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You searched for subject:(orbit determination). Showing records 1 – 30 of 64 total matches.

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Virginia Tech

1. Keil, Elizabeth Marie. Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit.

Degree: MS, Aerospace and Ocean Engineering, 2014, Virginia Tech

 This thesis details the development and implementation of an attitude and orbit determining Kalman filter algorithm for a satellite in a Molniya orbit. To apply… (more)

Subjects/Keywords: Attitude; Orbit; Determination; Kalman Filter

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Keil, E. M. (2014). Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49102

Chicago Manual of Style (16th Edition):

Keil, Elizabeth Marie. “Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit.” 2014. Masters Thesis, Virginia Tech. Accessed March 28, 2020. http://hdl.handle.net/10919/49102.

MLA Handbook (7th Edition):

Keil, Elizabeth Marie. “Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit.” 2014. Web. 28 Mar 2020.

Vancouver:

Keil EM. Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/10919/49102.

Council of Science Editors:

Keil EM. Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/49102


University of Colorado

2. Geeraert, Jeroen L. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.

Degree: PhD, 2017, University of Colorado

  Very long baseline interferometry (VLBI) specifically same-beam interferometry (SBI), and dual-satellite geolocation are two fields of research not previously connected. This is due to… (more)

Subjects/Keywords: astrodynamics; geolocation; interferometry; orbit determination; Aerospace Engineering

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APA (6th Edition):

Geeraert, J. L. (2017). Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/192

Chicago Manual of Style (16th Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Doctoral Dissertation, University of Colorado. Accessed March 28, 2020. https://scholar.colorado.edu/asen_gradetds/192.

MLA Handbook (7th Edition):

Geeraert, Jeroen L. “Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications.” 2017. Web. 28 Mar 2020.

Vancouver:

Geeraert JL. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2020 Mar 28]. Available from: https://scholar.colorado.edu/asen_gradetds/192.

Council of Science Editors:

Geeraert JL. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/192


University of Kansas

3. Lechtenberg, Travis Francis. DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES.

Degree: MS, Aerospace Engineering, 2010, University of Kansas

 Several models of atmospheric density exist in today's world, yet most possess significant errors when compared to data determined from actual satellite measurements. This research… (more)

Subjects/Keywords: Aerospace engineering; Atmospheric density; Orbit determination; Precision orbit ephemerides; Satellite drag

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APA (6th Edition):

Lechtenberg, T. F. (2010). DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/6295

Chicago Manual of Style (16th Edition):

Lechtenberg, Travis Francis. “DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES.” 2010. Masters Thesis, University of Kansas. Accessed March 28, 2020. http://hdl.handle.net/1808/6295.

MLA Handbook (7th Edition):

Lechtenberg, Travis Francis. “DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES.” 2010. Web. 28 Mar 2020.

Vancouver:

Lechtenberg TF. DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/1808/6295.

Council of Science Editors:

Lechtenberg TF. DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES. [Masters Thesis]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/6295


Luleå University of Technology

4. Reihs, Benedikt. Orbit Determination for Space Surveillance.

Degree: 2016, Luleå University of Technology

This thesis presents the assessment of candidates for orbit determination (OD) within the realtime simulation SpaceView & Analyst, developed at Fraunhofer FHR. The goal… (more)

Subjects/Keywords: Technology; Space Surveillance; Orbit Determination; Distributed Sensors; Orbit Database; Teknik

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APA (6th Edition):

Reihs, B. (2016). Orbit Determination for Space Surveillance. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-45642

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):

Reihs, Benedikt. “Orbit Determination for Space Surveillance.” 2016. Thesis, Luleå University of Technology. Accessed March 28, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-45642.

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

MLA Handbook (7th Edition):

Reihs, Benedikt. “Orbit Determination for Space Surveillance.” 2016. Web. 28 Mar 2020.

Vancouver:

Reihs B. Orbit Determination for Space Surveillance. [Internet] [Thesis]. Luleå University of Technology; 2016. [cited 2020 Mar 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-45642.

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

Council of Science Editors:

Reihs B. Orbit Determination for Space Surveillance. [Thesis]. Luleå University of Technology; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-45642

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


Indian Institute of Science

5. Akila, S. Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy.

Degree: 2006, Indian Institute of Science

Orbit of a spacecraft in three dimensional Inertial Reference Frame is in general represented by a standard set of six parameters like Keplerian Orbital Elements… (more)

Subjects/Keywords: Orbit Models; Spacecraft Orbits; Dynamic Filters; Orbit Dynamics; Orbit Determination (OD); Orbit Propagation; Kalman Filter; Dynamics Filter Compensation (DFC); Astronautics

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APA (6th Edition):

Akila, S. (2006). Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/398

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):

Akila, S. “Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy.” 2006. Thesis, Indian Institute of Science. Accessed March 28, 2020. http://hdl.handle.net/2005/398.

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

MLA Handbook (7th Edition):

Akila, S. “Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy.” 2006. Web. 28 Mar 2020.

Vancouver:

Akila S. Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy. [Internet] [Thesis]. Indian Institute of Science; 2006. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/2005/398.

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

Council of Science Editors:

Akila S. Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy. [Thesis]. Indian Institute of Science; 2006. Available from: http://hdl.handle.net/2005/398

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


University of Colorado

6. Jones, Brandon Allan. Efficient Models for the Evaluation and Estimation of the Gravity Field.

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

  Current astrodynamics applications require a rapid evaluation of the gravity field and an efficient approach to gravity estimation. The commonly used spherical harmonic model… (more)

Subjects/Keywords: asteroid; gravity estimation; gravity modeling; orbit determination; orbit propagation; spherical harmonics; Aerospace Engineering; Astrodynamics

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APA (6th Edition):

Jones, B. A. (2010). Efficient Models for the Evaluation and Estimation of the Gravity Field. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/11

Chicago Manual of Style (16th Edition):

Jones, Brandon Allan. “Efficient Models for the Evaluation and Estimation of the Gravity Field.” 2010. Doctoral Dissertation, University of Colorado. Accessed March 28, 2020. https://scholar.colorado.edu/asen_gradetds/11.

MLA Handbook (7th Edition):

Jones, Brandon Allan. “Efficient Models for the Evaluation and Estimation of the Gravity Field.” 2010. Web. 28 Mar 2020.

Vancouver:

Jones BA. Efficient Models for the Evaluation and Estimation of the Gravity Field. [Internet] [Doctoral dissertation]. University of Colorado; 2010. [cited 2020 Mar 28]. Available from: https://scholar.colorado.edu/asen_gradetds/11.

Council of Science Editors:

Jones BA. Efficient Models for the Evaluation and Estimation of the Gravity Field. [Doctoral Dissertation]. University of Colorado; 2010. Available from: https://scholar.colorado.edu/asen_gradetds/11

7. Bijnens, Nicholas. Satellite Orbit Determination Using Payload-Collected Observation Data.

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

 The algorithm developed in this research provides a novel way of preparing the space industry for the future. The rapid rise in small satellite deployment… (more)

Subjects/Keywords: Aerospace engineering; Satellite; Orbit; Orbit determination; Machine learning; Genetic algorithm; AIS; Payload; Data; Observations

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APA (6th Edition):

Bijnens, N. (2018). Satellite Orbit Determination Using Payload-Collected Observation Data. (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/34568

Chicago Manual of Style (16th Edition):

Bijnens, Nicholas. “Satellite Orbit Determination Using Payload-Collected Observation Data.” 2018. Masters Thesis, York University. Accessed March 28, 2020. http://hdl.handle.net/10315/34568.

MLA Handbook (7th Edition):

Bijnens, Nicholas. “Satellite Orbit Determination Using Payload-Collected Observation Data.” 2018. Web. 28 Mar 2020.

Vancouver:

Bijnens N. Satellite Orbit Determination Using Payload-Collected Observation Data. [Internet] [Masters thesis]. York University; 2018. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/10315/34568.

Council of Science Editors:

Bijnens N. Satellite Orbit Determination Using Payload-Collected Observation Data. [Masters Thesis]. York University; 2018. Available from: http://hdl.handle.net/10315/34568


Texas A&M University

8. Schaeperkoetter, Andrew Vernon. A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques.

Degree: 2012, Texas A&M University

 During the last two centuries many methods have been proposed to solve the angles-only initial orbit determination problem. As this problem continues to be relevant… (more)

Subjects/Keywords: Initial Orbit Determination; Gooding; Double R; Gauss; Laplace

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APA (6th Edition):

Schaeperkoetter, A. V. (2012). A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242

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):

Schaeperkoetter, Andrew Vernon. “A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques.” 2012. Thesis, Texas A&M University. Accessed March 28, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242.

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

MLA Handbook (7th Edition):

Schaeperkoetter, Andrew Vernon. “A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques.” 2012. Web. 28 Mar 2020.

Vancouver:

Schaeperkoetter AV. A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242.

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

Council of Science Editors:

Schaeperkoetter AV. A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242

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


University of Kansas

9. Mance, Stephen. An Investigation into Satellite Drag Modeling Performance.

Degree: MS, Aerospace Engineering, 2010, University of Kansas

 The errors in current atmospheric drag modeling are the primary source of error for orbit determination for objects in low Earth orbit (LEO) at lower… (more)

Subjects/Keywords: Aerospace engineering; Atmospheric density; Ballistic coefficient; Orbit determination; Satellite drag; Thermosphere

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APA (6th Edition):

Mance, S. (2010). An Investigation into Satellite Drag Modeling Performance. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/6289

Chicago Manual of Style (16th Edition):

Mance, Stephen. “An Investigation into Satellite Drag Modeling Performance.” 2010. Masters Thesis, University of Kansas. Accessed March 28, 2020. http://hdl.handle.net/1808/6289.

MLA Handbook (7th Edition):

Mance, Stephen. “An Investigation into Satellite Drag Modeling Performance.” 2010. Web. 28 Mar 2020.

Vancouver:

Mance S. An Investigation into Satellite Drag Modeling Performance. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/1808/6289.

Council of Science Editors:

Mance S. An Investigation into Satellite Drag Modeling Performance. [Masters Thesis]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/6289


Delft University of Technology

10. Van Helleputte, T. The integration of spaceborne accelerometry in the precise orbit determination of low-flying satellites.

Degree: 2011, Delft University of Technology

This dissertation describes the integration of accelerometer measurements of LEO-satellites in GPS-based orbit determination. Advisors/Committee Members: Ambrosius, B.A.C..

Subjects/Keywords: orbit determination; GPS; accelerometry

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APA (6th Edition):

Van Helleputte, T. (2011). The integration of spaceborne accelerometry in the precise orbit determination of low-flying satellites. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; urn:NBN:nl:ui:24-uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; urn:NBN:nl:ui:24-uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; http://resolver.tudelft.nl/uuid:c84217a2-967c-45c4-85cb-a1630590b926

Chicago Manual of Style (16th Edition):

Van Helleputte, T. “The integration of spaceborne accelerometry in the precise orbit determination of low-flying satellites.” 2011. Doctoral Dissertation, Delft University of Technology. Accessed March 28, 2020. http://resolver.tudelft.nl/uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; urn:NBN:nl:ui:24-uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; urn:NBN:nl:ui:24-uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; http://resolver.tudelft.nl/uuid:c84217a2-967c-45c4-85cb-a1630590b926.

MLA Handbook (7th Edition):

Van Helleputte, T. “The integration of spaceborne accelerometry in the precise orbit determination of low-flying satellites.” 2011. Web. 28 Mar 2020.

Vancouver:

Van Helleputte T. The integration of spaceborne accelerometry in the precise orbit determination of low-flying satellites. [Internet] [Doctoral dissertation]. Delft University of Technology; 2011. [cited 2020 Mar 28]. Available from: http://resolver.tudelft.nl/uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; urn:NBN:nl:ui:24-uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; urn:NBN:nl:ui:24-uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; http://resolver.tudelft.nl/uuid:c84217a2-967c-45c4-85cb-a1630590b926.

Council of Science Editors:

Van Helleputte T. The integration of spaceborne accelerometry in the precise orbit determination of low-flying satellites. [Doctoral Dissertation]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; urn:NBN:nl:ui:24-uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; urn:NBN:nl:ui:24-uuid:c84217a2-967c-45c4-85cb-a1630590b926 ; http://resolver.tudelft.nl/uuid:c84217a2-967c-45c4-85cb-a1630590b926


University of Colorado

11. Lubey, Daniel Patrick. Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator.

Degree: PhD, Aerospace Engineering Sciences, 2015, University of Colorado

  The Big Sky Theory once posited that the volume of Earth's orbital environment is so large that the chance of a collision ever occurring… (more)

Subjects/Keywords: orbit determination; state estimation; OCBE; ballistic; smoother; Aerospace Engineering

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APA (6th Edition):

Lubey, D. P. (2015). Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/114

Chicago Manual of Style (16th Edition):

Lubey, Daniel Patrick. “Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator.” 2015. Doctoral Dissertation, University of Colorado. Accessed March 28, 2020. https://scholar.colorado.edu/asen_gradetds/114.

MLA Handbook (7th Edition):

Lubey, Daniel Patrick. “Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator.” 2015. Web. 28 Mar 2020.

Vancouver:

Lubey DP. Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2020 Mar 28]. Available from: https://scholar.colorado.edu/asen_gradetds/114.

Council of Science Editors:

Lubey DP. Maneuver Detection and Reconstruction in Data Sparse Systems with an Optimal Control Based Estimator. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/114


University of Toronto

12. Tarantini, Vincent. Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite.

Degree: 2012, University of Toronto

Contributions to two missions are presented. The first is a demonstration mission called CanX-7 that uses a 4 square metre drag sail to de-orbit a… (more)

Subjects/Keywords: De-orbit; Drag sail; Thermal control; Attitude determination and control; 0538

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APA (6th Edition):

Tarantini, V. (2012). Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/33557

Chicago Manual of Style (16th Edition):

Tarantini, Vincent. “Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite.” 2012. Masters Thesis, University of Toronto. Accessed March 28, 2020. http://hdl.handle.net/1807/33557.

MLA Handbook (7th Edition):

Tarantini, Vincent. “Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite.” 2012. Web. 28 Mar 2020.

Vancouver:

Tarantini V. Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite. [Internet] [Masters thesis]. University of Toronto; 2012. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/1807/33557.

Council of Science Editors:

Tarantini V. Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite. [Masters Thesis]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/33557

13. Losada, Samuel Ocana. Orbit determination of asteroids using streak information.

Degree: Space Technology, 2020, Luleå University of Technology

  Asteroids are becoming a stepping stone for the human space exploration,as much as they are a threat for human life on Earth. Several agencies… (more)

Subjects/Keywords: asteroids; orbit determination; streaks; trailed observations; Aerospace Engineering; Rymd- och flygteknik

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APA (6th Edition):

Losada, S. O. (2020). Orbit determination of asteroids using streak information. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-78092

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):

Losada, Samuel Ocana. “Orbit determination of asteroids using streak information.” 2020. Thesis, Luleå University of Technology. Accessed March 28, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-78092.

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

MLA Handbook (7th Edition):

Losada, Samuel Ocana. “Orbit determination of asteroids using streak information.” 2020. Web. 28 Mar 2020.

Vancouver:

Losada SO. Orbit determination of asteroids using streak information. [Internet] [Thesis]. Luleå University of Technology; 2020. [cited 2020 Mar 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-78092.

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

Council of Science Editors:

Losada SO. Orbit determination of asteroids using streak information. [Thesis]. Luleå University of Technology; 2020. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-78092

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


University of Kansas

14. Fattig, Eric. Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites.

Degree: MS, Aerospace Engineering, 2011, University of Kansas

 Current atmospheric density models cannot adequately represent the density variations observed by satellites in Low Earth Orbit (LEO). Using an optimal orbit determination process, precision… (more)

Subjects/Keywords: Aerospace engineering; Atmospheric density; Champ satellite; Grace satellites; Orbit determination; Precision orbit data; Solar and geomagnetic activity

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APA (6th Edition):

Fattig, E. (2011). Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/7653

Chicago Manual of Style (16th Edition):

Fattig, Eric. “Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites.” 2011. Masters Thesis, University of Kansas. Accessed March 28, 2020. http://hdl.handle.net/1808/7653.

MLA Handbook (7th Edition):

Fattig, Eric. “Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites.” 2011. Web. 28 Mar 2020.

Vancouver:

Fattig E. Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/1808/7653.

Council of Science Editors:

Fattig E. Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites. [Masters Thesis]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/7653


University of Kansas

15. Arudra, Anoop Kumar. ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES.

Degree: MS, Aerospace Engineering, 2011, University of Kansas

 The current atmospheric density models are not capable enough to accurately model the atmospheric density, which varies continuously in the upper atmosphere mainly due to… (more)

Subjects/Keywords: Aerospace engineering; Atmospheric density; Atmospheric density models; Orbit determination; Precision orbit ephemerides; Satellite drag; Space weather

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Arudra, A. K. (2011). ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/7650

Chicago Manual of Style (16th Edition):

Arudra, Anoop Kumar. “ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES.” 2011. Masters Thesis, University of Kansas. Accessed March 28, 2020. http://hdl.handle.net/1808/7650.

MLA Handbook (7th Edition):

Arudra, Anoop Kumar. “ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES.” 2011. Web. 28 Mar 2020.

Vancouver:

Arudra AK. ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/1808/7650.

Council of Science Editors:

Arudra AK. ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES. [Masters Thesis]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/7650


University of Kansas

16. Hiatt, Andrew Timothy. Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides.

Degree: MS, Aerospace Engineering, 2009, University of Kansas

 Current atmospheric models are incapable of properly modeling all of the density variations in the Earth’s upper atmosphere. Precision orbit ephemerides (POE) are utilized in… (more)

Subjects/Keywords: Aerospace engineering; Atmospheric density estimates; Champ; Grace; Orbit determination; Precision orbit ephemerides; Thermospheric and exospheric density

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Hiatt, A. T. (2009). Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/4553

Chicago Manual of Style (16th Edition):

Hiatt, Andrew Timothy. “Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides.” 2009. Masters Thesis, University of Kansas. Accessed March 28, 2020. http://hdl.handle.net/1808/4553.

MLA Handbook (7th Edition):

Hiatt, Andrew Timothy. “Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides.” 2009. Web. 28 Mar 2020.

Vancouver:

Hiatt AT. Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides. [Internet] [Masters thesis]. University of Kansas; 2009. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/1808/4553.

Council of Science Editors:

Hiatt AT. Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides. [Masters Thesis]. University of Kansas; 2009. Available from: http://hdl.handle.net/1808/4553


Virginia Tech

17. Berry, Matthew M. A Variable-Step Double-Integration Multi-Step Integrator.

Degree: PhD, Aerospace and Ocean Engineering, 2004, Virginia Tech

 A new method of numerical integration is presented here, the variable-step Stormer-Cowell method. The method uses error control to regulate the step size, so larger… (more)

Subjects/Keywords: Variable-Step Integration; Orbit Propagation; Orbit Determination; Numerical Integration

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APA (6th Edition):

Berry, M. M. (2004). A Variable-Step Double-Integration Multi-Step Integrator. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/11155

Chicago Manual of Style (16th Edition):

Berry, Matthew M. “A Variable-Step Double-Integration Multi-Step Integrator.” 2004. Doctoral Dissertation, Virginia Tech. Accessed March 28, 2020. http://hdl.handle.net/10919/11155.

MLA Handbook (7th Edition):

Berry, Matthew M. “A Variable-Step Double-Integration Multi-Step Integrator.” 2004. Web. 28 Mar 2020.

Vancouver:

Berry MM. A Variable-Step Double-Integration Multi-Step Integrator. [Internet] [Doctoral dissertation]. Virginia Tech; 2004. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/10919/11155.

Council of Science Editors:

Berry MM. A Variable-Step Double-Integration Multi-Step Integrator. [Doctoral Dissertation]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/11155


University of Colorado

18. Gehly, Steven. Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods.

Degree: PhD, Aerospace Engineering Sciences, 2016, University of Colorado

 The use of near Earth space has increased dramatically in the past few decades, and operational satellites are an integral part of modern society. The… (more)

Subjects/Keywords: Geosynchronous Orbit; Information Gain; Initial Orbit Determination; Multitarget Filtering; Random Finite Sets; Sensor Allocation; Aerospace Engineering

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APA (6th Edition):

Gehly, S. (2016). Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/148

Chicago Manual of Style (16th Edition):

Gehly, Steven. “Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods.” 2016. Doctoral Dissertation, University of Colorado. Accessed March 28, 2020. https://scholar.colorado.edu/asen_gradetds/148.

MLA Handbook (7th Edition):

Gehly, Steven. “Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods.” 2016. Web. 28 Mar 2020.

Vancouver:

Gehly S. Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2020 Mar 28]. Available from: https://scholar.colorado.edu/asen_gradetds/148.

Council of Science Editors:

Gehly S. Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods. [Doctoral Dissertation]. University of Colorado; 2016. Available from: https://scholar.colorado.edu/asen_gradetds/148


Uppsala University

19. Alinder, Simon. Space Situational Awareness with the Swedish Allsky Meteor Network.

Degree: Observational Astronomy, 2019, Uppsala University

This thesis investigates the use of the Swedish Allsky Meteor Network (SAMN) for observing, identifying, and determining the orbits of satellites. The overall goal… (more)

Subjects/Keywords: SSA; space situational awareness; IOD; initial orbit determination; orbit determination; satellite identification; all-sky; rymdlägessituation; SSA; omloppsbana; banbestämning; Astronomy, Astrophysics and Cosmology; Astronomi, astrofysik och kosmologi

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APA (6th Edition):

Alinder, S. (2019). Space Situational Awareness with the Swedish Allsky Meteor Network. (Thesis). Uppsala University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-390397

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):

Alinder, Simon. “Space Situational Awareness with the Swedish Allsky Meteor Network.” 2019. Thesis, Uppsala University. Accessed March 28, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-390397.

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

MLA Handbook (7th Edition):

Alinder, Simon. “Space Situational Awareness with the Swedish Allsky Meteor Network.” 2019. Web. 28 Mar 2020.

Vancouver:

Alinder S. Space Situational Awareness with the Swedish Allsky Meteor Network. [Internet] [Thesis]. Uppsala University; 2019. [cited 2020 Mar 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-390397.

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

Council of Science Editors:

Alinder S. Space Situational Awareness with the Swedish Allsky Meteor Network. [Thesis]. Uppsala University; 2019. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-390397

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

20. Wright, Thomas Jonathan. Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites.

Degree: MSc -MS, Earth & Space Science, 2015, York University

 Attitude and orbit determination are critical parts of nanosatellite mission operations. The ability to perform attitude and orbit determination autonomously could lead to a wider… (more)

Subjects/Keywords: Aerospace engineering; SGP4; Orbit determination; Attitude determination; Nanosatellite; Satellite; Extended Kalman Filter; Magnetometer; Magnetic field; IGRF

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APA (6th Edition):

Wright, T. J. (2015). Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites. (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/28288

Chicago Manual of Style (16th Edition):

Wright, Thomas Jonathan. “Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites.” 2015. Masters Thesis, York University. Accessed March 28, 2020. http://hdl.handle.net/10315/28288.

MLA Handbook (7th Edition):

Wright, Thomas Jonathan. “Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites.” 2015. Web. 28 Mar 2020.

Vancouver:

Wright TJ. Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites. [Internet] [Masters thesis]. York University; 2015. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/10315/28288.

Council of Science Editors:

Wright TJ. Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites. [Masters Thesis]. York University; 2015. Available from: http://hdl.handle.net/10315/28288

21. Vivian Martins Gomes. Determinação de órbita e manobras utilizando GPS e motor com baixo empuxo.

Degree: 2008, Instituto Nacional de Pesquisas Espaciais

The Global Positioning System (GPS) is a satellite navigation system that allows the users to determine 3D positioning and the time with high precision. Its… (more)

Subjects/Keywords: determinação de órbita; manobras orbitais; filtro de Kalman; satélites artificiais; astrodinâmica; orbit determination; orbital maneuvers

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APA (6th Edition):

Gomes, V. M. (2008). Determinação de órbita e manobras utilizando GPS e motor com baixo empuxo. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2008/08.11.15.18

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):

Gomes, Vivian Martins. “Determinação de órbita e manobras utilizando GPS e motor com baixo empuxo.” 2008. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed March 28, 2020. http://urlib.net/sid.inpe.br/[email protected]/2008/08.11.15.18.

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

MLA Handbook (7th Edition):

Gomes, Vivian Martins. “Determinação de órbita e manobras utilizando GPS e motor com baixo empuxo.” 2008. Web. 28 Mar 2020.

Vancouver:

Gomes VM. Determinação de órbita e manobras utilizando GPS e motor com baixo empuxo. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2008. [cited 2020 Mar 28]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2008/08.11.15.18.

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

Council of Science Editors:

Gomes VM. Determinação de órbita e manobras utilizando GPS e motor com baixo empuxo. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2008. Available from: http://urlib.net/sid.inpe.br/[email protected]/2008/08.11.15.18

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


Texas A&M University

22. Karimi, Reza. Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets.

Degree: 2012, Texas A&M University

 A perfect duality exists between the problem of space-based orbit determination from line-of-sight measurements and the problem of designing an interplanetary autonomous navigation system. Mathematically,… (more)

Subjects/Keywords: Initial Orbit Determination; Spacecraft Navigation; Extended Kalman Filter; Light-time correction; light Aberration

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APA (6th Edition):

Karimi, R. (2012). Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11084

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):

Karimi, Reza. “Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets.” 2012. Thesis, Texas A&M University. Accessed March 28, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11084.

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

MLA Handbook (7th Edition):

Karimi, Reza. “Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets.” 2012. Web. 28 Mar 2020.

Vancouver:

Karimi R. Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11084.

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

Council of Science Editors:

Karimi R. Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11084

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


University of Southern California

23. Llanos de la Concha, Pedro J. Trajectory mission design and navigation for a space weather forecast.

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

 This thesis research will be based on the trajectory mission design and navigation design for prospective future missions to the Triangular Lagrange Points L5 and… (more)

Subjects/Keywords: trajectory mission design; navigation; orbit determination; maneuver analysis; Sun-Earth triangular points; astronautics; space physics

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APA (6th Edition):

Llanos de la Concha, P. J. (2012). Trajectory mission design and navigation for a space weather forecast. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/30564/rec/7555

Chicago Manual of Style (16th Edition):

Llanos de la Concha, Pedro J. “Trajectory mission design and navigation for a space weather forecast.” 2012. Doctoral Dissertation, University of Southern California. Accessed March 28, 2020. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/30564/rec/7555.

MLA Handbook (7th Edition):

Llanos de la Concha, Pedro J. “Trajectory mission design and navigation for a space weather forecast.” 2012. Web. 28 Mar 2020.

Vancouver:

Llanos de la Concha PJ. Trajectory mission design and navigation for a space weather forecast. [Internet] [Doctoral dissertation]. University of Southern California; 2012. [cited 2020 Mar 28]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/30564/rec/7555.

Council of Science Editors:

Llanos de la Concha PJ. Trajectory mission design and navigation for a space weather forecast. [Doctoral Dissertation]. University of Southern California; 2012. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/30564/rec/7555

24. Verma, Ashok Kumar. Improvement of the planetary ephemerides using spacecraft navigation data and its application to fundamental physics : Exploitation scientifique des données de navigation des sondes spatiales pour l'amélioration des éphémérides planétaires et applications.

Degree: Docteur es, Astrophysique, 2013, Besançon

Les éphémérides planétaires jouent un rôle important pour la navigation des missions spatiales actuelles et la mise en place des missions futures ainsi que la… (more)

Subjects/Keywords: Éphémérides planétaires; Navigation; Relativité générale; Couronne solaire; Solar corona; General relativity; Radioscience; Orbit determination; 520

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APA (6th Edition):

Verma, A. K. (2013). Improvement of the planetary ephemerides using spacecraft navigation data and its application to fundamental physics : Exploitation scientifique des données de navigation des sondes spatiales pour l'amélioration des éphémérides planétaires et applications. (Doctoral Dissertation). Besançon. Retrieved from http://www.theses.fr/2013BESA2030

Chicago Manual of Style (16th Edition):

Verma, Ashok Kumar. “Improvement of the planetary ephemerides using spacecraft navigation data and its application to fundamental physics : Exploitation scientifique des données de navigation des sondes spatiales pour l'amélioration des éphémérides planétaires et applications.” 2013. Doctoral Dissertation, Besançon. Accessed March 28, 2020. http://www.theses.fr/2013BESA2030.

MLA Handbook (7th Edition):

Verma, Ashok Kumar. “Improvement of the planetary ephemerides using spacecraft navigation data and its application to fundamental physics : Exploitation scientifique des données de navigation des sondes spatiales pour l'amélioration des éphémérides planétaires et applications.” 2013. Web. 28 Mar 2020.

Vancouver:

Verma AK. Improvement of the planetary ephemerides using spacecraft navigation data and its application to fundamental physics : Exploitation scientifique des données de navigation des sondes spatiales pour l'amélioration des éphémérides planétaires et applications. [Internet] [Doctoral dissertation]. Besançon; 2013. [cited 2020 Mar 28]. Available from: http://www.theses.fr/2013BESA2030.

Council of Science Editors:

Verma AK. Improvement of the planetary ephemerides using spacecraft navigation data and its application to fundamental physics : Exploitation scientifique des données de navigation des sondes spatiales pour l'amélioration des éphémérides planétaires et applications. [Doctoral Dissertation]. Besançon; 2013. Available from: http://www.theses.fr/2013BESA2030


University of Colorado

25. Dietrich, Ann Brown. Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies.

Degree: PhD, 2017, University of Colorado

 Spacecraft navigation in proximity to small celestial bodies, such as asteroids and comets, is challenging due to their complex dynamical environment and the lag in… (more)

Subjects/Keywords: lidar; orbit determination; small bodies; autonomous navigation; least-squares filter; Aerospace Engineering; Theory and Algorithms

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APA (6th Edition):

Dietrich, A. B. (2017). Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/215

Chicago Manual of Style (16th Edition):

Dietrich, Ann Brown. “Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies.” 2017. Doctoral Dissertation, University of Colorado. Accessed March 28, 2020. https://scholar.colorado.edu/asen_gradetds/215.

MLA Handbook (7th Edition):

Dietrich, Ann Brown. “Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies.” 2017. Web. 28 Mar 2020.

Vancouver:

Dietrich AB. Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2020 Mar 28]. Available from: https://scholar.colorado.edu/asen_gradetds/215.

Council of Science Editors:

Dietrich AB. Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/215


University of Colorado

26. McMahon, Jay Warren. An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.

Degree: PhD, Aerospace Engineering Sciences, 2011, University of Colorado

  Solar radiation pressure is the largest non-gravitational perturbation for most satellites in the solar system, and can therefore have a significant influence on their… (more)

Subjects/Keywords: astrodynamics; BYORP; celestial mechanics; orbital dynamics; orbit determination; solar radiation pressure; Aerospace Engineering; Astrodynamics

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APA (6th Edition):

McMahon, J. W. (2011). An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/26

Chicago Manual of Style (16th Edition):

McMahon, Jay Warren. “An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.” 2011. Doctoral Dissertation, University of Colorado. Accessed March 28, 2020. https://scholar.colorado.edu/asen_gradetds/26.

MLA Handbook (7th Edition):

McMahon, Jay Warren. “An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites.” 2011. Web. 28 Mar 2020.

Vancouver:

McMahon JW. An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites. [Internet] [Doctoral dissertation]. University of Colorado; 2011. [cited 2020 Mar 28]. Available from: https://scholar.colorado.edu/asen_gradetds/26.

Council of Science Editors:

McMahon JW. An Analytical Theory for the Perturbative Effect of Solar Radiation Pressure on Natural and Artificial Satellites. [Doctoral Dissertation]. University of Colorado; 2011. Available from: https://scholar.colorado.edu/asen_gradetds/26


University of Colorado

27. Dietrich, Ann Brown. Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies.

Degree: PhD, Aerospace Engineering Sciences, 2017, University of Colorado

 Spacecraft navigation in proximity to small celestial bodies, such as asteroids and comets, is challenging due to their complex dynamical environment and the lag in… (more)

Subjects/Keywords: Lidar; orbit determination; Small bodies; Aerospace Engineering; Astrodynamics; Navigation, Guidance, Control and Dynamics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Dietrich, A. B. (2017). Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/178

Chicago Manual of Style (16th Edition):

Dietrich, Ann Brown. “Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies.” 2017. Doctoral Dissertation, University of Colorado. Accessed March 28, 2020. https://scholar.colorado.edu/asen_gradetds/178.

MLA Handbook (7th Edition):

Dietrich, Ann Brown. “Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies.” 2017. Web. 28 Mar 2020.

Vancouver:

Dietrich AB. Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2020 Mar 28]. Available from: https://scholar.colorado.edu/asen_gradetds/178.

Council of Science Editors:

Dietrich AB. Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/178


University of Colorado

28. Leonard, Jason Michael. Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.

Degree: PhD, Aerospace Engineering Sciences, 2015, University of Colorado

  Crewed navigation in certain regions of the Earth-Moon system provides a unique challenge due to the unstable dynamics and observation geometry relative to standard… (more)

Subjects/Keywords: Autonomous Navigation; Navigation; Orbit Determination; Stochastic Processes; Navigation, Guidance, Control and Dynamics; Space Vehicles

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APA (6th Edition):

Leonard, J. M. (2015). Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/97

Chicago Manual of Style (16th Edition):

Leonard, Jason Michael. “Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.” 2015. Doctoral Dissertation, University of Colorado. Accessed March 28, 2020. https://scholar.colorado.edu/asen_gradetds/97.

MLA Handbook (7th Edition):

Leonard, Jason Michael. “Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.” 2015. Web. 28 Mar 2020.

Vancouver:

Leonard JM. Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2020 Mar 28]. Available from: https://scholar.colorado.edu/asen_gradetds/97.

Council of Science Editors:

Leonard JM. Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/97

29. Schwieger, Felix. Orbit Determination for UWE-4 based on Magnetometer and Sun Sensor Data using Equinoctial Orbital Elements.

Degree: Electrical and Space Engineering, 2017, Luleå University of Technology

  An autonomous, real-time orbit determination system was developed within thiswork for the next iteration of the University of W¨urzburg’s CubeSat programme.The algorithm only made… (more)

Subjects/Keywords: Extended Kalman Filter; Orbit Determination; UWE-4; Magnetometer; Sun Sensor; Aerospace Engineering; Rymd- och flygteknik

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Schwieger, F. (2017). Orbit Determination for UWE-4 based on Magnetometer and Sun Sensor Data using Equinoctial Orbital Elements. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61551

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):

Schwieger, Felix. “Orbit Determination for UWE-4 based on Magnetometer and Sun Sensor Data using Equinoctial Orbital Elements.” 2017. Thesis, Luleå University of Technology. Accessed March 28, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61551.

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

MLA Handbook (7th Edition):

Schwieger, Felix. “Orbit Determination for UWE-4 based on Magnetometer and Sun Sensor Data using Equinoctial Orbital Elements.” 2017. Web. 28 Mar 2020.

Vancouver:

Schwieger F. Orbit Determination for UWE-4 based on Magnetometer and Sun Sensor Data using Equinoctial Orbital Elements. [Internet] [Thesis]. Luleå University of Technology; 2017. [cited 2020 Mar 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61551.

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

Council of Science Editors:

Schwieger F. Orbit Determination for UWE-4 based on Magnetometer and Sun Sensor Data using Equinoctial Orbital Elements. [Thesis]. Luleå University of Technology; 2017. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61551

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


Stellenbosch University

30. Du Plessis, Jan Abraham Francois. Low earth orbit satellite propagators.

Degree: M.Ing., Electrical and Electronic Engineering, 1999, Stellenbosch University

ENGLISH ABSTRACT: The objective of this study was to implement an orbital propagation algorithm, which could be used for the purpose of mission planning and… (more)

Subjects/Keywords: Orbits; Artificial satellites; Dissertations  – Electronic engineering; Satellite orbit predictions; Orbit determination algorithms

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Du Plessis, J. A. F. (1999). Low earth orbit satellite propagators. (Masters Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/51326

Chicago Manual of Style (16th Edition):

Du Plessis, Jan Abraham Francois. “Low earth orbit satellite propagators.” 1999. Masters Thesis, Stellenbosch University. Accessed March 28, 2020. http://hdl.handle.net/10019.1/51326.

MLA Handbook (7th Edition):

Du Plessis, Jan Abraham Francois. “Low earth orbit satellite propagators.” 1999. Web. 28 Mar 2020.

Vancouver:

Du Plessis JAF. Low earth orbit satellite propagators. [Internet] [Masters thesis]. Stellenbosch University; 1999. [cited 2020 Mar 28]. Available from: http://hdl.handle.net/10019.1/51326.

Council of Science Editors:

Du Plessis JAF. Low earth orbit satellite propagators. [Masters Thesis]. Stellenbosch University; 1999. Available from: http://hdl.handle.net/10019.1/51326

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