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You searched for subject:(Space Vehicles). Showing records 1 – 30 of 300 total matches.

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Embry-Riddle Aeronautical University

1. Kaur, Jasleen. Behavioral Motivation of Prospective Mars’ Crewmembers.

Degree: MSin Aeronautics, College of Aviation, 2018, Embry-Riddle Aeronautical University

  Living in extreme climatic conditions is challenging on planet Earth which encourages researchers hoping to find life on other planets such as Mars. This… (more)

Subjects/Keywords: Aeronautical Vehicles; Aviation; Space Vehicles

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APA (6th Edition):

Kaur, J. (2018). Behavioral Motivation of Prospective Mars’ Crewmembers. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/437

Chicago Manual of Style (16th Edition):

Kaur, Jasleen. “Behavioral Motivation of Prospective Mars’ Crewmembers.” 2018. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/437.

MLA Handbook (7th Edition):

Kaur, Jasleen. “Behavioral Motivation of Prospective Mars’ Crewmembers.” 2018. Web. 09 Apr 2020.

Vancouver:

Kaur J. Behavioral Motivation of Prospective Mars’ Crewmembers. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/437.

Council of Science Editors:

Kaur J. Behavioral Motivation of Prospective Mars’ Crewmembers. [Masters Thesis]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/437


Embry-Riddle Aeronautical University

2. Smith, Casey L. The Effects of Familiarity and Persuasion on Risk Assessment.

Degree: MSin Human Factors & Systems, Human Factors and Systems, 2012, Embry-Riddle Aeronautical University

  Cognitive biases influence decisions and the analyses of risk. They are often derived from two separate processes: bias based on familiarity (familiarity bias) and… (more)

Subjects/Keywords: Psychology; Space Vehicles

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APA (6th Edition):

Smith, C. L. (2012). The Effects of Familiarity and Persuasion on Risk Assessment. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/131

Chicago Manual of Style (16th Edition):

Smith, Casey L. “The Effects of Familiarity and Persuasion on Risk Assessment.” 2012. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/131.

MLA Handbook (7th Edition):

Smith, Casey L. “The Effects of Familiarity and Persuasion on Risk Assessment.” 2012. Web. 09 Apr 2020.

Vancouver:

Smith CL. The Effects of Familiarity and Persuasion on Risk Assessment. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2012. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/131.

Council of Science Editors:

Smith CL. The Effects of Familiarity and Persuasion on Risk Assessment. [Masters Thesis]. Embry-Riddle Aeronautical University; 2012. Available from: https://commons.erau.edu/edt/131


Embry-Riddle Aeronautical University

3. Scheppa, Michael D. Preliminary Design of an Asteroid Hopping Mission.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2011, Embry-Riddle Aeronautical University

  In 2010, NASA announced that its new vision is to support private space launch operations. It is anticipated that this new direction will create… (more)

Subjects/Keywords: Aeronautical Vehicles; Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Scheppa, M. D. (2011). Preliminary Design of an Asteroid Hopping Mission. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/122

Chicago Manual of Style (16th Edition):

Scheppa, Michael D. “Preliminary Design of an Asteroid Hopping Mission.” 2011. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/122.

MLA Handbook (7th Edition):

Scheppa, Michael D. “Preliminary Design of an Asteroid Hopping Mission.” 2011. Web. 09 Apr 2020.

Vancouver:

Scheppa MD. Preliminary Design of an Asteroid Hopping Mission. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2011. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/122.

Council of Science Editors:

Scheppa MD. Preliminary Design of an Asteroid Hopping Mission. [Masters Thesis]. Embry-Riddle Aeronautical University; 2011. Available from: https://commons.erau.edu/edt/122


Embry-Riddle Aeronautical University

4. Plishka, Stephen N. An Experimental Investigation of Direct and Indirect Viewing of a Remote Manipulation.

Degree: MSin Human Factors & Systems, Human Factors and Systems, 2002, Embry-Riddle Aeronautical University

  The purpose of this study was to evaluate direct and indirect viewing of a remote manipulation. With continued exploration of inner and outer space,… (more)

Subjects/Keywords: Space Vehicles

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APA (6th Edition):

Plishka, S. N. (2002). An Experimental Investigation of Direct and Indirect Viewing of a Remote Manipulation. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/168

Chicago Manual of Style (16th Edition):

Plishka, Stephen N. “An Experimental Investigation of Direct and Indirect Viewing of a Remote Manipulation.” 2002. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/db-theses/168.

MLA Handbook (7th Edition):

Plishka, Stephen N. “An Experimental Investigation of Direct and Indirect Viewing of a Remote Manipulation.” 2002. Web. 09 Apr 2020.

Vancouver:

Plishka SN. An Experimental Investigation of Direct and Indirect Viewing of a Remote Manipulation. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2002. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/db-theses/168.

Council of Science Editors:

Plishka SN. An Experimental Investigation of Direct and Indirect Viewing of a Remote Manipulation. [Masters Thesis]. Embry-Riddle Aeronautical University; 2002. Available from: https://commons.erau.edu/db-theses/168


Embry-Riddle Aeronautical University

5. Scholz, Curtis. Modeling and Simulation of Radiation from Electronic Transitions in Hypersonic Atmospheric Reentry Flow.

Degree: MSin Aerospace Engineering, Graduate Studies, 2015, Embry-Riddle Aeronautical University

  A capability for higher accuracy heat transfer modeling in CFD for hypersonic re-entry flows, via inclusion of thermal radiation, is sought. With temperatures reaching… (more)

Subjects/Keywords: Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Scholz, C. (2015). Modeling and Simulation of Radiation from Electronic Transitions in Hypersonic Atmospheric Reentry Flow. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/245

Chicago Manual of Style (16th Edition):

Scholz, Curtis. “Modeling and Simulation of Radiation from Electronic Transitions in Hypersonic Atmospheric Reentry Flow.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/245.

MLA Handbook (7th Edition):

Scholz, Curtis. “Modeling and Simulation of Radiation from Electronic Transitions in Hypersonic Atmospheric Reentry Flow.” 2015. Web. 09 Apr 2020.

Vancouver:

Scholz C. Modeling and Simulation of Radiation from Electronic Transitions in Hypersonic Atmospheric Reentry Flow. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/245.

Council of Science Editors:

Scholz C. Modeling and Simulation of Radiation from Electronic Transitions in Hypersonic Atmospheric Reentry Flow. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: https://commons.erau.edu/edt/245


Embry-Riddle Aeronautical University

6. Brandt, Margarita Nataly. Supersonic Retro-Propulsion Computational Fluid Dynamics Analysis Applied to Future Mars Mission.

Degree: MSin Mechanical Engineering, Mechanical Engineering, 2015, Embry-Riddle Aeronautical University

  Supersonic Retro-Propulsion is one of the most promising emerging technologies being considered by NASA for use in future Mars missions. This new form of… (more)

Subjects/Keywords: Mechanical Engineering; Space Vehicles

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APA (6th Edition):

Brandt, M. N. (2015). Supersonic Retro-Propulsion Computational Fluid Dynamics Analysis Applied to Future Mars Mission. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/263

Chicago Manual of Style (16th Edition):

Brandt, Margarita Nataly. “Supersonic Retro-Propulsion Computational Fluid Dynamics Analysis Applied to Future Mars Mission.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/263.

MLA Handbook (7th Edition):

Brandt, Margarita Nataly. “Supersonic Retro-Propulsion Computational Fluid Dynamics Analysis Applied to Future Mars Mission.” 2015. Web. 09 Apr 2020.

Vancouver:

Brandt MN. Supersonic Retro-Propulsion Computational Fluid Dynamics Analysis Applied to Future Mars Mission. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/263.

Council of Science Editors:

Brandt MN. Supersonic Retro-Propulsion Computational Fluid Dynamics Analysis Applied to Future Mars Mission. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: https://commons.erau.edu/edt/263


Embry-Riddle Aeronautical University

7. Albarran, Robert M., II. Cubesat Wakes in the Earth’s Ionosphere.

Degree: MSin Engineering Physics, Physical Sciences, 2015, Embry-Riddle Aeronautical University

Space exploration is currently being revolutionized by the advent of the CubeSat: 10cm cubed satellites that typically deploy in constellations for less than $100,000.… (more)

Subjects/Keywords: Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Albarran, Robert M., I. (2015). Cubesat Wakes in the Earth’s Ionosphere. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/57

Chicago Manual of Style (16th Edition):

Albarran, Robert M., II. “Cubesat Wakes in the Earth’s Ionosphere.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/57.

MLA Handbook (7th Edition):

Albarran, Robert M., II. “Cubesat Wakes in the Earth’s Ionosphere.” 2015. Web. 09 Apr 2020.

Vancouver:

Albarran, Robert M. I. Cubesat Wakes in the Earth’s Ionosphere. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/57.

Council of Science Editors:

Albarran, Robert M. I. Cubesat Wakes in the Earth’s Ionosphere. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: https://commons.erau.edu/edt/57


Embry-Riddle Aeronautical University

8. Waelchli, Robert. A Novel Magnetorheological Fluid Damper for a Small Spacecraft with Flexible Appendages.

Degree: MSin Mechanical Engineering, Mechanical Engineering, 2018, Embry-Riddle Aeronautical University

  Small satellites have become increasingly popular over the past thirty years, particularly since the adoption of the common CubeSat architecture early this century. Because… (more)

Subjects/Keywords: Space Vehicles; Structures and Materials

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APA (6th Edition):

Waelchli, R. (2018). A Novel Magnetorheological Fluid Damper for a Small Spacecraft with Flexible Appendages. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/391

Chicago Manual of Style (16th Edition):

Waelchli, Robert. “A Novel Magnetorheological Fluid Damper for a Small Spacecraft with Flexible Appendages.” 2018. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/391.

MLA Handbook (7th Edition):

Waelchli, Robert. “A Novel Magnetorheological Fluid Damper for a Small Spacecraft with Flexible Appendages.” 2018. Web. 09 Apr 2020.

Vancouver:

Waelchli R. A Novel Magnetorheological Fluid Damper for a Small Spacecraft with Flexible Appendages. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/391.

Council of Science Editors:

Waelchli R. A Novel Magnetorheological Fluid Damper for a Small Spacecraft with Flexible Appendages. [Masters Thesis]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/391


Embry-Riddle Aeronautical University

9. Rivera, Karina. Design and Implementation of Intelligent Guidance Algorithms for UAV Mission Protection.

Degree: MSin Aerospace Engineering, Graduate Studies, 2018, Embry-Riddle Aeronautical University

  In recent years, the interest of investigating intelligent systems for Unmanned Aerial Vehicles (UAVs) have increased in popularity due to their large range of… (more)

Subjects/Keywords: Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Rivera, K. (2018). Design and Implementation of Intelligent Guidance Algorithms for UAV Mission Protection. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/433

Chicago Manual of Style (16th Edition):

Rivera, Karina. “Design and Implementation of Intelligent Guidance Algorithms for UAV Mission Protection.” 2018. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/433.

MLA Handbook (7th Edition):

Rivera, Karina. “Design and Implementation of Intelligent Guidance Algorithms for UAV Mission Protection.” 2018. Web. 09 Apr 2020.

Vancouver:

Rivera K. Design and Implementation of Intelligent Guidance Algorithms for UAV Mission Protection. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/433.

Council of Science Editors:

Rivera K. Design and Implementation of Intelligent Guidance Algorithms for UAV Mission Protection. [Masters Thesis]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/433


Embry-Riddle Aeronautical University

10. Kazarin, Petr. Variable Fidelity Studies in Wake Vortex Evolution, Safety, and Control.

Degree: PhD, College of Engineering, 2018, Embry-Riddle Aeronautical University

  The purpose of this research is to develop a variable-fidelity approach for addressing the safety of unmanned aerial system (UAS) operations in the national… (more)

Subjects/Keywords: Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Kazarin, P. (2018). Variable Fidelity Studies in Wake Vortex Evolution, Safety, and Control. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/429

Chicago Manual of Style (16th Edition):

Kazarin, Petr. “Variable Fidelity Studies in Wake Vortex Evolution, Safety, and Control.” 2018. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/429.

MLA Handbook (7th Edition):

Kazarin, Petr. “Variable Fidelity Studies in Wake Vortex Evolution, Safety, and Control.” 2018. Web. 09 Apr 2020.

Vancouver:

Kazarin P. Variable Fidelity Studies in Wake Vortex Evolution, Safety, and Control. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/429.

Council of Science Editors:

Kazarin P. Variable Fidelity Studies in Wake Vortex Evolution, Safety, and Control. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/429


Embry-Riddle Aeronautical University

11. Prabhakar, Nirmit. Direct Adaptive Control for a Trajectory Tracking UAV.

Degree: PhD, College of Engineering, 2018, Embry-Riddle Aeronautical University

  This research focuses on the theoretical development and analysis of a direct adaptive control algorithm to enable a fixed-wing UAV to track reference trajectories… (more)

Subjects/Keywords: Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Prabhakar, N. (2018). Direct Adaptive Control for a Trajectory Tracking UAV. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/431

Chicago Manual of Style (16th Edition):

Prabhakar, Nirmit. “Direct Adaptive Control for a Trajectory Tracking UAV.” 2018. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/431.

MLA Handbook (7th Edition):

Prabhakar, Nirmit. “Direct Adaptive Control for a Trajectory Tracking UAV.” 2018. Web. 09 Apr 2020.

Vancouver:

Prabhakar N. Direct Adaptive Control for a Trajectory Tracking UAV. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/431.

Council of Science Editors:

Prabhakar N. Direct Adaptive Control for a Trajectory Tracking UAV. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/431


Embry-Riddle Aeronautical University

12. Coulter, Nolan. Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics.

Degree: MSin Aerospace Engineering, Graduate Studies, 2018, Embry-Riddle Aeronautical University

  The presence of propellant slosh dynamics in a spacecraft system during a maneuver leads to attitude control system (ACS) performance degradation resulting in attitude… (more)

Subjects/Keywords: Aerospace Engineering; Astrodynamics; Space Vehicles

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APA (6th Edition):

Coulter, N. (2018). Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/424

Chicago Manual of Style (16th Edition):

Coulter, Nolan. “Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics.” 2018. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/424.

MLA Handbook (7th Edition):

Coulter, Nolan. “Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics.” 2018. Web. 09 Apr 2020.

Vancouver:

Coulter N. Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/424.

Council of Science Editors:

Coulter N. Design of an Attitude Control System for a Spacecraft with Propellant Slosh Dynamics. [Masters Thesis]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/424


University of Central Florida

13. Vazquez, Christian. The Effect of Martensite-Fractions Assumptions In Shape Memory Alloy Springs.

Degree: 2018, University of Central Florida

 This research addresses various models of a spring-mass system that uses a spring made of a shape memory alloy (SMA). The system model describes the… (more)

Subjects/Keywords: Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Vazquez, C. (2018). The Effect of Martensite-Fractions Assumptions In Shape Memory Alloy Springs. (Masters Thesis). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/6203

Chicago Manual of Style (16th Edition):

Vazquez, Christian. “The Effect of Martensite-Fractions Assumptions In Shape Memory Alloy Springs.” 2018. Masters Thesis, University of Central Florida. Accessed April 09, 2020. https://stars.library.ucf.edu/etd/6203.

MLA Handbook (7th Edition):

Vazquez, Christian. “The Effect of Martensite-Fractions Assumptions In Shape Memory Alloy Springs.” 2018. Web. 09 Apr 2020.

Vancouver:

Vazquez C. The Effect of Martensite-Fractions Assumptions In Shape Memory Alloy Springs. [Internet] [Masters thesis]. University of Central Florida; 2018. [cited 2020 Apr 09]. Available from: https://stars.library.ucf.edu/etd/6203.

Council of Science Editors:

Vazquez C. The Effect of Martensite-Fractions Assumptions In Shape Memory Alloy Springs. [Masters Thesis]. University of Central Florida; 2018. Available from: https://stars.library.ucf.edu/etd/6203


University of Central Florida

14. Jahan, Sanjida. Characterization of mechanical properties in nanoparticle reinforced hybrid carbon fiber composites using photoluminescence piezospectroscopy.

Degree: 2017, University of Central Florida

  Carbon fiber composites have become popular in aerospace structures and applications due to their light weight, high strength, and high performance. Hybrid carbon fiber… (more)

Subjects/Keywords: Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Jahan, S. (2017). Characterization of mechanical properties in nanoparticle reinforced hybrid carbon fiber composites using photoluminescence piezospectroscopy. (Masters Thesis). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/5666

Chicago Manual of Style (16th Edition):

Jahan, Sanjida. “Characterization of mechanical properties in nanoparticle reinforced hybrid carbon fiber composites using photoluminescence piezospectroscopy.” 2017. Masters Thesis, University of Central Florida. Accessed April 09, 2020. https://stars.library.ucf.edu/etd/5666.

MLA Handbook (7th Edition):

Jahan, Sanjida. “Characterization of mechanical properties in nanoparticle reinforced hybrid carbon fiber composites using photoluminescence piezospectroscopy.” 2017. Web. 09 Apr 2020.

Vancouver:

Jahan S. Characterization of mechanical properties in nanoparticle reinforced hybrid carbon fiber composites using photoluminescence piezospectroscopy. [Internet] [Masters thesis]. University of Central Florida; 2017. [cited 2020 Apr 09]. Available from: https://stars.library.ucf.edu/etd/5666.

Council of Science Editors:

Jahan S. Characterization of mechanical properties in nanoparticle reinforced hybrid carbon fiber composites using photoluminescence piezospectroscopy. [Masters Thesis]. University of Central Florida; 2017. Available from: https://stars.library.ucf.edu/etd/5666


University of Central Florida

15. Northam, Matthew. Investigation of PS-PVD and EB-PVD Thermal Barrier Coatings Over Lifetime Using Synchrotron X-ray Diffraction.

Degree: 2019, University of Central Florida

 Extreme operating temperatures within the turbine section of jet engines require sophisticated methods of cooling and material protection. Thermal barrier coatings (TBCs) achieve this through… (more)

Subjects/Keywords: Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Northam, M. (2019). Investigation of PS-PVD and EB-PVD Thermal Barrier Coatings Over Lifetime Using Synchrotron X-ray Diffraction. (Masters Thesis). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/6697

Chicago Manual of Style (16th Edition):

Northam, Matthew. “Investigation of PS-PVD and EB-PVD Thermal Barrier Coatings Over Lifetime Using Synchrotron X-ray Diffraction.” 2019. Masters Thesis, University of Central Florida. Accessed April 09, 2020. https://stars.library.ucf.edu/etd/6697.

MLA Handbook (7th Edition):

Northam, Matthew. “Investigation of PS-PVD and EB-PVD Thermal Barrier Coatings Over Lifetime Using Synchrotron X-ray Diffraction.” 2019. Web. 09 Apr 2020.

Vancouver:

Northam M. Investigation of PS-PVD and EB-PVD Thermal Barrier Coatings Over Lifetime Using Synchrotron X-ray Diffraction. [Internet] [Masters thesis]. University of Central Florida; 2019. [cited 2020 Apr 09]. Available from: https://stars.library.ucf.edu/etd/6697.

Council of Science Editors:

Northam M. Investigation of PS-PVD and EB-PVD Thermal Barrier Coatings Over Lifetime Using Synchrotron X-ray Diffraction. [Masters Thesis]. University of Central Florida; 2019. Available from: https://stars.library.ucf.edu/etd/6697


University of Central Florida

16. Defterli, Sinem Gozde. Kinematical Modelling and Its Analytical Inverse Kinematic Solution for the Handling Mechanism of an Agricultural Robot.

Degree: 2016, University of Central Florida

 Early detection of the crop diseases helps to prevent failure in the amount and the quality of the production. In agricultural robotics, the idea of… (more)

Subjects/Keywords: Aerospace Engineering; Engineering; Space Vehicles

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APA (6th Edition):

Defterli, S. G. (2016). Kinematical Modelling and Its Analytical Inverse Kinematic Solution for the Handling Mechanism of an Agricultural Robot. (Masters Thesis). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/5210

Chicago Manual of Style (16th Edition):

Defterli, Sinem Gozde. “Kinematical Modelling and Its Analytical Inverse Kinematic Solution for the Handling Mechanism of an Agricultural Robot.” 2016. Masters Thesis, University of Central Florida. Accessed April 09, 2020. https://stars.library.ucf.edu/etd/5210.

MLA Handbook (7th Edition):

Defterli, Sinem Gozde. “Kinematical Modelling and Its Analytical Inverse Kinematic Solution for the Handling Mechanism of an Agricultural Robot.” 2016. Web. 09 Apr 2020.

Vancouver:

Defterli SG. Kinematical Modelling and Its Analytical Inverse Kinematic Solution for the Handling Mechanism of an Agricultural Robot. [Internet] [Masters thesis]. University of Central Florida; 2016. [cited 2020 Apr 09]. Available from: https://stars.library.ucf.edu/etd/5210.

Council of Science Editors:

Defterli SG. Kinematical Modelling and Its Analytical Inverse Kinematic Solution for the Handling Mechanism of an Agricultural Robot. [Masters Thesis]. University of Central Florida; 2016. Available from: https://stars.library.ucf.edu/etd/5210


University of Central Florida

17. Menendez-Aponte, Pablo. Approximated Control Affine Dynamics Mode For an Agricultural Field Robot Considering Wheel Terrain Interaction.

Degree: 2016, University of Central Florida

 As populations and the demand for higher crop yields grow, so to does the need for efficient agricultural wheeled mobile robots. To achieve precise navigation… (more)

Subjects/Keywords: Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Menendez-Aponte, P. (2016). Approximated Control Affine Dynamics Mode For an Agricultural Field Robot Considering Wheel Terrain Interaction. (Masters Thesis). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/5323

Chicago Manual of Style (16th Edition):

Menendez-Aponte, Pablo. “Approximated Control Affine Dynamics Mode For an Agricultural Field Robot Considering Wheel Terrain Interaction.” 2016. Masters Thesis, University of Central Florida. Accessed April 09, 2020. https://stars.library.ucf.edu/etd/5323.

MLA Handbook (7th Edition):

Menendez-Aponte, Pablo. “Approximated Control Affine Dynamics Mode For an Agricultural Field Robot Considering Wheel Terrain Interaction.” 2016. Web. 09 Apr 2020.

Vancouver:

Menendez-Aponte P. Approximated Control Affine Dynamics Mode For an Agricultural Field Robot Considering Wheel Terrain Interaction. [Internet] [Masters thesis]. University of Central Florida; 2016. [cited 2020 Apr 09]. Available from: https://stars.library.ucf.edu/etd/5323.

Council of Science Editors:

Menendez-Aponte P. Approximated Control Affine Dynamics Mode For an Agricultural Field Robot Considering Wheel Terrain Interaction. [Masters Thesis]. University of Central Florida; 2016. Available from: https://stars.library.ucf.edu/etd/5323


Ryerson University

18. Manzoor, Waqas A. A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point.

Degree: 2011, Ryerson University

 This thesis examines the performance of control methods that fall under the optimal, predictive and adaptive classifications, subjected to sensor/actuator faults, and presents approaches to… (more)

Subjects/Keywords: Space vehicles  – Dynamics; Space vehicles  – Attitude control systems; Solar sails; Space trajectories

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APA (6th Edition):

Manzoor, W. A. (2011). A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1814

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):

Manzoor, Waqas A. “A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point.” 2011. Thesis, Ryerson University. Accessed April 09, 2020. https://digital.library.ryerson.ca/islandora/object/RULA%3A1814.

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

MLA Handbook (7th Edition):

Manzoor, Waqas A. “A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point.” 2011. Web. 09 Apr 2020.

Vancouver:

Manzoor WA. A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point. [Internet] [Thesis]. Ryerson University; 2011. [cited 2020 Apr 09]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1814.

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

Council of Science Editors:

Manzoor WA. A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point. [Thesis]. Ryerson University; 2011. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1814

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


Rutgers University

19. Reddy, Srikanth K., 1986-. Study of structural integrity of interstellar spacecraft reaction chamber and thrust structure in support of Project Icarus.

Degree: MS, Mechanical and Aerospace Engineering, 2014, Rutgers University

 This thesis supports studies of the international effort of Project Icarus, dedicated to the unmanned, interstellar exploration of nearby stellar systems within the next century.… (more)

Subjects/Keywords: Outer space – Exploration; Interstellar travel; Space vehicles – Design and construction; Space vehicles – Propulsion systems

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APA (6th Edition):

Reddy, Srikanth K., 1. (2014). Study of structural integrity of interstellar spacecraft reaction chamber and thrust structure in support of Project Icarus. (Masters Thesis). Rutgers University. Retrieved from https://rucore.libraries.rutgers.edu/rutgers-lib/42443/

Chicago Manual of Style (16th Edition):

Reddy, Srikanth K., 1986-. “Study of structural integrity of interstellar spacecraft reaction chamber and thrust structure in support of Project Icarus.” 2014. Masters Thesis, Rutgers University. Accessed April 09, 2020. https://rucore.libraries.rutgers.edu/rutgers-lib/42443/.

MLA Handbook (7th Edition):

Reddy, Srikanth K., 1986-. “Study of structural integrity of interstellar spacecraft reaction chamber and thrust structure in support of Project Icarus.” 2014. Web. 09 Apr 2020.

Vancouver:

Reddy, Srikanth K. 1. Study of structural integrity of interstellar spacecraft reaction chamber and thrust structure in support of Project Icarus. [Internet] [Masters thesis]. Rutgers University; 2014. [cited 2020 Apr 09]. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/42443/.

Council of Science Editors:

Reddy, Srikanth K. 1. Study of structural integrity of interstellar spacecraft reaction chamber and thrust structure in support of Project Icarus. [Masters Thesis]. Rutgers University; 2014. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/42443/


Georgia Tech

20. Kutty, Prasad M. Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics.

Degree: MS, Aerospace Engineering, 2014, Georgia Tech

 The reconstruction of entry, descent and landing (EDL) trajectories is significantly affected by the knowledge of the atmospheric conditions during flight. Away from Earth, this… (more)

Subjects/Keywords: Trajectory reconstruction; Entry, descent and landing; Space vehicles; Space trajectories; Space vehicles Atmospheric entry; Algorithms

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APA (6th Edition):

Kutty, P. M. (2014). Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51893

Chicago Manual of Style (16th Edition):

Kutty, Prasad M. “Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics.” 2014. Masters Thesis, Georgia Tech. Accessed April 09, 2020. http://hdl.handle.net/1853/51893.

MLA Handbook (7th Edition):

Kutty, Prasad M. “Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics.” 2014. Web. 09 Apr 2020.

Vancouver:

Kutty PM. Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics. [Internet] [Masters thesis]. Georgia Tech; 2014. [cited 2020 Apr 09]. Available from: http://hdl.handle.net/1853/51893.

Council of Science Editors:

Kutty PM. Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics. [Masters Thesis]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51893


The Ohio State University

21. Mostafa, Osama A. Variable structure control system maneuvering of spacecraft .

Degree: PhD, Graduate School, 1986, The Ohio State University

Subjects/Keywords: Engineering; Space vehicles

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APA (6th Edition):

Mostafa, O. A. (1986). Variable structure control system maneuvering of spacecraft . (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1487267546980772

Chicago Manual of Style (16th Edition):

Mostafa, Osama A. “Variable structure control system maneuvering of spacecraft .” 1986. Doctoral Dissertation, The Ohio State University. Accessed April 09, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1487267546980772.

MLA Handbook (7th Edition):

Mostafa, Osama A. “Variable structure control system maneuvering of spacecraft .” 1986. Web. 09 Apr 2020.

Vancouver:

Mostafa OA. Variable structure control system maneuvering of spacecraft . [Internet] [Doctoral dissertation]. The Ohio State University; 1986. [cited 2020 Apr 09]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1487267546980772.

Council of Science Editors:

Mostafa OA. Variable structure control system maneuvering of spacecraft . [Doctoral Dissertation]. The Ohio State University; 1986. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1487267546980772


The Ohio State University

22. Boling, Norman Lee. Investigation of a low-power MPD ARC.

Degree: PhD, Graduate School, 1969, The Ohio State University

Subjects/Keywords: Physics; Space vehicles

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APA (6th Edition):

Boling, N. L. (1969). Investigation of a low-power MPD ARC. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1486654338997012

Chicago Manual of Style (16th Edition):

Boling, Norman Lee. “Investigation of a low-power MPD ARC.” 1969. Doctoral Dissertation, The Ohio State University. Accessed April 09, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1486654338997012.

MLA Handbook (7th Edition):

Boling, Norman Lee. “Investigation of a low-power MPD ARC.” 1969. Web. 09 Apr 2020.

Vancouver:

Boling NL. Investigation of a low-power MPD ARC. [Internet] [Doctoral dissertation]. The Ohio State University; 1969. [cited 2020 Apr 09]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486654338997012.

Council of Science Editors:

Boling NL. Investigation of a low-power MPD ARC. [Doctoral Dissertation]. The Ohio State University; 1969. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486654338997012


University of Oklahoma

23. Boone, Tom. Financial Operational Losses in Space Launch.

Degree: PhD, 2017, University of Oklahoma

 The high cost of access to space has been a problem since the beginning of the space age. Most attempts to reduce this cost are… (more)

Subjects/Keywords: launch vehicles; space operations; cost estimation

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APA (6th Edition):

Boone, T. (2017). Financial Operational Losses in Space Launch. (Doctoral Dissertation). University of Oklahoma. Retrieved from http://hdl.handle.net/11244/50708

Chicago Manual of Style (16th Edition):

Boone, Tom. “Financial Operational Losses in Space Launch.” 2017. Doctoral Dissertation, University of Oklahoma. Accessed April 09, 2020. http://hdl.handle.net/11244/50708.

MLA Handbook (7th Edition):

Boone, Tom. “Financial Operational Losses in Space Launch.” 2017. Web. 09 Apr 2020.

Vancouver:

Boone T. Financial Operational Losses in Space Launch. [Internet] [Doctoral dissertation]. University of Oklahoma; 2017. [cited 2020 Apr 09]. Available from: http://hdl.handle.net/11244/50708.

Council of Science Editors:

Boone T. Financial Operational Losses in Space Launch. [Doctoral Dissertation]. University of Oklahoma; 2017. Available from: http://hdl.handle.net/11244/50708


Embry-Riddle Aeronautical University

24. Harvey, Megan Lewis. The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters.

Degree: MSin Engineering Physics, Physical Sciences, 2014, Embry-Riddle Aeronautical University

  Electric propulsion engines, in particular Hall thrusters, provide the possibility of long-distance, low-cost space travel. The geometrical details of the Hall thrusters, especially the… (more)

Subjects/Keywords: Aerospace Engineering; Propulsion and Power; Space Vehicles

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APA (6th Edition):

Harvey, M. L. (2014). The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/160

Chicago Manual of Style (16th Edition):

Harvey, Megan Lewis. “The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/160.

MLA Handbook (7th Edition):

Harvey, Megan Lewis. “The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters.” 2014. Web. 09 Apr 2020.

Vancouver:

Harvey ML. The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/160.

Council of Science Editors:

Harvey ML. The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/160


Embry-Riddle Aeronautical University

25. Schultz, Daniel Clyde. Spacecraft and Propulsion Technician Error.

Degree: MSin Aeronautics, Applied Aviation Sciences, 2012, Embry-Riddle Aeronautical University

  Commercial aviation and commercial space similarly launch, fly, and land passenger vehicles. Unlike aviation, the U.S. government has not established maintenance policies for commercial… (more)

Subjects/Keywords: Aviation Safety and Security; Space Vehicles

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APA (6th Edition):

Schultz, D. C. (2012). Spacecraft and Propulsion Technician Error. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/128

Chicago Manual of Style (16th Edition):

Schultz, Daniel Clyde. “Spacecraft and Propulsion Technician Error.” 2012. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/128.

MLA Handbook (7th Edition):

Schultz, Daniel Clyde. “Spacecraft and Propulsion Technician Error.” 2012. Web. 09 Apr 2020.

Vancouver:

Schultz DC. Spacecraft and Propulsion Technician Error. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2012. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/128.

Council of Science Editors:

Schultz DC. Spacecraft and Propulsion Technician Error. [Masters Thesis]. Embry-Riddle Aeronautical University; 2012. Available from: https://commons.erau.edu/edt/128


Embry-Riddle Aeronautical University

26. Ehrlich, Joshua W. Investigation of a Lagrangian-point Propellant Depot Rendezvous Approach for an Interplanetary Mission to Mars.

Degree: MSin Mechanical Engineering, Mechanical Engineering, 2013, Embry-Riddle Aeronautical University

  This thesis investigates the feasibility of a refueling station for a beyond Earth orbit (BEO) mission. The propellant depot is located at the … (more)

Subjects/Keywords: Aerospace Engineering; Astrophysics and Astronomy; Space Vehicles

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APA (6th Edition):

Ehrlich, J. W. (2013). Investigation of a Lagrangian-point Propellant Depot Rendezvous Approach for an Interplanetary Mission to Mars. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/61

Chicago Manual of Style (16th Edition):

Ehrlich, Joshua W. “Investigation of a Lagrangian-point Propellant Depot Rendezvous Approach for an Interplanetary Mission to Mars.” 2013. Masters Thesis, Embry-Riddle Aeronautical University. Accessed April 09, 2020. https://commons.erau.edu/edt/61.

MLA Handbook (7th Edition):

Ehrlich, Joshua W. “Investigation of a Lagrangian-point Propellant Depot Rendezvous Approach for an Interplanetary Mission to Mars.” 2013. Web. 09 Apr 2020.

Vancouver:

Ehrlich JW. Investigation of a Lagrangian-point Propellant Depot Rendezvous Approach for an Interplanetary Mission to Mars. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2013. [cited 2020 Apr 09]. Available from: https://commons.erau.edu/edt/61.

Council of Science Editors:

Ehrlich JW. Investigation of a Lagrangian-point Propellant Depot Rendezvous Approach for an Interplanetary Mission to Mars. [Masters Thesis]. Embry-Riddle Aeronautical University; 2013. Available from: https://commons.erau.edu/edt/61


University of Colorado

27. Howard, Micah A. Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems.

Degree: PhD, Aerospace Engineering Sciences, 2010, University of Colorado

  The design of supersonic and hypersonic aerospace vehicles is by nature a multi-disciplinary problem requiring the close integration of compressible fluid dynamics, heat transfer,… (more)

Subjects/Keywords: aerospace vehicles; aerothermoelastic behavior; thermal and structural performance; Aeronautical Vehicles; Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Howard, M. A. (2010). Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/9

Chicago Manual of Style (16th Edition):

Howard, Micah A. “Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems.” 2010. Doctoral Dissertation, University of Colorado. Accessed April 09, 2020. https://scholar.colorado.edu/asen_gradetds/9.

MLA Handbook (7th Edition):

Howard, Micah A. “Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems.” 2010. Web. 09 Apr 2020.

Vancouver:

Howard MA. Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems. [Internet] [Doctoral dissertation]. University of Colorado; 2010. [cited 2020 Apr 09]. Available from: https://scholar.colorado.edu/asen_gradetds/9.

Council of Science Editors:

Howard MA. Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems. [Doctoral Dissertation]. University of Colorado; 2010. Available from: https://scholar.colorado.edu/asen_gradetds/9


Stellenbosch University

28. Mfiri, Tatenda Joshua. Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform.

Degree: MScEng, Electrical and Electronic Engineering, 2019, Stellenbosch University

ENGLISH ABSTRACT: This thesis contributes to the research of persistent tethered aerial vehicles by presenting a strategy to autonomously land a tethered multi-rotor UAV. A… (more)

Subjects/Keywords: Landing aids (Aeronautics); Tethered space vehicles; Unmanned aerial vehicles; UCTD

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APA (6th Edition):

Mfiri, T. J. (2019). Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform. (Masters Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/105897

Chicago Manual of Style (16th Edition):

Mfiri, Tatenda Joshua. “Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform.” 2019. Masters Thesis, Stellenbosch University. Accessed April 09, 2020. http://hdl.handle.net/10019.1/105897.

MLA Handbook (7th Edition):

Mfiri, Tatenda Joshua. “Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform.” 2019. Web. 09 Apr 2020.

Vancouver:

Mfiri TJ. Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform. [Internet] [Masters thesis]. Stellenbosch University; 2019. [cited 2020 Apr 09]. Available from: http://hdl.handle.net/10019.1/105897.

Council of Science Editors:

Mfiri TJ. Autonomous landing of a tethered multi-rotor unmanned aerial vehicle on a stationary platform. [Masters Thesis]. Stellenbosch University; 2019. Available from: http://hdl.handle.net/10019.1/105897


Ryerson University

29. Frias, Alexander. Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics.

Degree: 2012, Ryerson University

 Spacecraft formation flying with coupled orbital-attitude dynamics is one of the most intriguing topics in the field of astronautics. Orbital-attitude coupling is induced when a… (more)

Subjects/Keywords: Space vehicles  – Design and construction; Astronautics  – Systems engineering; Orbital mechanics; Space vehicles  – Control systems

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APA (6th Edition):

Frias, A. (2012). Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1610

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):

Frias, Alexander. “Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics.” 2012. Thesis, Ryerson University. Accessed April 09, 2020. https://digital.library.ryerson.ca/islandora/object/RULA%3A1610.

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

MLA Handbook (7th Edition):

Frias, Alexander. “Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics.” 2012. Web. 09 Apr 2020.

Vancouver:

Frias A. Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics. [Internet] [Thesis]. Ryerson University; 2012. [cited 2020 Apr 09]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1610.

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

Council of Science Editors:

Frias A. Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics. [Thesis]. Ryerson University; 2012. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1610

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


Ryerson University

30. Vaz, Brendon. Online calibration for star trackers.

Degree: 2013, Ryerson University

 Star trackers are perhaps the most accurate means of measuring a spacecraft's orientation in space and are becoming a popular sensing instrument for attitude determination… (more)

Subjects/Keywords: Star trackers; Star tracking systems; Space vehicles  – Attitude control systems; Space vehicles  – Dynamics

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APA (6th Edition):

Vaz, B. (2013). Online calibration for star trackers. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A2874

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):

Vaz, Brendon. “Online calibration for star trackers.” 2013. Thesis, Ryerson University. Accessed April 09, 2020. https://digital.library.ryerson.ca/islandora/object/RULA%3A2874.

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

MLA Handbook (7th Edition):

Vaz, Brendon. “Online calibration for star trackers.” 2013. Web. 09 Apr 2020.

Vancouver:

Vaz B. Online calibration for star trackers. [Internet] [Thesis]. Ryerson University; 2013. [cited 2020 Apr 09]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A2874.

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

Council of Science Editors:

Vaz B. Online calibration for star trackers. [Thesis]. Ryerson University; 2013. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A2874

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

[1] [2] [3] [4] [5] [6] [7] [8] [9] [10]

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