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You searched for subject:(aircraft electrical system). Showing records 1 – 15 of 15 total matches.

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The Ohio State University

1. Alexander, Richard. Analysis of Aircraft Power Systems, Including System Modeling and Energy Optimization, with Predictions of Future Aircraft Development.

Degree: MS, Electrical and Computer Engineering, 2018, The Ohio State University

 The aviation industry has been one of the biggest beneficiaries of the major rise in electric power system technology for the past several decades. With… (more)

Subjects/Keywords: Electrical Engineering; All-Electric Aircraft; More Electric Aircraft; Electric Power System; Batteries

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APA (6th Edition):

Alexander, R. (2018). Analysis of Aircraft Power Systems, Including System Modeling and Energy Optimization, with Predictions of Future Aircraft Development. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1523541008209354

Chicago Manual of Style (16th Edition):

Alexander, Richard. “Analysis of Aircraft Power Systems, Including System Modeling and Energy Optimization, with Predictions of Future Aircraft Development.” 2018. Masters Thesis, The Ohio State University. Accessed October 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1523541008209354.

MLA Handbook (7th Edition):

Alexander, Richard. “Analysis of Aircraft Power Systems, Including System Modeling and Energy Optimization, with Predictions of Future Aircraft Development.” 2018. Web. 22 Oct 2019.

Vancouver:

Alexander R. Analysis of Aircraft Power Systems, Including System Modeling and Energy Optimization, with Predictions of Future Aircraft Development. [Internet] [Masters thesis]. The Ohio State University; 2018. [cited 2019 Oct 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1523541008209354.

Council of Science Editors:

Alexander R. Analysis of Aircraft Power Systems, Including System Modeling and Energy Optimization, with Predictions of Future Aircraft Development. [Masters Thesis]. The Ohio State University; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1523541008209354

2. Mak, Christopher. Modeling and simulation of commercial aircraft electrical systems.

Degree: MS, Electrical & Computer Engineering, 2015, University of Illinois – Urbana-Champaign

 In this thesis a modeling and simulation based methodology is proposed to study the general power flow and dynamics of commercial aircraft electrical systems. This… (more)

Subjects/Keywords: aircraft electrical system; modeling

…future work are discussed. 4 2 SYSTEM OVERVIEW 2.1 Aircraft Electrical System Overview The… …electrical system for a commercial aircraft is a complex mix of ac components and dc components… …an aircraft electrical system configuration for an aircraft. The generators convert… …intended to form a reliable and redundant system. The electrical system can be divided into four… …Electrical System Simulink Model Overview One of the goals in designing and developing this toolset… 

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APA (6th Edition):

Mak, C. (2015). Modeling and simulation of commercial aircraft electrical systems. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/88123

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Mak, Christopher. “Modeling and simulation of commercial aircraft electrical systems.” 2015. Thesis, University of Illinois – Urbana-Champaign. Accessed October 22, 2019. http://hdl.handle.net/2142/88123.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Mak, Christopher. “Modeling and simulation of commercial aircraft electrical systems.” 2015. Web. 22 Oct 2019.

Vancouver:

Mak C. Modeling and simulation of commercial aircraft electrical systems. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2015. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/2142/88123.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Mak C. Modeling and simulation of commercial aircraft electrical systems. [Thesis]. University of Illinois – Urbana-Champaign; 2015. Available from: http://hdl.handle.net/2142/88123

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Wright State University

3. Al-Agele, Saif. Electrical Power and Storage for NASA Next Generation Aircraft.

Degree: MSME, Mechanical Engineering, 2017, Wright State University

 Next generation aircraft will incorporate more electrical power generation and storage for both a distributed electric propulsion system and onboard subsystems. The power generation in… (more)

Subjects/Keywords: Aerospace Engineering; NASA next-generation aircraft; N3X; Electrical power generation; Turbo-generator system; Electric aircraft; Electrical distribution systems; Battery banks

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APA (6th Edition):

Al-Agele, S. (2017). Electrical Power and Storage for NASA Next Generation Aircraft. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1515632677356171

Chicago Manual of Style (16th Edition):

Al-Agele, Saif. “Electrical Power and Storage for NASA Next Generation Aircraft.” 2017. Masters Thesis, Wright State University. Accessed October 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=wright1515632677356171.

MLA Handbook (7th Edition):

Al-Agele, Saif. “Electrical Power and Storage for NASA Next Generation Aircraft.” 2017. Web. 22 Oct 2019.

Vancouver:

Al-Agele S. Electrical Power and Storage for NASA Next Generation Aircraft. [Internet] [Masters thesis]. Wright State University; 2017. [cited 2019 Oct 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1515632677356171.

Council of Science Editors:

Al-Agele S. Electrical Power and Storage for NASA Next Generation Aircraft. [Masters Thesis]. Wright State University; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1515632677356171

4. Beckman, Mathias. Performance Assessment of Electrical Motor for Electric Aircraft Propulsion Applications : Evaluation of the Permanent Magnet Motor and its Limitations in Aircraft Propulsion.

Degree: Society and Engineering, 2019, Mälardalen University

  This thesis project will evaluate which kind of electrical motor is best suited for aircraft propulsion and which parameters effect the efficiency. An economic… (more)

Subjects/Keywords: Electric Aircraft; Permanent Magnet Electrical Motor; Losses; Hybrid-Electric Propulsion System; Environment; Global Warming; Aircraft Emission; Energy Engineering; Energiteknik

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APA (6th Edition):

Beckman, M. (2019). Performance Assessment of Electrical Motor for Electric Aircraft Propulsion Applications : Evaluation of the Permanent Magnet Motor and its Limitations in Aircraft Propulsion. (Thesis). Mälardalen University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-45157

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Beckman, Mathias. “Performance Assessment of Electrical Motor for Electric Aircraft Propulsion Applications : Evaluation of the Permanent Magnet Motor and its Limitations in Aircraft Propulsion.” 2019. Thesis, Mälardalen University. Accessed October 22, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-45157.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Beckman, Mathias. “Performance Assessment of Electrical Motor for Electric Aircraft Propulsion Applications : Evaluation of the Permanent Magnet Motor and its Limitations in Aircraft Propulsion.” 2019. Web. 22 Oct 2019.

Vancouver:

Beckman M. Performance Assessment of Electrical Motor for Electric Aircraft Propulsion Applications : Evaluation of the Permanent Magnet Motor and its Limitations in Aircraft Propulsion. [Internet] [Thesis]. Mälardalen University; 2019. [cited 2019 Oct 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-45157.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Beckman M. Performance Assessment of Electrical Motor for Electric Aircraft Propulsion Applications : Evaluation of the Permanent Magnet Motor and its Limitations in Aircraft Propulsion. [Thesis]. Mälardalen University; 2019. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-45157

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of South Carolina

5. Young Lentijo, Kathleen Deborah. High-Fidelity Power Injection From A Fuel Cell Onto A Variable-Frequency AC Power Bus.

Degree: PhD, Electrical Engineering, 2009, University of South Carolina

  Synchronization of DC-source fed inverters to AC power systems is essential to the integration of DC sources such as fuel cells, batteries, and photovoltaics.… (more)

Subjects/Keywords: Electrical and Computer Engineering; Electrical and Electronics; Engineering; aircraft power system; fuel cell; microgrid; PLL; variable-frequency

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APA (6th Edition):

Young Lentijo, K. D. (2009). High-Fidelity Power Injection From A Fuel Cell Onto A Variable-Frequency AC Power Bus. (Doctoral Dissertation). University of South Carolina. Retrieved from https://scholarcommons.sc.edu/etd/116

Chicago Manual of Style (16th Edition):

Young Lentijo, Kathleen Deborah. “High-Fidelity Power Injection From A Fuel Cell Onto A Variable-Frequency AC Power Bus.” 2009. Doctoral Dissertation, University of South Carolina. Accessed October 22, 2019. https://scholarcommons.sc.edu/etd/116.

MLA Handbook (7th Edition):

Young Lentijo, Kathleen Deborah. “High-Fidelity Power Injection From A Fuel Cell Onto A Variable-Frequency AC Power Bus.” 2009. Web. 22 Oct 2019.

Vancouver:

Young Lentijo KD. High-Fidelity Power Injection From A Fuel Cell Onto A Variable-Frequency AC Power Bus. [Internet] [Doctoral dissertation]. University of South Carolina; 2009. [cited 2019 Oct 22]. Available from: https://scholarcommons.sc.edu/etd/116.

Council of Science Editors:

Young Lentijo KD. High-Fidelity Power Injection From A Fuel Cell Onto A Variable-Frequency AC Power Bus. [Doctoral Dissertation]. University of South Carolina; 2009. Available from: https://scholarcommons.sc.edu/etd/116


Portland State University

6. Kirkpatrick, Daniel Eugene. Design of a Hardware Platform for GPS-Based Orientation Sensing.

Degree: MS(M.S.) in Electrical and Computer Engineering, Electrical and Computer Engineering, 2015, Portland State University

  Unmanned aerial vehicles (UAV's) have recently gained popularity in military, civil service, agriculture, commercial, and hobby use. This is due in part to their… (more)

Subjects/Keywords: Global Positioning System; Drone aircraft  – Control systems  – Design and construction; Inertial navigation; Electrical and Computer Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Kirkpatrick, D. E. (2015). Design of a Hardware Platform for GPS-Based Orientation Sensing. (Masters Thesis). Portland State University. Retrieved from https://pdxscholar.library.pdx.edu/open_access_etds/2197

Chicago Manual of Style (16th Edition):

Kirkpatrick, Daniel Eugene. “Design of a Hardware Platform for GPS-Based Orientation Sensing.” 2015. Masters Thesis, Portland State University. Accessed October 22, 2019. https://pdxscholar.library.pdx.edu/open_access_etds/2197.

MLA Handbook (7th Edition):

Kirkpatrick, Daniel Eugene. “Design of a Hardware Platform for GPS-Based Orientation Sensing.” 2015. Web. 22 Oct 2019.

Vancouver:

Kirkpatrick DE. Design of a Hardware Platform for GPS-Based Orientation Sensing. [Internet] [Masters thesis]. Portland State University; 2015. [cited 2019 Oct 22]. Available from: https://pdxscholar.library.pdx.edu/open_access_etds/2197.

Council of Science Editors:

Kirkpatrick DE. Design of a Hardware Platform for GPS-Based Orientation Sensing. [Masters Thesis]. Portland State University; 2015. Available from: https://pdxscholar.library.pdx.edu/open_access_etds/2197


Ohio University

7. Duan, Pengfei. Predictive Alerting for Improved Aircraft State Awareness.

Degree: PhD, Electrical Engineering & Computer Science (Engineering and Technology), 2018, Ohio University

 The lack of aircraft state awareness has been one of the leading causal and contributing factors in aviation accidents. Many of these accidents were due… (more)

Subjects/Keywords: Engineering; Electrical Engineering; aviation safety; aircraft state awareness; multiple hypothesis prediction; VNAV; autopilot; state prediction; alerting system; HITL; avionics

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APA (6th Edition):

Duan, P. (2018). Predictive Alerting for Improved Aircraft State Awareness. (Doctoral Dissertation). Ohio University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1539871688328245

Chicago Manual of Style (16th Edition):

Duan, Pengfei. “Predictive Alerting for Improved Aircraft State Awareness.” 2018. Doctoral Dissertation, Ohio University. Accessed October 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1539871688328245.

MLA Handbook (7th Edition):

Duan, Pengfei. “Predictive Alerting for Improved Aircraft State Awareness.” 2018. Web. 22 Oct 2019.

Vancouver:

Duan P. Predictive Alerting for Improved Aircraft State Awareness. [Internet] [Doctoral dissertation]. Ohio University; 2018. [cited 2019 Oct 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1539871688328245.

Council of Science Editors:

Duan P. Predictive Alerting for Improved Aircraft State Awareness. [Doctoral Dissertation]. Ohio University; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1539871688328245


Brno University of Technology

8. Harasim, Tomáš. Návrh diagnostické soustavy pro malý dopravní letoun .

Degree: 2015, Brno University of Technology

 Díky tlaku leteckých společností a provozovatelů letadel na snížení provozních nákladů, jsou do systémů letadel intalovány diagnostické soustavy, kterými lze sledovat opotřebení jednotlivých funkčních prvků.… (more)

Subjects/Keywords: Diagnostická soustava; hydraulická soustava; elektrická soustava; palivová soustava; motorová soustava; výběr kritických prvků; diagnostické parametry; měření; snímání; prediktivní kvalitativní analýza; letadlo; Diagnostic system; hyraulic system; electrical system; fuel system; engine system; selection of critical elements; diagnostic parameters; measurement; sensing; reading; predictive qualitative analysis; aircraft

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APA (6th Edition):

Harasim, T. (2015). Návrh diagnostické soustavy pro malý dopravní letoun . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/39248

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Harasim, Tomáš. “Návrh diagnostické soustavy pro malý dopravní letoun .” 2015. Thesis, Brno University of Technology. Accessed October 22, 2019. http://hdl.handle.net/11012/39248.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Harasim, Tomáš. “Návrh diagnostické soustavy pro malý dopravní letoun .” 2015. Web. 22 Oct 2019.

Vancouver:

Harasim T. Návrh diagnostické soustavy pro malý dopravní letoun . [Internet] [Thesis]. Brno University of Technology; 2015. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/11012/39248.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Harasim T. Návrh diagnostické soustavy pro malý dopravní letoun . [Thesis]. Brno University of Technology; 2015. Available from: http://hdl.handle.net/11012/39248

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

9. Hadbi, Djamel. Formulations de problèmes d’optimisation multiniveaux pour la conception de réseaux de bord électriques en aéronautique : Multilevel optimization problem setting for the design of electric aircraft networks.

Degree: Docteur es, Génie électrique, 2015, Grenoble Alpes

Dans le contexte de l’avion plus électrique, les réseaux électriques aéronautiques sont en pleine évolution. Cette évolution est poussée par le besoin d’une intégration à… (more)

Subjects/Keywords: Formulation de problèmes d'optimisation; Avion plus électrique; Optimisation multiniveau; Qualité de l'énergie; Réseaux électriques embarqués; Optimization problem setting; More electric aircraft; Multilevel optimization; Power quality; Embedded electrical system; 620

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APA (6th Edition):

Hadbi, D. (2015). Formulations de problèmes d’optimisation multiniveaux pour la conception de réseaux de bord électriques en aéronautique : Multilevel optimization problem setting for the design of electric aircraft networks. (Doctoral Dissertation). Grenoble Alpes. Retrieved from http://www.theses.fr/2015GREAT115

Chicago Manual of Style (16th Edition):

Hadbi, Djamel. “Formulations de problèmes d’optimisation multiniveaux pour la conception de réseaux de bord électriques en aéronautique : Multilevel optimization problem setting for the design of electric aircraft networks.” 2015. Doctoral Dissertation, Grenoble Alpes. Accessed October 22, 2019. http://www.theses.fr/2015GREAT115.

MLA Handbook (7th Edition):

Hadbi, Djamel. “Formulations de problèmes d’optimisation multiniveaux pour la conception de réseaux de bord électriques en aéronautique : Multilevel optimization problem setting for the design of electric aircraft networks.” 2015. Web. 22 Oct 2019.

Vancouver:

Hadbi D. Formulations de problèmes d’optimisation multiniveaux pour la conception de réseaux de bord électriques en aéronautique : Multilevel optimization problem setting for the design of electric aircraft networks. [Internet] [Doctoral dissertation]. Grenoble Alpes; 2015. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2015GREAT115.

Council of Science Editors:

Hadbi D. Formulations de problèmes d’optimisation multiniveaux pour la conception de réseaux de bord électriques en aéronautique : Multilevel optimization problem setting for the design of electric aircraft networks. [Doctoral Dissertation]. Grenoble Alpes; 2015. Available from: http://www.theses.fr/2015GREAT115

10. Majewski, Łukasz. Integration and assessment of a dual core chip - Atmel’s DIOPSIS 940 - for a flight control system.

Degree: 2009, , Department of Computer and Information Science

  A dual core Atmel DIOPSIS 940 chip consists of a DSP and an ARM9 functional units in a single silicon die. This thesis presents… (more)

Subjects/Keywords: Unmanned Aircraft System; UAS; Flight Control System; DSP; mAgicV; ARM9; Real-Time Linux; AT572D940HF; DIOPSIS; Kalman filter; Other Electrical Engineering, Electronic Engineering, Information Engineering; Annan elektroteknik och elektronik; Software Engineering; Programvaruteknik

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APA (6th Edition):

Majewski, . (2009). Integration and assessment of a dual core chip - Atmel’s DIOPSIS 940 - for a flight control system. (Thesis). , Department of Computer and Information Science. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-20022

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Majewski, Łukasz. “Integration and assessment of a dual core chip - Atmel’s DIOPSIS 940 - for a flight control system.” 2009. Thesis, , Department of Computer and Information Science. Accessed October 22, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-20022.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Majewski, Łukasz. “Integration and assessment of a dual core chip - Atmel’s DIOPSIS 940 - for a flight control system.” 2009. Web. 22 Oct 2019.

Vancouver:

Majewski . Integration and assessment of a dual core chip - Atmel’s DIOPSIS 940 - for a flight control system. [Internet] [Thesis]. , Department of Computer and Information Science; 2009. [cited 2019 Oct 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-20022.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Majewski . Integration and assessment of a dual core chip - Atmel’s DIOPSIS 940 - for a flight control system. [Thesis]. , Department of Computer and Information Science; 2009. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-20022

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

11. Reysset, Aurelien. Conception préliminaire d'actionneurs électromécaniques - outils d'aide à la spécification et à la génération de procédures de dimensionnement pour l'optimisation : Preliminary design of electromechanical actuators – development of tools dedicated to technical specification and optimal sizing sequence conditioning.

Degree: Docteur es, Génie Mécanique, Mécanique des Matériaux, 2015, Toulouse, INSA

Cette thèse a pour objectif d’apporter un ensemble d’outils logiciels s’inscrivant dans une méthodologie globale de conception de systèmes mécatroniques. Elle arrive en complément de… (more)

Subjects/Keywords: Avion plus électrique; Profils de mission; Conception optimale; Méta-modèles; Ordonnancement calcul; Modélisation multi-physique; Théorie des graphes; Spécification système; Actionneurs électromécanique; More-electrical aircraft (MEA); Electromechanical actuator (EMA); System specification; Mission profiles; Optimal design; Meta-models; Calculation sequence conditioning; Multi-physics simulation; Graph theory; 629.8

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APA (6th Edition):

Reysset, A. (2015). Conception préliminaire d'actionneurs électromécaniques - outils d'aide à la spécification et à la génération de procédures de dimensionnement pour l'optimisation : Preliminary design of electromechanical actuators – development of tools dedicated to technical specification and optimal sizing sequence conditioning. (Doctoral Dissertation). Toulouse, INSA. Retrieved from http://www.theses.fr/2015ISAT0003

Chicago Manual of Style (16th Edition):

Reysset, Aurelien. “Conception préliminaire d'actionneurs électromécaniques - outils d'aide à la spécification et à la génération de procédures de dimensionnement pour l'optimisation : Preliminary design of electromechanical actuators – development of tools dedicated to technical specification and optimal sizing sequence conditioning.” 2015. Doctoral Dissertation, Toulouse, INSA. Accessed October 22, 2019. http://www.theses.fr/2015ISAT0003.

MLA Handbook (7th Edition):

Reysset, Aurelien. “Conception préliminaire d'actionneurs électromécaniques - outils d'aide à la spécification et à la génération de procédures de dimensionnement pour l'optimisation : Preliminary design of electromechanical actuators – development of tools dedicated to technical specification and optimal sizing sequence conditioning.” 2015. Web. 22 Oct 2019.

Vancouver:

Reysset A. Conception préliminaire d'actionneurs électromécaniques - outils d'aide à la spécification et à la génération de procédures de dimensionnement pour l'optimisation : Preliminary design of electromechanical actuators – development of tools dedicated to technical specification and optimal sizing sequence conditioning. [Internet] [Doctoral dissertation]. Toulouse, INSA; 2015. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2015ISAT0003.

Council of Science Editors:

Reysset A. Conception préliminaire d'actionneurs électromécaniques - outils d'aide à la spécification et à la génération de procédures de dimensionnement pour l'optimisation : Preliminary design of electromechanical actuators – development of tools dedicated to technical specification and optimal sizing sequence conditioning. [Doctoral Dissertation]. Toulouse, INSA; 2015. Available from: http://www.theses.fr/2015ISAT0003

12. Giraud, Xavier. Méthodes et outils pour la conception optimale des réseaux de distribution d'électricité dans les aéronefs : Methods and tools for the optimal design of aircraft electrical power systems.

Degree: Docteur es, Systèmes Embarqués, 2014, Toulouse, INSA

 Dans le domaine aéronautique, la dernière décennie a été marquée par une augmentation constante et progressive du taux d’électrification des systèmes embarqués. L’avion plus électrique… (more)

Subjects/Keywords: Avion plus électrique; Conception optimale d’architecture; Électronique de puissance; Optimisation combinatoire; Recherche opérationnelle; Reconfiguration de réseau; Système expert; Modélisation multi-physique; Théorie des graphes; Approche système; Combinatorial optimization; Graph theory; Expert system; More electrical aircraft; Operational research; Optimal architecture design; Multi-physical modelling; Network reconfiguration; Power electronics; System approach; 629

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APA (6th Edition):

Giraud, X. (2014). Méthodes et outils pour la conception optimale des réseaux de distribution d'électricité dans les aéronefs : Methods and tools for the optimal design of aircraft electrical power systems. (Doctoral Dissertation). Toulouse, INSA. Retrieved from http://www.theses.fr/2014ISAT0004

Chicago Manual of Style (16th Edition):

Giraud, Xavier. “Méthodes et outils pour la conception optimale des réseaux de distribution d'électricité dans les aéronefs : Methods and tools for the optimal design of aircraft electrical power systems.” 2014. Doctoral Dissertation, Toulouse, INSA. Accessed October 22, 2019. http://www.theses.fr/2014ISAT0004.

MLA Handbook (7th Edition):

Giraud, Xavier. “Méthodes et outils pour la conception optimale des réseaux de distribution d'électricité dans les aéronefs : Methods and tools for the optimal design of aircraft electrical power systems.” 2014. Web. 22 Oct 2019.

Vancouver:

Giraud X. Méthodes et outils pour la conception optimale des réseaux de distribution d'électricité dans les aéronefs : Methods and tools for the optimal design of aircraft electrical power systems. [Internet] [Doctoral dissertation]. Toulouse, INSA; 2014. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2014ISAT0004.

Council of Science Editors:

Giraud X. Méthodes et outils pour la conception optimale des réseaux de distribution d'électricité dans les aéronefs : Methods and tools for the optimal design of aircraft electrical power systems. [Doctoral Dissertation]. Toulouse, INSA; 2014. Available from: http://www.theses.fr/2014ISAT0004

13. Bradley, Cullen Philip. LADAR: A Mono-static System for Sense and Avoid Applications.

Degree: MS(M.S.), Electro-Optics, 2013, University of Dayton

 In this thesis we study a laser radar, aka LADAR, system design to be mounted in an Unmanned Aircraft Systems (UAS) to prevent collisions with… (more)

Subjects/Keywords: Electrical Engineering; Optics; LADAR; Sense and Avoid; Mono-static System; Unmanned Aircraft Systems (UAS); Laser Range and Detection

…flying an Unmanned Aircraft System (UAS) in commercial airspace is the lack of… …intruder aircraft, and the LADAR system which receives laser pulse returns from the much smaller… …and perform accurately. The LADAR system will be tracking other 6 aircraft and so it’s… …45 WHOLE SYSTEM TESTING… …45 3.2 Mono‐static LADAR System… 

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APA (6th Edition):

Bradley, C. P. (2013). LADAR: A Mono-static System for Sense and Avoid Applications. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1366631049

Chicago Manual of Style (16th Edition):

Bradley, Cullen Philip. “LADAR: A Mono-static System for Sense and Avoid Applications.” 2013. Masters Thesis, University of Dayton. Accessed October 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1366631049.

MLA Handbook (7th Edition):

Bradley, Cullen Philip. “LADAR: A Mono-static System for Sense and Avoid Applications.” 2013. Web. 22 Oct 2019.

Vancouver:

Bradley CP. LADAR: A Mono-static System for Sense and Avoid Applications. [Internet] [Masters thesis]. University of Dayton; 2013. [cited 2019 Oct 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1366631049.

Council of Science Editors:

Bradley CP. LADAR: A Mono-static System for Sense and Avoid Applications. [Masters Thesis]. University of Dayton; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1366631049

14. Deric, Sanjin. Increased Capacity for VDL Mode 2 Aeronautical Data Communication.

Degree: MSin Electrical Engineering, Fenn College of Engineering, 2013, Cleveland State University

 VDL Mode 2 is the principal data communication technology for aeronautical communications implemented in the NextGen project for the National Airspace System (NAS), with potentially… (more)

Subjects/Keywords: Aerospace Engineering; Electrical Engineering; Engineering; Technical Communication; VDL Mode 2; VDL2; VDL M2; aeronautical communication; frequency reuse; capacity; frequency planning; NextGen; Data Comm; OPNET; Simulation; co-channel interference; aircraft; FAA; NAS; National Airspace System

…communication system capable of handling a larger load of data and aircraft. The three key NextGen… …communication capabilities in 2012. Dual stack aircraft have both Future Air Navigation System (… …47 viii NOMENCLATURE Acronym Definition ACARS Aircraft Communications Addressing and… …Reporting System ADS-B Automatic Dependent Surveillance-Broadcast AMCP Aeronautical Mobile… …Electronic Flight Instrument System FAA Federal Aviation Administration FANS Future Air… 

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APA (6th Edition):

Deric, S. (2013). Increased Capacity for VDL Mode 2 Aeronautical Data Communication. (Masters Thesis). Cleveland State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=csu1376063529

Chicago Manual of Style (16th Edition):

Deric, Sanjin. “Increased Capacity for VDL Mode 2 Aeronautical Data Communication.” 2013. Masters Thesis, Cleveland State University. Accessed October 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=csu1376063529.

MLA Handbook (7th Edition):

Deric, Sanjin. “Increased Capacity for VDL Mode 2 Aeronautical Data Communication.” 2013. Web. 22 Oct 2019.

Vancouver:

Deric S. Increased Capacity for VDL Mode 2 Aeronautical Data Communication. [Internet] [Masters thesis]. Cleveland State University; 2013. [cited 2019 Oct 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=csu1376063529.

Council of Science Editors:

Deric S. Increased Capacity for VDL Mode 2 Aeronautical Data Communication. [Masters Thesis]. Cleveland State University; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=csu1376063529

15. Sahawneh, Laith Rasmi. Airborne Collision Detection and Avoidance for Small UAS Sense and Avoid Systems.

Degree: PhD, 2016, Brigham Young University

  The increasing demand to integrate unmanned aircraft systems (UAS) into the national airspace is motivated by the rapid growth of the UAS industry, especially… (more)

Subjects/Keywords: unmanned aircraft system; small UAS; sense and avoid; minimum sensing range; airborne collision detection and avoidance; collision detection; collision risk assessment; collision avoidance; conflict detection; conflict avoidance; path planning; Electrical and Computer Engineering

…collisions. Not every aircraft that is observed by the sensing system, however, presents a conflict… …Additionally, a collision avoidance system should only maneuver to avoid other aircraft when a… …ownship unmanned aircraft block in this work refers to a generic system architecture of an… …analysis of multiple components of an aircraft alerting system, however we focus on the collision… …and mandated cooperative collision avoidance system and is used by many manned aircraft with… 

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APA (6th Edition):

Sahawneh, L. R. (2016). Airborne Collision Detection and Avoidance for Small UAS Sense and Avoid Systems. (Doctoral Dissertation). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6839&context=etd

Chicago Manual of Style (16th Edition):

Sahawneh, Laith Rasmi. “Airborne Collision Detection and Avoidance for Small UAS Sense and Avoid Systems.” 2016. Doctoral Dissertation, Brigham Young University. Accessed October 22, 2019. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6839&context=etd.

MLA Handbook (7th Edition):

Sahawneh, Laith Rasmi. “Airborne Collision Detection and Avoidance for Small UAS Sense and Avoid Systems.” 2016. Web. 22 Oct 2019.

Vancouver:

Sahawneh LR. Airborne Collision Detection and Avoidance for Small UAS Sense and Avoid Systems. [Internet] [Doctoral dissertation]. Brigham Young University; 2016. [cited 2019 Oct 22]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6839&context=etd.

Council of Science Editors:

Sahawneh LR. Airborne Collision Detection and Avoidance for Small UAS Sense and Avoid Systems. [Doctoral Dissertation]. Brigham Young University; 2016. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6839&context=etd

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