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You searched for subject:(Spacecraft). Showing records 1 – 30 of 382 total matches.

[1] [2] [3] [4] [5] … [13]

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Cornell University

1. Manchester, Zachary. Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment .

Degree: 2015, Cornell University

 The rise of the consumer electronics industry has led to a profusion of ever smaller, cheaper, and more capable devices, from sensors to computers to… (more)

Subjects/Keywords: Small Spacecraft; Spacecraft Dynamics; Space Systems

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APA (6th Edition):

Manchester, Z. (2015). Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/41055

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):

Manchester, Zachary. “Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment .” 2015. Thesis, Cornell University. Accessed August 08, 2020. http://hdl.handle.net/1813/41055.

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

MLA Handbook (7th Edition):

Manchester, Zachary. “Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment .” 2015. Web. 08 Aug 2020.

Vancouver:

Manchester Z. Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment . [Internet] [Thesis]. Cornell University; 2015. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1813/41055.

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

Council of Science Editors:

Manchester Z. Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment . [Thesis]. Cornell University; 2015. Available from: http://hdl.handle.net/1813/41055

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


Virginia Tech

2. Evans, Julianna Marie. Spacecraft-ns3: Spacecraft Discrete-Event Network Simulation.

Degree: MS, Aerospace Engineering, 2020, Virginia Tech

 Near-Earth space has become more crowded in recent years due to the increasing number of large constellations of satellites in this region. Autonomous vehicle research… (more)

Subjects/Keywords: Spacecraft; Network; Simulation

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APA (6th Edition):

Evans, J. M. (2020). Spacecraft-ns3: Spacecraft Discrete-Event Network Simulation. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/99102

Chicago Manual of Style (16th Edition):

Evans, Julianna Marie. “Spacecraft-ns3: Spacecraft Discrete-Event Network Simulation.” 2020. Masters Thesis, Virginia Tech. Accessed August 08, 2020. http://hdl.handle.net/10919/99102.

MLA Handbook (7th Edition):

Evans, Julianna Marie. “Spacecraft-ns3: Spacecraft Discrete-Event Network Simulation.” 2020. Web. 08 Aug 2020.

Vancouver:

Evans JM. Spacecraft-ns3: Spacecraft Discrete-Event Network Simulation. [Internet] [Masters thesis]. Virginia Tech; 2020. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/10919/99102.

Council of Science Editors:

Evans JM. Spacecraft-ns3: Spacecraft Discrete-Event Network Simulation. [Masters Thesis]. Virginia Tech; 2020. Available from: http://hdl.handle.net/10919/99102


Cornell University

3. Reinhardt, Benjamin. Induction Couplers: Contactless On-Orbit Actuation For Space Robotics .

Degree: 2015, Cornell University

 Induction couplers exploit eddy-current effects to create force and torque on a target without mechanical contact. Nearly all spacecraft structures include conductive material, so induction… (more)

Subjects/Keywords: Spacecraft; Robotics; Electromagnetism

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APA (6th Edition):

Reinhardt, B. (2015). Induction Couplers: Contactless On-Orbit Actuation For Space Robotics . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/40607

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):

Reinhardt, Benjamin. “Induction Couplers: Contactless On-Orbit Actuation For Space Robotics .” 2015. Thesis, Cornell University. Accessed August 08, 2020. http://hdl.handle.net/1813/40607.

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

MLA Handbook (7th Edition):

Reinhardt, Benjamin. “Induction Couplers: Contactless On-Orbit Actuation For Space Robotics .” 2015. Web. 08 Aug 2020.

Vancouver:

Reinhardt B. Induction Couplers: Contactless On-Orbit Actuation For Space Robotics . [Internet] [Thesis]. Cornell University; 2015. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1813/40607.

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

Council of Science Editors:

Reinhardt B. Induction Couplers: Contactless On-Orbit Actuation For Space Robotics . [Thesis]. Cornell University; 2015. Available from: http://hdl.handle.net/1813/40607

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


University of Southern California

4. Reddy, Shalini A. Control of spacecraft with flexible structures using pulse-modulated thrusters.

Degree: PhD, Mechanical Engineering, 2012, University of Southern California

 A methodology for the design of robust control systems for flexible spacecraft undergoing a large angle maneuver using pulse-modulated thrusters is proposed. The need for… (more)

Subjects/Keywords: spacecraft; dynamics; control

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APA (6th Edition):

Reddy, S. A. (2012). Control of spacecraft with flexible structures using pulse-modulated thrusters. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/84663/rec/1641

Chicago Manual of Style (16th Edition):

Reddy, Shalini A. “Control of spacecraft with flexible structures using pulse-modulated thrusters.” 2012. Doctoral Dissertation, University of Southern California. Accessed August 08, 2020. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/84663/rec/1641.

MLA Handbook (7th Edition):

Reddy, Shalini A. “Control of spacecraft with flexible structures using pulse-modulated thrusters.” 2012. Web. 08 Aug 2020.

Vancouver:

Reddy SA. Control of spacecraft with flexible structures using pulse-modulated thrusters. [Internet] [Doctoral dissertation]. University of Southern California; 2012. [cited 2020 Aug 08]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/84663/rec/1641.

Council of Science Editors:

Reddy SA. Control of spacecraft with flexible structures using pulse-modulated thrusters. [Doctoral Dissertation]. University of Southern California; 2012. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/84663/rec/1641

5. Pande, Seetesh. Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -.

Degree: Aerospace Engineering, 2013, University of Petroleum and Energy Studies (UPES)

Abstract avalible

References p.116 - 120 and Appendix p.121 - 129

Advisors/Committee Members: Ugur, Guven.

Subjects/Keywords: Spacecraft; Stellar

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APA (6th Edition):

Pande, S. (2013). Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -. (Thesis). University of Petroleum and Energy Studies (UPES). Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/41384

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):

Pande, Seetesh. “Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -.” 2013. Thesis, University of Petroleum and Energy Studies (UPES). Accessed August 08, 2020. http://shodhganga.inflibnet.ac.in/handle/10603/41384.

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

MLA Handbook (7th Edition):

Pande, Seetesh. “Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -.” 2013. Web. 08 Aug 2020.

Vancouver:

Pande S. Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -. [Internet] [Thesis]. University of Petroleum and Energy Studies (UPES); 2013. [cited 2020 Aug 08]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/41384.

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

Council of Science Editors:

Pande S. Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -. [Thesis]. University of Petroleum and Energy Studies (UPES); 2013. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/41384

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


Delft University of Technology

6. Kuiper, J.M. Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures.

Degree: 2012, Delft University of Technology

 Mass-spring and liquid dampers enable structural vibration control to attenuate single, coupled lateral and torsional vibrations in diverse structures. Out of these, the passively tuned… (more)

Subjects/Keywords: Spacecraft ADCS

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APA (6th Edition):

Kuiper, J. M. (2012). Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60

Chicago Manual of Style (16th Edition):

Kuiper, J M. “Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures.” 2012. Doctoral Dissertation, Delft University of Technology. Accessed August 08, 2020. http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60.

MLA Handbook (7th Edition):

Kuiper, J M. “Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures.” 2012. Web. 08 Aug 2020.

Vancouver:

Kuiper JM. Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures. [Internet] [Doctoral dissertation]. Delft University of Technology; 2012. [cited 2020 Aug 08]. Available from: http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60.

Council of Science Editors:

Kuiper JM. Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures. [Doctoral Dissertation]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60


Rice University

7. Warden, David. Analysis of Passive Radiation Shielding from Galactic Cosmic Rays in Cis-Lunar Space.

Degree: PhD, Engineering, 2019, Rice University

 Adequate long-term radiation protection protocols do not yet exist for the contemplated spaceflights beyond the Earth’s magnetosphere or for colonization of places like the Moon… (more)

Subjects/Keywords: GCR Radiation; Spacecraft; Shielding

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APA (6th Edition):

Warden, D. (2019). Analysis of Passive Radiation Shielding from Galactic Cosmic Rays in Cis-Lunar Space. (Doctoral Dissertation). Rice University. Retrieved from http://hdl.handle.net/1911/105991

Chicago Manual of Style (16th Edition):

Warden, David. “Analysis of Passive Radiation Shielding from Galactic Cosmic Rays in Cis-Lunar Space.” 2019. Doctoral Dissertation, Rice University. Accessed August 08, 2020. http://hdl.handle.net/1911/105991.

MLA Handbook (7th Edition):

Warden, David. “Analysis of Passive Radiation Shielding from Galactic Cosmic Rays in Cis-Lunar Space.” 2019. Web. 08 Aug 2020.

Vancouver:

Warden D. Analysis of Passive Radiation Shielding from Galactic Cosmic Rays in Cis-Lunar Space. [Internet] [Doctoral dissertation]. Rice University; 2019. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1911/105991.

Council of Science Editors:

Warden D. Analysis of Passive Radiation Shielding from Galactic Cosmic Rays in Cis-Lunar Space. [Doctoral Dissertation]. Rice University; 2019. Available from: http://hdl.handle.net/1911/105991


University of Florida

8. Ausay, Erick Alberto. Model Predictive Control with Continuous Thrust for Spacecraft Formation Flying Applications.

Degree: MS, Mechanical Engineering - Mechanical and Aerospace Engineering, 2019, University of Florida

Spacecraft formation flying offers many advantages in the form of cost, functionality, and performance. Future missions involving spacecraft formation flying will require high levels of… (more)

Subjects/Keywords: control  – formation  – mpc  – optimal  – spacecraft

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APA (6th Edition):

Ausay, E. A. (2019). Model Predictive Control with Continuous Thrust for Spacecraft Formation Flying Applications. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0056167

Chicago Manual of Style (16th Edition):

Ausay, Erick Alberto. “Model Predictive Control with Continuous Thrust for Spacecraft Formation Flying Applications.” 2019. Masters Thesis, University of Florida. Accessed August 08, 2020. https://ufdc.ufl.edu/UFE0056167.

MLA Handbook (7th Edition):

Ausay, Erick Alberto. “Model Predictive Control with Continuous Thrust for Spacecraft Formation Flying Applications.” 2019. Web. 08 Aug 2020.

Vancouver:

Ausay EA. Model Predictive Control with Continuous Thrust for Spacecraft Formation Flying Applications. [Internet] [Masters thesis]. University of Florida; 2019. [cited 2020 Aug 08]. Available from: https://ufdc.ufl.edu/UFE0056167.

Council of Science Editors:

Ausay EA. Model Predictive Control with Continuous Thrust for Spacecraft Formation Flying Applications. [Masters Thesis]. University of Florida; 2019. Available from: https://ufdc.ufl.edu/UFE0056167


Penn State University

9. Muncks, John P. Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft.

Degree: MS, Aerospace Engineering, 2014, Penn State University

 In this thesis, a process to identify cost-efficient tracking solutions for interplanetary missions is presented. The process is flexible enough to be used in a… (more)

Subjects/Keywords: interplanetary spacecraft; spacecraft tracking; cost-efficient; Deep Space Network

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APA (6th Edition):

Muncks, J. P. (2014). Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/23702

Chicago Manual of Style (16th Edition):

Muncks, John P. “Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft.” 2014. Masters Thesis, Penn State University. Accessed August 08, 2020. https://etda.libraries.psu.edu/catalog/23702.

MLA Handbook (7th Edition):

Muncks, John P. “Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft.” 2014. Web. 08 Aug 2020.

Vancouver:

Muncks JP. Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft. [Internet] [Masters thesis]. Penn State University; 2014. [cited 2020 Aug 08]. Available from: https://etda.libraries.psu.edu/catalog/23702.

Council of Science Editors:

Muncks JP. Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft. [Masters Thesis]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/23702


Virginia Tech

10. Berryman, John Fagan. Analytical and Numerical Analysis of Static Coulomb Formations.

Degree: MS, Aerospace and Ocean Engineering, 2005, Virginia Tech

 For close proximity flying on the order of 10-100 meters, Coulomb thrusting presents a promising alternative to other methods of propulsion. This clean and fuel-efficient… (more)

Subjects/Keywords: Spacecraft Formation; Coulomb Spacecraft

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APA (6th Edition):

Berryman, J. F. (2005). Analytical and Numerical Analysis of Static Coulomb Formations. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36000

Chicago Manual of Style (16th Edition):

Berryman, John Fagan. “Analytical and Numerical Analysis of Static Coulomb Formations.” 2005. Masters Thesis, Virginia Tech. Accessed August 08, 2020. http://hdl.handle.net/10919/36000.

MLA Handbook (7th Edition):

Berryman, John Fagan. “Analytical and Numerical Analysis of Static Coulomb Formations.” 2005. Web. 08 Aug 2020.

Vancouver:

Berryman JF. Analytical and Numerical Analysis of Static Coulomb Formations. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/10919/36000.

Council of Science Editors:

Berryman JF. Analytical and Numerical Analysis of Static Coulomb Formations. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/36000


University of Cincinnati

11. Dadhich, Anang. Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 This thesis concentrates on developing an innovative method to generate thrust force for spacecraft in localized geomagnetic fields by various electromagnetic systems. The proposed electromagnetic… (more)

Subjects/Keywords: Aerospace Materials; Electromagnetic Propulsion; Superconductivity; Cryogenics; Spacecraft; Satellite; Spacecraft Propulsion

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APA (6th Edition):

Dadhich, A. (2016). Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1461592799

Chicago Manual of Style (16th Edition):

Dadhich, Anang. “Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors.” 2016. Masters Thesis, University of Cincinnati. Accessed August 08, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1461592799.

MLA Handbook (7th Edition):

Dadhich, Anang. “Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors.” 2016. Web. 08 Aug 2020.

Vancouver:

Dadhich A. Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors. [Internet] [Masters thesis]. University of Cincinnati; 2016. [cited 2020 Aug 08]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1461592799.

Council of Science Editors:

Dadhich A. Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors. [Masters Thesis]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1461592799


University of Colorado

12. Stiles, Laura Ann. Electrostatic In ation of Membrane Space Structures.

Degree: PhD, Aerospace Engineering Sciences, 2013, University of Colorado

  Membrane space structures provide a lightweight and cost effective alternative to traditional mechanical systems. The low-mass and high deployed-to-stored volume ratios allow for larger… (more)

Subjects/Keywords: Deployable Spacecraft; Inflatable Structures; Plasma Physics; Spacecraft Charging; Aerospace Engineering

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APA (6th Edition):

Stiles, L. A. (2013). Electrostatic In ation of Membrane Space Structures. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/92

Chicago Manual of Style (16th Edition):

Stiles, Laura Ann. “Electrostatic In ation of Membrane Space Structures.” 2013. Doctoral Dissertation, University of Colorado. Accessed August 08, 2020. https://scholar.colorado.edu/asen_gradetds/92.

MLA Handbook (7th Edition):

Stiles, Laura Ann. “Electrostatic In ation of Membrane Space Structures.” 2013. Web. 08 Aug 2020.

Vancouver:

Stiles LA. Electrostatic In ation of Membrane Space Structures. [Internet] [Doctoral dissertation]. University of Colorado; 2013. [cited 2020 Aug 08]. Available from: https://scholar.colorado.edu/asen_gradetds/92.

Council of Science Editors:

Stiles LA. Electrostatic In ation of Membrane Space Structures. [Doctoral Dissertation]. University of Colorado; 2013. Available from: https://scholar.colorado.edu/asen_gradetds/92

13. Shear, Eric Magnus. Small Spacecraft for Planetary Exploration.

Degree: MSc -MS, Earth & Space Science, 2018, York University

 After an overview of the progress that have been made in small spacecraft for planetary exploration, two planetary mission studies utilizing small spacecraft technologies are… (more)

Subjects/Keywords: Planetology; CubeSats; Spacecraft networks; Small spacecraft; Saturn; Rings; Planetary science

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APA (6th Edition):

Shear, E. M. (2018). Small Spacecraft for Planetary Exploration. (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/34545

Chicago Manual of Style (16th Edition):

Shear, Eric Magnus. “Small Spacecraft for Planetary Exploration.” 2018. Masters Thesis, York University. Accessed August 08, 2020. http://hdl.handle.net/10315/34545.

MLA Handbook (7th Edition):

Shear, Eric Magnus. “Small Spacecraft for Planetary Exploration.” 2018. Web. 08 Aug 2020.

Vancouver:

Shear EM. Small Spacecraft for Planetary Exploration. [Internet] [Masters thesis]. York University; 2018. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/10315/34545.

Council of Science Editors:

Shear EM. Small Spacecraft for Planetary Exploration. [Masters Thesis]. York University; 2018. Available from: http://hdl.handle.net/10315/34545


Georgia Tech

14. Francis, Parker. Development of the evolved common hardware bus (TECHBus).

Degree: MS, Aerospace Engineering, 2016, Georgia Tech

 This thesis presents the design and analysis of a small spacecraft bus for use by the Georgia Tech Space Systems Design Lab. It is designed… (more)

Subjects/Keywords: Spacecraft design; Spacecraft bus; Reliability; CubeSat; Nanosatellite; Small satellite

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APA (6th Edition):

Francis, P. (2016). Development of the evolved common hardware bus (TECHBus). (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55671

Chicago Manual of Style (16th Edition):

Francis, Parker. “Development of the evolved common hardware bus (TECHBus).” 2016. Masters Thesis, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/55671.

MLA Handbook (7th Edition):

Francis, Parker. “Development of the evolved common hardware bus (TECHBus).” 2016. Web. 08 Aug 2020.

Vancouver:

Francis P. Development of the evolved common hardware bus (TECHBus). [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/55671.

Council of Science Editors:

Francis P. Development of the evolved common hardware bus (TECHBus). [Masters Thesis]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55671


Lehigh University

15. Zhu, Shiqiao. Analysis of Spacecraft Attitude Control.

Degree: MS, Mechanical Engineering, 2016, Lehigh University

 The thesis studies about repositioning the spacecraft to obtain a moving target problem. We model the spacecraft as a rigid body with axis torque controlling… (more)

Subjects/Keywords: alalysis of spacecraft attitude control; analysis control; attitude; attitude control; attitude of spacecraft; spacecraft control; Engineering; Mechanical Engineering

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APA (6th Edition):

Zhu, S. (2016). Analysis of Spacecraft Attitude Control. (Thesis). Lehigh University. Retrieved from https://preserve.lehigh.edu/etd/2915

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):

Zhu, Shiqiao. “Analysis of Spacecraft Attitude Control.” 2016. Thesis, Lehigh University. Accessed August 08, 2020. https://preserve.lehigh.edu/etd/2915.

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

MLA Handbook (7th Edition):

Zhu, Shiqiao. “Analysis of Spacecraft Attitude Control.” 2016. Web. 08 Aug 2020.

Vancouver:

Zhu S. Analysis of Spacecraft Attitude Control. [Internet] [Thesis]. Lehigh University; 2016. [cited 2020 Aug 08]. Available from: https://preserve.lehigh.edu/etd/2915.

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

Council of Science Editors:

Zhu S. Analysis of Spacecraft Attitude Control. [Thesis]. Lehigh University; 2016. Available from: https://preserve.lehigh.edu/etd/2915

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


Cleveland State University

16. Jurns, John M. Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions.

Degree: MSin Mechanical Engineering, Fenn College of Engineering, 2007, Cleveland State University

 Cryogenic fluid systems are fundamental to space flight architecture. Due to the unique properties of cryogenic fluids and the environments in which they operate for… (more)

Subjects/Keywords: Cryogenic; refrigeration; Joule-Thomson; spacecraft; fluid management

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APA (6th Edition):

Jurns, J. M. (2007). Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions. (Masters Thesis). Cleveland State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=csu1198954696

Chicago Manual of Style (16th Edition):

Jurns, John M. “Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions.” 2007. Masters Thesis, Cleveland State University. Accessed August 08, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=csu1198954696.

MLA Handbook (7th Edition):

Jurns, John M. “Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions.” 2007. Web. 08 Aug 2020.

Vancouver:

Jurns JM. Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions. [Internet] [Masters thesis]. Cleveland State University; 2007. [cited 2020 Aug 08]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=csu1198954696.

Council of Science Editors:

Jurns JM. Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions. [Masters Thesis]. Cleveland State University; 2007. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=csu1198954696


Penn State University

17. Abaimov, Mikhail D. Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.

Degree: MS, Aerospace Engineering, 2015, Penn State University

 CubeSats are small satellites that conform to combinations of a standard 10×10×10 cm form factor. Currently, CubeSats have limited propulsion options because their restrictive size.… (more)

Subjects/Keywords: microwave; electrothermal; thruster; CubeSat; small; spacecraft

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APA (6th Edition):

Abaimov, M. D. (2015). Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/26633

Chicago Manual of Style (16th Edition):

Abaimov, Mikhail D. “Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.” 2015. Masters Thesis, Penn State University. Accessed August 08, 2020. https://etda.libraries.psu.edu/catalog/26633.

MLA Handbook (7th Edition):

Abaimov, Mikhail D. “Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.” 2015. Web. 08 Aug 2020.

Vancouver:

Abaimov MD. Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft. [Internet] [Masters thesis]. Penn State University; 2015. [cited 2020 Aug 08]. Available from: https://etda.libraries.psu.edu/catalog/26633.

Council of Science Editors:

Abaimov MD. Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft. [Masters Thesis]. Penn State University; 2015. Available from: https://etda.libraries.psu.edu/catalog/26633


Penn State University

18. Peterson-Burch, Shea Donald Forrest. A Reusable Spacecraft Command and Telemetry Storage Framework.

Degree: MS, Aerospace Engineering, 2009, Penn State University

 The problem of successfully managing the ever increasing quantity of spacecraft commands and telemetry involved in today’s typical spacecraft missions demands building a standardized spacecraft(more)

Subjects/Keywords: spacecraft; commands; telemetry; command and telemetry database

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APA (6th Edition):

Peterson-Burch, S. D. F. (2009). A Reusable Spacecraft Command and Telemetry Storage Framework. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9696

Chicago Manual of Style (16th Edition):

Peterson-Burch, Shea Donald Forrest. “A Reusable Spacecraft Command and Telemetry Storage Framework.” 2009. Masters Thesis, Penn State University. Accessed August 08, 2020. https://etda.libraries.psu.edu/catalog/9696.

MLA Handbook (7th Edition):

Peterson-Burch, Shea Donald Forrest. “A Reusable Spacecraft Command and Telemetry Storage Framework.” 2009. Web. 08 Aug 2020.

Vancouver:

Peterson-Burch SDF. A Reusable Spacecraft Command and Telemetry Storage Framework. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2020 Aug 08]. Available from: https://etda.libraries.psu.edu/catalog/9696.

Council of Science Editors:

Peterson-Burch SDF. A Reusable Spacecraft Command and Telemetry Storage Framework. [Masters Thesis]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9696


Penn State University

19. Hassa, Christopher Louis. Drag Coefficient Estimation using Satellite Attitude and Orbit Data.

Degree: MS, Aerospace Engineering, 2013, Penn State University

 The coefficient of drag for spacecraft in a variety of orbits and solar cycle conditions is generally assumed to be a constant value of 2.2.… (more)

Subjects/Keywords: Swift; coefficient of drag; spacecraft drag coefficient

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APA (6th Edition):

Hassa, C. L. (2013). Drag Coefficient Estimation using Satellite Attitude and Orbit Data. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/19949

Chicago Manual of Style (16th Edition):

Hassa, Christopher Louis. “Drag Coefficient Estimation using Satellite Attitude and Orbit Data.” 2013. Masters Thesis, Penn State University. Accessed August 08, 2020. https://etda.libraries.psu.edu/catalog/19949.

MLA Handbook (7th Edition):

Hassa, Christopher Louis. “Drag Coefficient Estimation using Satellite Attitude and Orbit Data.” 2013. Web. 08 Aug 2020.

Vancouver:

Hassa CL. Drag Coefficient Estimation using Satellite Attitude and Orbit Data. [Internet] [Masters thesis]. Penn State University; 2013. [cited 2020 Aug 08]. Available from: https://etda.libraries.psu.edu/catalog/19949.

Council of Science Editors:

Hassa CL. Drag Coefficient Estimation using Satellite Attitude and Orbit Data. [Masters Thesis]. Penn State University; 2013. Available from: https://etda.libraries.psu.edu/catalog/19949


Texas A&M University

20. Hart, Jeremy Jay. Methodology for prototyping increased levels of automation for spacecraft rendezvous functions.

Degree: 2009, Texas A&M University

 The Crew Exploration Vehicle (CEV) necessitates higher levels of automation than previous NASA vehicles due to program requirements for automation, including Automated Rendezvous and Docking… (more)

Subjects/Keywords: Automation; Spacecraft; Rendezvous; Decision-making; Fuzzy Logic

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APA (6th Edition):

Hart, J. J. (2009). Methodology for prototyping increased levels of automation for spacecraft rendezvous functions. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1220

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):

Hart, Jeremy Jay. “Methodology for prototyping increased levels of automation for spacecraft rendezvous functions.” 2009. Thesis, Texas A&M University. Accessed August 08, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1220.

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

MLA Handbook (7th Edition):

Hart, Jeremy Jay. “Methodology for prototyping increased levels of automation for spacecraft rendezvous functions.” 2009. Web. 08 Aug 2020.

Vancouver:

Hart JJ. Methodology for prototyping increased levels of automation for spacecraft rendezvous functions. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1220.

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

Council of Science Editors:

Hart JJ. Methodology for prototyping increased levels of automation for spacecraft rendezvous functions. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1220

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


Texas A&M University

21. Morris, Jeffery C. Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor.

Degree: 2010, Texas A&M University

 Automated spacecraft docking is a concept of operations with several important potential applications. One application that has received a great deal of attention recently is… (more)

Subjects/Keywords: Spacecraft docking; Vision-based sensors; relative navigation

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APA (6th Edition):

Morris, J. C. (2010). Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2820

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):

Morris, Jeffery C. “Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor.” 2010. Thesis, Texas A&M University. Accessed August 08, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2820.

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

MLA Handbook (7th Edition):

Morris, Jeffery C. “Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor.” 2010. Web. 08 Aug 2020.

Vancouver:

Morris JC. Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2820.

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

Council of Science Editors:

Morris JC. Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2820

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

22. Rohrer, Todd Edward Bloomquist. An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument.

Degree: MS, Electrical and Computer Engineering, 2017, Virginia Tech

 Neutral gas pressure measurements in low Earth orbit (LEO) can facilitate the monitoring of atmospheric gravity waves, which can trigger instabilities that severely disrupt radio… (more)

Subjects/Keywords: Space; Spacecraft; CubeSat; Instrumentation; Analog Circuit Design

Page 1 Page 2

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APA (6th Edition):

Rohrer, T. E. B. (2017). An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/74916

Chicago Manual of Style (16th Edition):

Rohrer, Todd Edward Bloomquist. “An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument.” 2017. Masters Thesis, Virginia Tech. Accessed August 08, 2020. http://hdl.handle.net/10919/74916.

MLA Handbook (7th Edition):

Rohrer, Todd Edward Bloomquist. “An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument.” 2017. Web. 08 Aug 2020.

Vancouver:

Rohrer TEB. An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/10919/74916.

Council of Science Editors:

Rohrer TEB. An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/74916


Virginia Tech

23. Marshall, Peter Johannes. Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method.

Degree: MS, Aerospace and Ocean Engineering, 2018, Virginia Tech

Spacecraft structures are subject to a series of load environments during their service life, with the most severe of these occurring during the spacecraft's launch… (more)

Subjects/Keywords: Acoustics; Spacecraft Structures; Boundary Element Method

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APA (6th Edition):

Marshall, P. J. (2018). Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/83460

Chicago Manual of Style (16th Edition):

Marshall, Peter Johannes. “Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method.” 2018. Masters Thesis, Virginia Tech. Accessed August 08, 2020. http://hdl.handle.net/10919/83460.

MLA Handbook (7th Edition):

Marshall, Peter Johannes. “Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method.” 2018. Web. 08 Aug 2020.

Vancouver:

Marshall PJ. Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/10919/83460.

Council of Science Editors:

Marshall PJ. Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/83460


Cornell University

24. Norman, Michael. Integrals Of Motion For Fractionated Space Systems .

Degree: 2011, Cornell University

 As space system architectures begin to rely upon cooperation between multiple spacecraft to perform a single task, the analysis and control of the relative motion… (more)

Subjects/Keywords: Spacecraft; Integrals of Motion; Parameter Estimation

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APA (6th Edition):

Norman, M. (2011). Integrals Of Motion For Fractionated Space Systems . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/30688

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):

Norman, Michael. “Integrals Of Motion For Fractionated Space Systems .” 2011. Thesis, Cornell University. Accessed August 08, 2020. http://hdl.handle.net/1813/30688.

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

MLA Handbook (7th Edition):

Norman, Michael. “Integrals Of Motion For Fractionated Space Systems .” 2011. Web. 08 Aug 2020.

Vancouver:

Norman M. Integrals Of Motion For Fractionated Space Systems . [Internet] [Thesis]. Cornell University; 2011. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1813/30688.

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

Council of Science Editors:

Norman M. Integrals Of Motion For Fractionated Space Systems . [Thesis]. Cornell University; 2011. Available from: http://hdl.handle.net/1813/30688

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


Cornell University

25. Jones, Laura. The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment .

Degree: 2012, Cornell University

 Advanced space systems are increasingly reliant on close-proximity operations to achieve complex mission objectives on orbit. These maneuvers - such as docking and rendezvous, formation… (more)

Subjects/Keywords: Flux-pinned interface; spacecraft technology; superconducting physics

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APA (6th Edition):

Jones, L. (2012). The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/31088

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):

Jones, Laura. “The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment .” 2012. Thesis, Cornell University. Accessed August 08, 2020. http://hdl.handle.net/1813/31088.

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

MLA Handbook (7th Edition):

Jones, Laura. “The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment .” 2012. Web. 08 Aug 2020.

Vancouver:

Jones L. The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment . [Internet] [Thesis]. Cornell University; 2012. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1813/31088.

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

Council of Science Editors:

Jones L. The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment . [Thesis]. Cornell University; 2012. Available from: http://hdl.handle.net/1813/31088

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


Cornell University

26. Zeledon, Rodrigo. Electrolysis Propulsion For Small-Scale Spacecraft .

Degree: 2015, Cornell University

 In the past decade, CubeSats have revolutionized small spacecraft missions. These miniature satellites began as educational projects but have lowered the bar for access to… (more)

Subjects/Keywords: Electrolysis propulsion; Small satellites; Spacecraft dynamics

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APA (6th Edition):

Zeledon, R. (2015). Electrolysis Propulsion For Small-Scale Spacecraft . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/40701

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):

Zeledon, Rodrigo. “Electrolysis Propulsion For Small-Scale Spacecraft .” 2015. Thesis, Cornell University. Accessed August 08, 2020. http://hdl.handle.net/1813/40701.

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

MLA Handbook (7th Edition):

Zeledon, Rodrigo. “Electrolysis Propulsion For Small-Scale Spacecraft .” 2015. Web. 08 Aug 2020.

Vancouver:

Zeledon R. Electrolysis Propulsion For Small-Scale Spacecraft . [Internet] [Thesis]. Cornell University; 2015. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1813/40701.

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

Council of Science Editors:

Zeledon R. Electrolysis Propulsion For Small-Scale Spacecraft . [Thesis]. Cornell University; 2015. Available from: http://hdl.handle.net/1813/40701

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


University of Colorado

27. Handzo, Ryan E. Satellite Navigation Using High Definition Television Signals.

Degree: MS, 2016, University of Colorado

Spacecraft operators can use a variety of observables to perform orbit determination throughout a mission. Currently the mission design community has an interest in… (more)

Subjects/Keywords: spacecraft navigation; satellites; HDTV; signals; Aerospace Engineering

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APA (6th Edition):

Handzo, R. E. (2016). Satellite Navigation Using High Definition Television Signals. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/189

Chicago Manual of Style (16th Edition):

Handzo, Ryan E. “Satellite Navigation Using High Definition Television Signals.” 2016. Masters Thesis, University of Colorado. Accessed August 08, 2020. https://scholar.colorado.edu/asen_gradetds/189.

MLA Handbook (7th Edition):

Handzo, Ryan E. “Satellite Navigation Using High Definition Television Signals.” 2016. Web. 08 Aug 2020.

Vancouver:

Handzo RE. Satellite Navigation Using High Definition Television Signals. [Internet] [Masters thesis]. University of Colorado; 2016. [cited 2020 Aug 08]. Available from: https://scholar.colorado.edu/asen_gradetds/189.

Council of Science Editors:

Handzo RE. Satellite Navigation Using High Definition Television Signals. [Masters Thesis]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/189


University of Toronto

28. Hiemstra, Jesse Mathew. Mechanical Design and Development of a Modular Drag Sail for the CanX-7 Nanosatellite Mission.

Degree: 2014, University of Toronto

The drag sail developed for the CanX-7 nanosatellite mission is an aerodynamic deorbiting device suited to small spacecraft. The drag sail enables spacecraft within a… (more)

Subjects/Keywords: Deorbiting; Drag sails; Nanosatellites; Spacecraft; 0538

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APA (6th Edition):

Hiemstra, J. M. (2014). Mechanical Design and Development of a Modular Drag Sail for the CanX-7 Nanosatellite Mission. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/68017

Chicago Manual of Style (16th Edition):

Hiemstra, Jesse Mathew. “Mechanical Design and Development of a Modular Drag Sail for the CanX-7 Nanosatellite Mission.” 2014. Masters Thesis, University of Toronto. Accessed August 08, 2020. http://hdl.handle.net/1807/68017.

MLA Handbook (7th Edition):

Hiemstra, Jesse Mathew. “Mechanical Design and Development of a Modular Drag Sail for the CanX-7 Nanosatellite Mission.” 2014. Web. 08 Aug 2020.

Vancouver:

Hiemstra JM. Mechanical Design and Development of a Modular Drag Sail for the CanX-7 Nanosatellite Mission. [Internet] [Masters thesis]. University of Toronto; 2014. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1807/68017.

Council of Science Editors:

Hiemstra JM. Mechanical Design and Development of a Modular Drag Sail for the CanX-7 Nanosatellite Mission. [Masters Thesis]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/68017


University of Michigan

29. Bell, Iverson C. A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities.

Degree: PhD, Electrical Engineering, 2015, University of Michigan

 The work presented in this thesis evaluates the potential of electrodynamic tether (EDT) propulsion technology to provide picosatellites (100 g–1 kg) and femtosatellites (<100 g)… (more)

Subjects/Keywords: electrodynamic tether; small spacecraft; Electrical Engineering; Engineering

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APA (6th Edition):

Bell, I. C. (2015). A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/113575

Chicago Manual of Style (16th Edition):

Bell, Iverson C. “A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities.” 2015. Doctoral Dissertation, University of Michigan. Accessed August 08, 2020. http://hdl.handle.net/2027.42/113575.

MLA Handbook (7th Edition):

Bell, Iverson C. “A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities.” 2015. Web. 08 Aug 2020.

Vancouver:

Bell IC. A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities. [Internet] [Doctoral dissertation]. University of Michigan; 2015. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/2027.42/113575.

Council of Science Editors:

Bell IC. A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities. [Doctoral Dissertation]. University of Michigan; 2015. Available from: http://hdl.handle.net/2027.42/113575


University of New South Wales

30. Biswas, Sanat. Computationally Efficient Non-linear Kalman Filters for On-board Space Vehicle Navigation.

Degree: Electrical Engineering & Telecommunications, 2017, University of New South Wales

 The Extended Kalman Filter (EKF) is the most popular non-linear estimation algorithm due to its computational efficiency. It is frequently used in on-board space vehicle… (more)

Subjects/Keywords: Navigation; Unscented Kalman Filter; GNSS; Spacecraft; Estimation

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APA (6th Edition):

Biswas, S. (2017). Computationally Efficient Non-linear Kalman Filters for On-board Space Vehicle Navigation. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/58357 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:45843/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Biswas, Sanat. “Computationally Efficient Non-linear Kalman Filters for On-board Space Vehicle Navigation.” 2017. Doctoral Dissertation, University of New South Wales. Accessed August 08, 2020. http://handle.unsw.edu.au/1959.4/58357 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:45843/SOURCE02?view=true.

MLA Handbook (7th Edition):

Biswas, Sanat. “Computationally Efficient Non-linear Kalman Filters for On-board Space Vehicle Navigation.” 2017. Web. 08 Aug 2020.

Vancouver:

Biswas S. Computationally Efficient Non-linear Kalman Filters for On-board Space Vehicle Navigation. [Internet] [Doctoral dissertation]. University of New South Wales; 2017. [cited 2020 Aug 08]. Available from: http://handle.unsw.edu.au/1959.4/58357 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:45843/SOURCE02?view=true.

Council of Science Editors:

Biswas S. Computationally Efficient Non-linear Kalman Filters for On-board Space Vehicle Navigation. [Doctoral Dissertation]. University of New South Wales; 2017. Available from: http://handle.unsw.edu.au/1959.4/58357 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:45843/SOURCE02?view=true

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