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You searched for subject:(orbit determination). Showing records 1 – 30 of 87 total matches.

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Delft University of Technology

1. Villamil, Sebastian (author). On the effect of laser altimeter crossover observables on orbit determination with the JUICE mission as case study.

Degree: 2019, Delft University of Technology

This thesis' work aims to evaluate the potential added benefit to spacecraft orbit determination procedures upon using non-conventional measurements for orbit reconstruction. As a spacecraft… (more)

Subjects/Keywords: orbit determination; crossovers; JUICE

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

APA (6th Edition):

Villamil, S. (. (2019). On the effect of laser altimeter crossover observables on orbit determination with the JUICE mission as case study. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d8a3326e-43d1-4797-8799-4b4456b76b18

Chicago Manual of Style (16th Edition):

Villamil, Sebastian (author). “On the effect of laser altimeter crossover observables on orbit determination with the JUICE mission as case study.” 2019. Masters Thesis, Delft University of Technology. Accessed May 09, 2021. http://resolver.tudelft.nl/uuid:d8a3326e-43d1-4797-8799-4b4456b76b18.

MLA Handbook (7th Edition):

Villamil, Sebastian (author). “On the effect of laser altimeter crossover observables on orbit determination with the JUICE mission as case study.” 2019. Web. 09 May 2021.

Vancouver:

Villamil S(. On the effect of laser altimeter crossover observables on orbit determination with the JUICE mission as case study. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 May 09]. Available from: http://resolver.tudelft.nl/uuid:d8a3326e-43d1-4797-8799-4b4456b76b18.

Council of Science Editors:

Villamil S(. On the effect of laser altimeter crossover observables on orbit determination with the JUICE mission as case study. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:d8a3326e-43d1-4797-8799-4b4456b76b18


University of Texas – Austin

2. Petsche, Clayton Jay. The distribution of Galois orbits of low height.

Degree: PhD, Mathematics, 2003, University of Texas – Austin

Subjects/Keywords: Orbit determination

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APA (6th Edition):

Petsche, C. J. (2003). The distribution of Galois orbits of low height. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/858

Chicago Manual of Style (16th Edition):

Petsche, Clayton Jay. “The distribution of Galois orbits of low height.” 2003. Doctoral Dissertation, University of Texas – Austin. Accessed May 09, 2021. http://hdl.handle.net/2152/858.

MLA Handbook (7th Edition):

Petsche, Clayton Jay. “The distribution of Galois orbits of low height.” 2003. Web. 09 May 2021.

Vancouver:

Petsche CJ. The distribution of Galois orbits of low height. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2003. [cited 2021 May 09]. Available from: http://hdl.handle.net/2152/858.

Council of Science Editors:

Petsche CJ. The distribution of Galois orbits of low height. [Doctoral Dissertation]. University of Texas – Austin; 2003. Available from: http://hdl.handle.net/2152/858


Virginia Tech

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

Degree: MS, Aerospace 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 (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 May 09, 2021. 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. 09 May 2021.

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 2021 May 09]. 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

4. 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 May 09, 2021. 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. 09 May 2021.

Vancouver:

Geeraert JL. Multi-Satellite Orbit Determination Using Interferometric Observables with RF Localization Applications. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2021 May 09]. 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


Delft University of Technology

5. Abdolhay, Hamid Reza (author). Planetary Ephemerides Generation From Interplanetary Laser Ranging Data.

Degree: 2018, Delft University of Technology

 With the introduction of Interplanetary Laser Ranging (ILR), the acquired tracking measurements accuracy of planets can be improved drastically (up to a few millimeters) which… (more)

Subjects/Keywords: Laser Ranging; Planetary Epehemerides; orbit determination

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APA (6th Edition):

Abdolhay, H. R. (. (2018). Planetary Ephemerides Generation From Interplanetary Laser Ranging Data. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:2903d222-5280-455b-859f-1aeb8289858f

Chicago Manual of Style (16th Edition):

Abdolhay, Hamid Reza (author). “Planetary Ephemerides Generation From Interplanetary Laser Ranging Data.” 2018. Masters Thesis, Delft University of Technology. Accessed May 09, 2021. http://resolver.tudelft.nl/uuid:2903d222-5280-455b-859f-1aeb8289858f.

MLA Handbook (7th Edition):

Abdolhay, Hamid Reza (author). “Planetary Ephemerides Generation From Interplanetary Laser Ranging Data.” 2018. Web. 09 May 2021.

Vancouver:

Abdolhay HR(. Planetary Ephemerides Generation From Interplanetary Laser Ranging Data. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 May 09]. Available from: http://resolver.tudelft.nl/uuid:2903d222-5280-455b-859f-1aeb8289858f.

Council of Science Editors:

Abdolhay HR(. Planetary Ephemerides Generation From Interplanetary Laser Ranging Data. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:2903d222-5280-455b-859f-1aeb8289858f


Delft University of Technology

6. Inamdar, Jayraj (author). Impact of Non-gravitational Forces on Magellan Orbit Determination: A Historic Mission To Venus.

Degree: 2018, Delft University of Technology

A detailed modeling of non-gravitational forces is an area that has been left unexplored in the past for orbit modeling of Magellan, primarily due to… (more)

Subjects/Keywords: orbit determination; Magellan mission; Venus; Orbit modeling; gravity recovery

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APA (6th Edition):

Inamdar, J. (. (2018). Impact of Non-gravitational Forces on Magellan Orbit Determination: A Historic Mission To Venus. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3dea56be-bdfb-4d0d-aabc-14b2cdace755

Chicago Manual of Style (16th Edition):

Inamdar, Jayraj (author). “Impact of Non-gravitational Forces on Magellan Orbit Determination: A Historic Mission To Venus.” 2018. Masters Thesis, Delft University of Technology. Accessed May 09, 2021. http://resolver.tudelft.nl/uuid:3dea56be-bdfb-4d0d-aabc-14b2cdace755.

MLA Handbook (7th Edition):

Inamdar, Jayraj (author). “Impact of Non-gravitational Forces on Magellan Orbit Determination: A Historic Mission To Venus.” 2018. Web. 09 May 2021.

Vancouver:

Inamdar J(. Impact of Non-gravitational Forces on Magellan Orbit Determination: A Historic Mission To Venus. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 May 09]. Available from: http://resolver.tudelft.nl/uuid:3dea56be-bdfb-4d0d-aabc-14b2cdace755.

Council of Science Editors:

Inamdar J(. Impact of Non-gravitational Forces on Magellan Orbit Determination: A Historic Mission To Venus. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:3dea56be-bdfb-4d0d-aabc-14b2cdace755


Luleå University of Technology

7. 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 May 09, 2021. 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. 09 May 2021.

Vancouver:

Reihs B. Orbit Determination for Space Surveillance. [Internet] [Thesis]. Luleå University of Technology; 2016. [cited 2021 May 09]. 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


Stellenbosch University

8. Rossouw, Nico Chris. A GPS-based on-board orbit propagator for low earth-orbiting CubeSats.

Degree: MEng, Electrical and Electronic Engineering, 2015, Stellenbosch University

ENGLISH ABSTRACT: On-board knowledge of satellite position is vital to all space missions. Due to the stringent power budgets of the CubeSat form factor, permanently… (more)

Subjects/Keywords: On-board orbit propagator; Orbit determination; Kalman filtering; Earth-orbiting CubeSats; UCTD

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APA (6th Edition):

Rossouw, N. C. (2015). A GPS-based on-board orbit propagator for low earth-orbiting CubeSats. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/97908

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):

Rossouw, Nico Chris. “A GPS-based on-board orbit propagator for low earth-orbiting CubeSats.” 2015. Thesis, Stellenbosch University. Accessed May 09, 2021. http://hdl.handle.net/10019.1/97908.

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

MLA Handbook (7th Edition):

Rossouw, Nico Chris. “A GPS-based on-board orbit propagator for low earth-orbiting CubeSats.” 2015. Web. 09 May 2021.

Vancouver:

Rossouw NC. A GPS-based on-board orbit propagator for low earth-orbiting CubeSats. [Internet] [Thesis]. Stellenbosch University; 2015. [cited 2021 May 09]. Available from: http://hdl.handle.net/10019.1/97908.

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

Council of Science Editors:

Rossouw NC. A GPS-based on-board orbit propagator for low earth-orbiting CubeSats. [Thesis]. Stellenbosch University; 2015. Available from: http://hdl.handle.net/10019.1/97908

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


University of Colorado

9. 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 May 09, 2021. 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. 09 May 2021.

Vancouver:

Jones BA. Efficient Models for the Evaluation and Estimation of the Gravity Field. [Internet] [Doctoral dissertation]. University of Colorado; 2010. [cited 2021 May 09]. 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


York University

10. 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 May 09, 2021. http://hdl.handle.net/10315/34568.

MLA Handbook (7th Edition):

Bijnens, Nicholas. “Satellite Orbit Determination Using Payload-Collected Observation Data.” 2018. Web. 09 May 2021.

Vancouver:

Bijnens N. Satellite Orbit Determination Using Payload-Collected Observation Data. [Internet] [Masters thesis]. York University; 2018. [cited 2021 May 09]. 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


Delft University of Technology

11. Brunt, Casper (author). Assessment of the LPS Ephemeris Accuracy using Inter-Satellite Linking.

Degree: 2020, Delft University of Technology

The number of Moon missions is increasing, but to facilitate these missions, an improved approach for lunar navigation is required. The proposed strategy is to… (more)

Subjects/Keywords: LPS; PECMEO; Navigation; Positioning; Orbit Determination; Constellation; Moon; Lunar; Inter-Satellite Links; Inter-Satellite Linking; Kinematic Orbit Determination; least-squares

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

APA (6th Edition):

Brunt, C. (. (2020). Assessment of the LPS Ephemeris Accuracy using Inter-Satellite Linking. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:fb364570-c3d3-47cc-963b-e1422d2dfbc5

Chicago Manual of Style (16th Edition):

Brunt, Casper (author). “Assessment of the LPS Ephemeris Accuracy using Inter-Satellite Linking.” 2020. Masters Thesis, Delft University of Technology. Accessed May 09, 2021. http://resolver.tudelft.nl/uuid:fb364570-c3d3-47cc-963b-e1422d2dfbc5.

MLA Handbook (7th Edition):

Brunt, Casper (author). “Assessment of the LPS Ephemeris Accuracy using Inter-Satellite Linking.” 2020. Web. 09 May 2021.

Vancouver:

Brunt C(. Assessment of the LPS Ephemeris Accuracy using Inter-Satellite Linking. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 May 09]. Available from: http://resolver.tudelft.nl/uuid:fb364570-c3d3-47cc-963b-e1422d2dfbc5.

Council of Science Editors:

Brunt C(. Assessment of the LPS Ephemeris Accuracy using Inter-Satellite Linking. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:fb364570-c3d3-47cc-963b-e1422d2dfbc5


Texas A&M University

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

Degree: MS, Aerospace Engineering, 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. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242

Chicago Manual of Style (16th Edition):

Schaeperkoetter, Andrew Vernon. “A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques.” 2012. Masters Thesis, Texas A&M University. Accessed May 09, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242.

MLA Handbook (7th Edition):

Schaeperkoetter, Andrew Vernon. “A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques.” 2012. Web. 09 May 2021.

Vancouver:

Schaeperkoetter AV. A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 May 09]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242.

Council of Science Editors:

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


Penn State University

13. Ciliberto, David. Extended Kalman Filtering in Burdet Coordinates for Orbit Determination.

Degree: 2019, Penn State University

 The objective of this thesis is to develop a formulation of the extended Kalman filter (EKF) in regularized coordinates for use in orbit determination. Regularizing… (more)

Subjects/Keywords: Kalman Filtering; Estimation; Orbit Determination; Space Situational Awareness; Regularization

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APA (6th Edition):

Ciliberto, D. (2019). Extended Kalman Filtering in Burdet Coordinates for Orbit Determination. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/16497dmc5758

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):

Ciliberto, David. “Extended Kalman Filtering in Burdet Coordinates for Orbit Determination.” 2019. Thesis, Penn State University. Accessed May 09, 2021. https://submit-etda.libraries.psu.edu/catalog/16497dmc5758.

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

MLA Handbook (7th Edition):

Ciliberto, David. “Extended Kalman Filtering in Burdet Coordinates for Orbit Determination.” 2019. Web. 09 May 2021.

Vancouver:

Ciliberto D. Extended Kalman Filtering in Burdet Coordinates for Orbit Determination. [Internet] [Thesis]. Penn State University; 2019. [cited 2021 May 09]. Available from: https://submit-etda.libraries.psu.edu/catalog/16497dmc5758.

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

Council of Science Editors:

Ciliberto D. Extended Kalman Filtering in Burdet Coordinates for Orbit Determination. [Thesis]. Penn State University; 2019. Available from: https://submit-etda.libraries.psu.edu/catalog/16497dmc5758

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


University of Toronto

14. 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 May 09, 2021. 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. 09 May 2021.

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 2021 May 09]. 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


Delft University of Technology

15. Peñarroya Rodriguez, Pelayo (author). Investigation of convex residual penalty functions for orbit determination.

Degree: 2017, Delft University of Technology

This thesis aims to assess how different convex penalty functions can be used in orbit determination methods and to design an algorithm to test them… (more)

Subjects/Keywords: convex functions; orbit determination; observations; robustness; penalty functions

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APA (6th Edition):

Peñarroya Rodriguez, P. (. (2017). Investigation of convex residual penalty functions for orbit determination. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3a185b36-12c2-48e5-ad30-63b8da44e110

Chicago Manual of Style (16th Edition):

Peñarroya Rodriguez, Pelayo (author). “Investigation of convex residual penalty functions for orbit determination.” 2017. Masters Thesis, Delft University of Technology. Accessed May 09, 2021. http://resolver.tudelft.nl/uuid:3a185b36-12c2-48e5-ad30-63b8da44e110.

MLA Handbook (7th Edition):

Peñarroya Rodriguez, Pelayo (author). “Investigation of convex residual penalty functions for orbit determination.” 2017. Web. 09 May 2021.

Vancouver:

Peñarroya Rodriguez P(. Investigation of convex residual penalty functions for orbit determination. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 May 09]. Available from: http://resolver.tudelft.nl/uuid:3a185b36-12c2-48e5-ad30-63b8da44e110.

Council of Science Editors:

Peñarroya Rodriguez P(. Investigation of convex residual penalty functions for orbit determination. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:3a185b36-12c2-48e5-ad30-63b8da44e110


University of Colorado

16. 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 May 09, 2021. 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. 09 May 2021.

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 2021 May 09]. 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


Delft University of Technology

17. Gurumoorthy, Ramanathan (author). CryoSat-2 precise orbit determination using DORIS phase measurements.

Degree: 2019, Delft University of Technology

CryoSat-2 is a European Space Agency (ESA) altimeter mission with an objective to study the connection between cryosphere melting and global sea level rise. The… (more)

Subjects/Keywords: Precise orbit determination (POD); DORIS; IDS; GEODYN-II; RINEX; Doppler

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APA (6th Edition):

Gurumoorthy, R. (. (2019). CryoSat-2 precise orbit determination using DORIS phase measurements. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:159d1c59-a4d8-4fcd-9cc8-7c1b3ba816c6

Chicago Manual of Style (16th Edition):

Gurumoorthy, Ramanathan (author). “CryoSat-2 precise orbit determination using DORIS phase measurements.” 2019. Masters Thesis, Delft University of Technology. Accessed May 09, 2021. http://resolver.tudelft.nl/uuid:159d1c59-a4d8-4fcd-9cc8-7c1b3ba816c6.

MLA Handbook (7th Edition):

Gurumoorthy, Ramanathan (author). “CryoSat-2 precise orbit determination using DORIS phase measurements.” 2019. Web. 09 May 2021.

Vancouver:

Gurumoorthy R(. CryoSat-2 precise orbit determination using DORIS phase measurements. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 May 09]. Available from: http://resolver.tudelft.nl/uuid:159d1c59-a4d8-4fcd-9cc8-7c1b3ba816c6.

Council of Science Editors:

Gurumoorthy R(. CryoSat-2 precise orbit determination using DORIS phase measurements. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:159d1c59-a4d8-4fcd-9cc8-7c1b3ba816c6


Delft University of Technology

18. Guindal Martínez, Alvaro (author). Precise absolute and relative navigation in Medium-Earth Orbits by means of Global Navigation Satellite Systems and Inter-Satellite Links.

Degree: 2020, Delft University of Technology

 The first close-up image of a black hole has been taken recently by means of a network of high-resolution telescopes situated all around the globe,… (more)

Subjects/Keywords: POD; GNSS; Inter-Satellite Links; Relative Navigation; Absolute Navigation; Orbit Determination

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APA (6th Edition):

Guindal Martínez, A. (. (2020). Precise absolute and relative navigation in Medium-Earth Orbits by means of Global Navigation Satellite Systems and Inter-Satellite Links. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f7dfe188-ceac-47cb-bf3a-0615e89f1785

Chicago Manual of Style (16th Edition):

Guindal Martínez, Alvaro (author). “Precise absolute and relative navigation in Medium-Earth Orbits by means of Global Navigation Satellite Systems and Inter-Satellite Links.” 2020. Masters Thesis, Delft University of Technology. Accessed May 09, 2021. http://resolver.tudelft.nl/uuid:f7dfe188-ceac-47cb-bf3a-0615e89f1785.

MLA Handbook (7th Edition):

Guindal Martínez, Alvaro (author). “Precise absolute and relative navigation in Medium-Earth Orbits by means of Global Navigation Satellite Systems and Inter-Satellite Links.” 2020. Web. 09 May 2021.

Vancouver:

Guindal Martínez A(. Precise absolute and relative navigation in Medium-Earth Orbits by means of Global Navigation Satellite Systems and Inter-Satellite Links. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 May 09]. Available from: http://resolver.tudelft.nl/uuid:f7dfe188-ceac-47cb-bf3a-0615e89f1785.

Council of Science Editors:

Guindal Martínez A(. Precise absolute and relative navigation in Medium-Earth Orbits by means of Global Navigation Satellite Systems and Inter-Satellite Links. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:f7dfe188-ceac-47cb-bf3a-0615e89f1785


Delft University of Technology

19. Lopez Jimenez, Sergi (author). New techniques for uncertainty realism improvement in Space Surveillance and Tracking orbit determination processes.

Degree: 2020, Delft University of Technology

 The future space environment is predicted to grow in number of both operational and inactive man-made objects and the era of constellations is expected to… (more)

Subjects/Keywords: Space Debris; SST; orbit determination; Covariance Analysis; covariance realism

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APA (6th Edition):

Lopez Jimenez, S. (. (2020). New techniques for uncertainty realism improvement in Space Surveillance and Tracking orbit determination processes. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c9c99702-aff5-40fd-b155-07a169281843

Chicago Manual of Style (16th Edition):

Lopez Jimenez, Sergi (author). “New techniques for uncertainty realism improvement in Space Surveillance and Tracking orbit determination processes.” 2020. Masters Thesis, Delft University of Technology. Accessed May 09, 2021. http://resolver.tudelft.nl/uuid:c9c99702-aff5-40fd-b155-07a169281843.

MLA Handbook (7th Edition):

Lopez Jimenez, Sergi (author). “New techniques for uncertainty realism improvement in Space Surveillance and Tracking orbit determination processes.” 2020. Web. 09 May 2021.

Vancouver:

Lopez Jimenez S(. New techniques for uncertainty realism improvement in Space Surveillance and Tracking orbit determination processes. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 May 09]. Available from: http://resolver.tudelft.nl/uuid:c9c99702-aff5-40fd-b155-07a169281843.

Council of Science Editors:

Lopez Jimenez S(. New techniques for uncertainty realism improvement in Space Surveillance and Tracking orbit determination processes. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:c9c99702-aff5-40fd-b155-07a169281843

20. 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 May 09, 2021. 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. 09 May 2021.

Vancouver:

Losada SO. Orbit determination of asteroids using streak information. [Internet] [Thesis]. Luleå University of Technology; 2020. [cited 2021 May 09]. 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


Delft University of Technology

21. 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 May 09, 2021. 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. 09 May 2021.

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 2021 May 09]. 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


Cal Poly

22. Stoker, Kyle. Initial Orbit Determination Error Analysis of Low-Earth Orbit Rocket Body Debris and Feasibility Study for Debris Cataloguing from One Optical Facility.

Degree: MS, Aerospace Engineering, 2020, Cal Poly

  This paper is predicated on determining the effectiveness of angles-only initial orbit determination (IOD) methods when limited observational data is available for low-Earth orbit(more)

Subjects/Keywords: initial orbit determination; debris; LEO; accuracy; optical observation; SpOT; Astrodynamics

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APA (6th Edition):

Stoker, K. (2020). Initial Orbit Determination Error Analysis of Low-Earth Orbit Rocket Body Debris and Feasibility Study for Debris Cataloguing from One Optical Facility. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2153 ; 10.15368/theses.2020.41

Chicago Manual of Style (16th Edition):

Stoker, Kyle. “Initial Orbit Determination Error Analysis of Low-Earth Orbit Rocket Body Debris and Feasibility Study for Debris Cataloguing from One Optical Facility.” 2020. Masters Thesis, Cal Poly. Accessed May 09, 2021. https://digitalcommons.calpoly.edu/theses/2153 ; 10.15368/theses.2020.41.

MLA Handbook (7th Edition):

Stoker, Kyle. “Initial Orbit Determination Error Analysis of Low-Earth Orbit Rocket Body Debris and Feasibility Study for Debris Cataloguing from One Optical Facility.” 2020. Web. 09 May 2021.

Vancouver:

Stoker K. Initial Orbit Determination Error Analysis of Low-Earth Orbit Rocket Body Debris and Feasibility Study for Debris Cataloguing from One Optical Facility. [Internet] [Masters thesis]. Cal Poly; 2020. [cited 2021 May 09]. Available from: https://digitalcommons.calpoly.edu/theses/2153 ; 10.15368/theses.2020.41.

Council of Science Editors:

Stoker K. Initial Orbit Determination Error Analysis of Low-Earth Orbit Rocket Body Debris and Feasibility Study for Debris Cataloguing from One Optical Facility. [Masters Thesis]. Cal Poly; 2020. Available from: https://digitalcommons.calpoly.edu/theses/2153 ; 10.15368/theses.2020.41


Delft University of Technology

23. Vancraen, Sander (author). COTS GNSS Receiver: Testing of an on-board receiver for the Indian Space Research Organisation satellite INS-1C.

Degree: 2021, Delft University of Technology

The Indian Space Research Organisation(ISRO) plans to equip future satellites of its Indian Nano Satellite(INS) with COTS dual frequency receivers in order to let them… (more)

Subjects/Keywords: GNSS receiver; Dual frequency receiver; CubeSats; NanoSat; GPS; Glonass; Orbit determination

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APA (6th Edition):

Vancraen, S. (. (2021). COTS GNSS Receiver: Testing of an on-board receiver for the Indian Space Research Organisation satellite INS-1C. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:751df0f0-6b9a-4b5b-9d54-51a44c347536

Chicago Manual of Style (16th Edition):

Vancraen, Sander (author). “COTS GNSS Receiver: Testing of an on-board receiver for the Indian Space Research Organisation satellite INS-1C.” 2021. Masters Thesis, Delft University of Technology. Accessed May 09, 2021. http://resolver.tudelft.nl/uuid:751df0f0-6b9a-4b5b-9d54-51a44c347536.

MLA Handbook (7th Edition):

Vancraen, Sander (author). “COTS GNSS Receiver: Testing of an on-board receiver for the Indian Space Research Organisation satellite INS-1C.” 2021. Web. 09 May 2021.

Vancouver:

Vancraen S(. COTS GNSS Receiver: Testing of an on-board receiver for the Indian Space Research Organisation satellite INS-1C. [Internet] [Masters thesis]. Delft University of Technology; 2021. [cited 2021 May 09]. Available from: http://resolver.tudelft.nl/uuid:751df0f0-6b9a-4b5b-9d54-51a44c347536.

Council of Science Editors:

Vancraen S(. COTS GNSS Receiver: Testing of an on-board receiver for the Indian Space Research Organisation satellite INS-1C. [Masters Thesis]. Delft University of Technology; 2021. Available from: http://resolver.tudelft.nl/uuid:751df0f0-6b9a-4b5b-9d54-51a44c347536


University of Kansas

24. 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 May 09, 2021. 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. 09 May 2021.

Vancouver:

Fattig E. Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2021 May 09]. 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

25. 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 (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 May 09, 2021. http://hdl.handle.net/1808/7650.

MLA Handbook (7th Edition):

Arudra, Anoop Kumar. “ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES.” 2011. Web. 09 May 2021.

Vancouver:

Arudra AK. ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2021 May 09]. 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 Colorado

26. 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 May 09, 2021. 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. 09 May 2021.

Vancouver:

Gehly S. Estimation of Geosynchronous Space Objects Using Finite Set Statistics Filtering Methods. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2021 May 09]. 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


Virginia Tech

27. 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 May 09, 2021. http://hdl.handle.net/10919/11155.

MLA Handbook (7th Edition):

Berry, Matthew M. “A Variable-Step Double-Integration Multi-Step Integrator.” 2004. Web. 09 May 2021.

Vancouver:

Berry MM. A Variable-Step Double-Integration Multi-Step Integrator. [Internet] [Doctoral dissertation]. Virginia Tech; 2004. [cited 2021 May 09]. 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


Uppsala University

28. 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 May 09, 2021. 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. 09 May 2021.

Vancouver:

Alinder S. Space Situational Awareness with the Swedish Allsky Meteor Network. [Internet] [Thesis]. Uppsala University; 2019. [cited 2021 May 09]. 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


York University

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

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 May 09, 2021. 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. 09 May 2021.

Vancouver:

Wright TJ. Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites. [Internet] [Masters thesis]. York University; 2015. [cited 2021 May 09]. 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

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

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 May 09, 2021. 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. 09 May 2021.

Vancouver:

Gomes VM. Determinação de órbita e manobras utilizando GPS e motor com baixo empuxo. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2008. [cited 2021 May 09]. 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

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