next decade tend to transform the stakes inherent in space activities. In effect, the launching of space stations and platforms pave the way towards new industrial prospects previously unheard of to date. Thus, the objective of this thesis is to present an outline of these new prospects and to undertake a legal analysis motivating the transition from basic research to commercial applications.<br>Consequently, the preliminary chapter will describe the general characteristics of those future trends towards commercial and industria

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10

Fabbri, Riccardo. "Conceptualization, design & simulation of a small asteroid probe." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2019.

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The Asteroid Impact and Deflection Assessment (AIDA), is an upcoming mission resulting from the collaboration of ESA and NASA and aims at assessing the effects of a kinetic impact on an asteroid for the purpose of threat mitigation. In this framework, this research seeks to prove the feasibility of a small lander design able to autonomously land on the secondary object of the asteroid system Didymos. Initially, an overview of the most suitable guidance laws and sensors is provided. This highlighted that some types of proportional navigation guidance laws and the ZEM/ZEV could be good candidat

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11

Ma, Weitao. "Cost modelling for manufacturing of aerospace composites." Thesis, Cranfield University, 2011. http://dspace.lib.cranfield.ac.uk/handle/1826/6279.

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The application of composites has been increasing dramatically in aerospace structures recently, for example, composites have contributed over 50 percent of the structure mass of large transport airplanes Boeing 787 and Airbus 350XWB. However, the further usage has been restricted because of the high material and manufacturing costs. Hence, it is essential to utilize cost estimation tools for accurate cost estimation in the early design stages, and then efficient decisions and design optimizations could be made to reduce the cost of composite products. This research project aims to develop a c

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12

Mirmasoudi, Sara. "High Temperature Transient Creep Analysis of Metals." Wright State University / OhioLINK, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=wright1452693927.

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13

Stang, Eric Thomas. "Constitutive Modeling of Creep in Leaded and Lead-Free Solder Alloys Using Constant Strain Rate Tensile Testing." Wright State University / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=wright1548338008633472.

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14

Navarro, Rodriguez Berta. "Plasma pre-treatment for adhesive bonding of aerospace composite components." Thesis, Brunel University, 2016. http://bura.brunel.ac.uk/handle/2438/14669.

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A cold atmospheric pressure plasma source was investigated as an alternative pre-treatment for carbon fibre reinforced epoxy substrates prior to bonding. For reference, common surface pre-treatments were also investigated (peel ply, manual abrasion, and grit blasting). In the aerospace industry, the peel ply, is usually added to one side of the composite surface during manufacture and peeled off prior to bonding. Peel ply can be used independently or in combination with other techniques. The strength of the bonded joints of the different pre-treatments was assessed through tensile lap shear te

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15

Kradinov, Vladimir Y. "Optimum design of bolted composite lap joints under mechanical and thermal loading." Diss., The University of Arizona, 2003. http://hdl.handle.net/10150/280296.

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A new approach is developed for the analysis and design of mechanically fastened composite lap joints under mechanical and thermal loading. Based on the combined complex potential and variational formulation, the solution method satisfies the equilibrium equations exactly while the boundary conditions are satisfied by minimizing the total potential. This approach is capable of modeling finite laminate planform dimensions, uniform and variable laminate thickness, laminate lay-up, interaction among bolts, bolt torque, bolt flexibility, bolt size, bolt-hole clearance and interference, insert dime

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16

Jolly, Prateek. "Lamb wave based active damage identification in adhesively bonded composite lap joints." Thesis, Mississippi State University, 2016. http://pqdtopen.proquest.com/#viewpdf?dispub=10100288.

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<p> Bonding composite structures using adhesives offers several advantages over mechanical fastening such as better flow stress, weight saving, improved fatigue resistance and the ability to join dissimilar structures. The hesitation to adopt adhesively bonded composite joints stems from the lack of knowledge regarding damage initiation and propagation mechanisms within the joint. A means of overcoming this hesitation is to continuously monitor damage in the joint. This study proposes a methodology to conduct structural health monitoring (SHM) of an adhesively bonded composite lap joint using

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17

Knapke, Robert D. "Unsteady Analysis of a Counter-Rotating Aspirated Compressor Using Phase-Lag and Non-Linear Harmonic Methods." University of Cincinnati / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1324409778.

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18

Chen, Yung-Yu. "A Multi-Physics Software Framework on Hybrid Parallel Computing for High-Fidelity Solutions of Conservation Laws." The Ohio State University, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=osu1313000975.

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19

Makiewicz, Kurt Timothy. "Development of Simultaneous Transformation Kinetics Microstructure Model with Application to Laser Metal Deposited Ti-6Al-4V and Alloy 718." The Ohio State University, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=osu1366023857.

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20

Langenbrunner, Nisrene A. "Understanding the Responses of a Metal and a CMCTurbine Blade during a Controlled Rub Event using a Segmented Shroud." The Ohio State University, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=osu1366191740.

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21

Reddy, Karunanidhi. "Aerospace law : the regulation of space activities and space exploration." Thesis, 1985. http://hdl.handle.net/10413/5220.

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22

Bardhan, Rajarshi. "Differential Games Guidance Laws for Aerospace Applications." Thesis, 2015. http://etd.iisc.ac.in/handle/2005/3889.

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This thesis addresses several aerospace guidance and decision making problems using both no cooperative and cooperative game theoretical solution concepts in the differential games framework. In the first part of the thesis, state dependent Riccati equation (SDRE) method has been extended to a zero-sum nonlinear differential games setting. This framework is used to study problems of intercepting a manoeuvring target, with and without terminal impact angle constraints, in the zero-sum differential games theory perspective. The guidance laws derived according to the proposed method are in closed

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23

Bardhan, Rajarshi. "Differential Games Guidance Laws for Aerospace Applications." Thesis, 2015. http://etd.iisc.ernet.in/2005/3889.

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This thesis addresses several aerospace guidance and decision making problems using both no cooperative and cooperative game theoretical solution concepts in the differential games framework. In the first part of the thesis, state dependent Riccati equation (SDRE) method has been extended to a zero-sum nonlinear differential games setting. This framework is used to study problems of intercepting a manoeuvring target, with and without terminal impact angle constraints, in the zero-sum differential games theory perspective. The guidance laws derived according to the proposed method are in closed

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24

Sheeba, P. S. "Optimal Resource Allocation In Lanchester Attrition Model Based Conflicts." Thesis, 2007. https://etd.iisc.ac.in/handle/2005/482.

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Force deployment and optimal resource allocation has been an area of considerable research interest in conventional warfare. In the modern scenario, with significant advances in technology related to communication and computation, sophisticated decision-making in these situations has become feasible. This has generated renewed interest in formulating decision-making problems in these areas and seeking optimal solutions to them. This thesis addresses one such problem in which the defending forces need to optimally Partition their resources between several attacking forces of differing strengths

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25

Sheeba, P. S. "Optimal Resource Allocation In Lanchester Attrition Model Based Conflicts." Thesis, 2007. http://hdl.handle.net/2005/482.

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Force deployment and optimal resource allocation has been an area of considerable research interest in conventional warfare. In the modern scenario, with significant advances in technology related to communication and computation, sophisticated decision-making in these situations has become feasible. This has generated renewed interest in formulating decision-making problems in these areas and seeking optimal solutions to them. This thesis addresses one such problem in which the defending forces need to optimally Partition their resources between several attacking forces of differing strengths

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26

Dhabale, Ashwin. "Impact Angle Constrained Guidance Using Cubic Splines." Thesis, 2015. http://etd.iisc.ac.in/handle/2005/3658.

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In this thesis the cubic spline guidance law and its variants are derived. A detailed analysis is carried out to find the initial conditions for successful interception. The results are applied to three dimensional guidance design and for solving waypoint following problems. The basic cubic spline guidance law is derived for intercepting a stationary target at a desired impact angle in a surface-to-surface engagement scenario. The guidance law is obtained using an inverse method, from a cubic spline curve based trajectory. For overcoming the drawbacks of the basic cubic spline guida

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27

Dhabale, Ashwin. "Impact Angle Constrained Guidance Using Cubic Splines." Thesis, 2015. http://etd.iisc.ernet.in/2005/3658.

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In this thesis the cubic spline guidance law and its variants are derived. A detailed analysis is carried out to find the initial conditions for successful interception. The results are applied to three dimensional guidance design and for solving waypoint following problems. The basic cubic spline guidance law is derived for intercepting a stationary target at a desired impact angle in a surface-to-surface engagement scenario. The guidance law is obtained using an inverse method, from a cubic spline curve based trajectory. For overcoming the drawbacks of the basic cubic spline guida

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28

Abdul, Saleem P. K. "Guidance Laws for Engagement Time Control." Thesis, 2016. http://etd.iisc.ac.in/handle/2005/2926.

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Autonomous aerial vehicles like missiles and unmanned aerial vehicles (UAVs) have attracted various military and civilian applications. The primary guidance objective of any autonomous vehicle is to reach the desired destination point (target or waypoint). However, many practical engagements impose additional constraints like minimum control effort, a desired final velocity direction or a predefined engagement time. This thesis addresses engagement time constrained guidance problems pertaining to missiles and UAVs. The first part of the thesis discusses a nonlinear guidance law for impact tim

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29

Abdul, Saleem P. K. "Guidance Laws for Engagement Time Control." Thesis, 2016. http://hdl.handle.net/2005/2926.

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Autonomous aerial vehicles like missiles and unmanned aerial vehicles (UAVs) have attracted various military and civilian applications. The primary guidance objective of any autonomous vehicle is to reach the desired destination point (target or waypoint). However, many practical engagements impose additional constraints like minimum control effort, a desired final velocity direction or a predefined engagement time. This thesis addresses engagement time constrained guidance problems pertaining to missiles and UAVs. The first part of the thesis discusses a nonlinear guidance law for impact tim

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30

(8698980), Zherui Guo. "Design optimization of multi-ply soft armor targets based on failure modes under projectile normal impact." Thesis, 2020.

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At the ballistic limit velocity of a soft armor target pack, the impact response has been shown to be decoupled in the thickness direction, with the initial few plies behaving in an inelastic fashion via off-axis failure modes such as transverse shear or diametral compression. Past the initial few layers, the remaining plies dissipate energy via membrane-like responses, which only involve in-plane tensile failure modes of the constituent fibers. Since these initial plies only contribute to energy absorption via inelastic kinetic energy transfer, previous studi

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31

(8741097), Ritwik Bandyopadhyay. "ENSURING FATIGUE PERFORMANCE VIA LOCATION-SPECIFIC LIFING IN AEROSPACE COMPONENTS MADE OF TITANIUM ALLOYS AND NICKEL-BASE SUPERALLOYS." Thesis, 2020.

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<div>In this thesis, the role of location-specific microstructural features in the fatigue performance of the safety-critical aerospace components made of Nickel (Ni)-base superalloys and linear friction welded (LFW) Titanium (Ti) alloys has been studied using crystal plasticity finite element (CPFE) simulations, energy dispersive X-ray diffraction (EDD), backscatter electron (BSE) images and digital image correlation (DIC).</div><div><br></div><div>In order to develop a microstructure-sensitive fatigue life prediction framework, first, it is essential to build trust in the quantitative predic

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32

Maruthi, N. H. "Hybird Central Solvers for Hyperbolic Conservation Laws." Thesis, 2015. http://etd.iisc.ac.in/handle/2005/3523.

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The hyperbolic conservation laws model the phenomena of nonlinear waves including discontinuities. The coupled nonlinear equations representing such conservation laws may lead to discontinuous solutions even for smooth initial data. To solve such equations, developing numerical methods which are accurate, robust, and resolve all the wave structures appearing in the solutions is a challenging task. Among several discretization techniques developed for solving hyperbolic conservation laws numerically, Finite Volume Method (FVM) is the most popular. Numerical algorithms, in the framework of FVM,

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33

Maruthi, N. H. "Hybird Central Solvers for Hyperbolic Conservation Laws." Thesis, 2015. http://etd.iisc.ernet.in/2005/3523.

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The hyperbolic conservation laws model the phenomena of nonlinear waves including discontinuities. The coupled nonlinear equations representing such conservation laws may lead to discontinuous solutions even for smooth initial data. To solve such equations, developing numerical methods which are accurate, robust, and resolve all the wave structures appearing in the solutions is a challenging task. Among several discretization techniques developed for solving hyperbolic conservation laws numerically, Finite Volume Method (FVM) is the most popular. Numerical algorithms, in the framework of FVM,

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34

Vijaya, Kumar R. L. "Some Experimental and Numerical Studies on Evaluation of Adhesive Bond Integrity of Composites Lap Shear Joints." Thesis, 2014. http://etd.iisc.ac.in/handle/2005/3220.

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Adhesive bonding which has been in use for long as a traditional joining method has gained ground in the last couple of decades due to the introduction of advanced composite materials into the aerospace industry. Bonded structures have advantages such as high corrosion and fatigue resistance, ability to join dissimilar materials, reduced stress concentration, uniform stress distribution, good damping characteristics etc. They also have certain limitations like environmental degradation, existence of defects like pores, voids and disbonds, difficulty in maintenance and repair etc. A serious dra

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35

Vijaya, Kumar R. L. "Some Experimental and Numerical Studies on Evaluation of Adhesive Bond Integrity of Composites Lap Shear Joints." Thesis, 2014. http://hdl.handle.net/2005/3220.

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Adhesive bonding which has been in use for long as a traditional joining method has gained ground in the last couple of decades due to the introduction of advanced composite materials into the aerospace industry. Bonded structures have advantages such as high corrosion and fatigue resistance, ability to join dissimilar materials, reduced stress concentration, uniform stress distribution, good damping characteristics etc. They also have certain limitations like environmental degradation, existence of defects like pores, voids and disbonds, difficulty in maintenance and repair etc. A serious dra

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36

(6641012), Genisson Silva Coutinho. "FACULTY BELIEFS AND ORIENTATIONS TO TEACHING AND LEARNING IN THE LAB: AN EXPLORATORY CASE STUDY." Thesis, 2019.

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<div>This dissertation presents a two-phase multiple case study conducted to investigate the faculty</div><div>beliefs regarding the integration of labs into engineering and engineering technology education</div><div>and the relationship between such beliefs and the teaching practices adopted in the labs. In the first</div><div>phase, an exploratory study grounded on a framework of beliefs was conducted to elicit the beliefs</div><div>espoused by the participants. Interviews were used to elicit the participants’ beliefs. The</div><div>transcribed interviews were analyzed through the constant c

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37

Mukherjee, Dwaipayan. "Cyclic Pursuit : Variants and Applications." Thesis, 2014. http://etd.iisc.ac.in/handle/2005/3089.

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The classical n-bugs problem has attracted considerable attention from researchers. This problem stems from the study of movement of a group of animals. In the context of multi- agent systems the problem has been modelled as cyclic pursuit. Under this paradigm, every agent, indexed i, chases its unique leader, agent i + 1 (modulo n), with n being the total number of agents. In the existing literature, cyclic pursuit has been studied for homogeneous agents where each agent’s velocity is proportional to the distance separating it from its leader and is directed along the line joining it to its l

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38

Mukherjee, Dwaipayan. "Cyclic Pursuit : Variants and Applications." Thesis, 2014. http://hdl.handle.net/2005/3089.

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The classical n-bugs problem has attracted considerable attention from researchers. This problem stems from the study of movement of a group of animals. In the context of multi- agent systems the problem has been modelled as cyclic pursuit. Under this paradigm, every agent, indexed i, chases its unique leader, agent i + 1 (modulo n), with n being the total number of agents. In the existing literature, cyclic pursuit has been studied for homogeneous agents where each agent’s velocity is proportional to the distance separating it from its leader and is directed along the line joining it to its l

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39

Kumar, Shashi Ranjan. "Sliding Mode Control Based Guidance Strategies with Terminal Constraints." Thesis, 2015. http://etd.iisc.ac.in/handle/2005/3876.

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In the guidance literature, minimizing miss distance along with optimizing the energy usage had been an objective for several decades. In current day applications, additional terminal performance such as impact angle and impact time are of paramount importance. These terminal constraints increase warhead effectiveness and survivability of the interceptor. This thesis contributes to the design of guidance laws addressing terminal constraints such as impact angle, impact time, and both impact time as well as impact angle, in addition to interception of targets. In the first part of the thesis,

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40

Kumar, Shashi Ranjan. "Sliding Mode Control Based Guidance Strategies with Terminal Constraints." Thesis, 2015. http://etd.iisc.ernet.in/2005/3876.

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In the guidance literature, minimizing miss distance along with optimizing the energy usage had been an objective for several decades. In current day applications, additional terminal performance such as impact angle and impact time are of paramount importance. These terminal constraints increase warhead effectiveness and survivability of the interceptor. This thesis contributes to the design of guidance laws addressing terminal constraints such as impact angle, impact time, and both impact time as well as impact angle, in addition to interception of targets. In the first part of the thesis,

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41

Saroj, Kumar G. "An Integrated Estimation-Guidance Approach for Seeker-less Interceptors." Thesis, 2015. http://etd.iisc.ac.in/handle/2005/3828.

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In this thesis, the problem of intercepting highly manoeuvrable threats using seeker-less interceptors that operate in the command guidance mode, is addressed. These systems are more prone to estimation errors than standard seeker-based systems. Several non-linear and optimal estimation and guidance concepts are presented in this thesis for interception of randomly maneuvering targets by seeker-less interceptors. The key contributions of the thesis can be broadly categorized into six groups, namely (i) an optimal selection of bank of lters in interactive multiple model (IMM) scheme to cater to

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42

Saroj, Kumar G. "An Integrated Estimation-Guidance Approach for Seeker-less Interceptors." Thesis, 2015. http://etd.iisc.ernet.in/2005/3828.

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In this thesis, the problem of intercepting highly manoeuvrable threats using seeker-less interceptors that operate in the command guidance mode, is addressed. These systems are more prone to estimation errors than standard seeker-based systems. Several non-linear and optimal estimation and guidance concepts are presented in this thesis for interception of randomly maneuvering targets by seeker-less interceptors. The key contributions of the thesis can be broadly categorized into six groups, namely (i) an optimal selection of bank of lters in interactive multiple model (IMM) scheme to cater to

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