Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(Attitude AND Orbit Control). Showing records 1 – 20 of 20 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


University of Toronto

1. Ibrahim, Najmus. Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.

Degree: 2013, University of Toronto

Terrestrial target tracking using low Earth orbit satellites provides essential daily services and vital scientific data. In this thesis, the Attitude and Orbit Control System… (more)

Subjects/Keywords: satellite; attitude; attitude and orbit control; microsatellite; control; estimation; tracking; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ibrahim, N. (2013). Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/42965

Chicago Manual of Style (16th Edition):

Ibrahim, Najmus. “Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.” 2013. Masters Thesis, University of Toronto. Accessed March 07, 2021. http://hdl.handle.net/1807/42965.

MLA Handbook (7th Edition):

Ibrahim, Najmus. “Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.” 2013. Web. 07 Mar 2021.

Vancouver:

Ibrahim N. Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1807/42965.

Council of Science Editors:

Ibrahim N. Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/42965


University of Toronto

2. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 07, 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. 07 Mar 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 Mar 07]. 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

3. Trullas Ballester, Marc (author). Asteroid Mission Guidance and Control using Dual Quaternions.

Degree: 2018, Delft University of Technology

The investigation of small bodies in the Solar System such as asteroids and comets is of increasing interest to the space exploration community for scientific… (more)

Subjects/Keywords: Asteroids; Dual Quaternions; Control; Attitude; Pose; Quaternions; Landing; Hover; Orbit

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Trullas Ballester, M. (. (2018). Asteroid Mission Guidance and Control using Dual Quaternions. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:49257a61-5d9e-402d-acde-e82ef5fa6ed8

Chicago Manual of Style (16th Edition):

Trullas Ballester, Marc (author). “Asteroid Mission Guidance and Control using Dual Quaternions.” 2018. Masters Thesis, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:49257a61-5d9e-402d-acde-e82ef5fa6ed8.

MLA Handbook (7th Edition):

Trullas Ballester, Marc (author). “Asteroid Mission Guidance and Control using Dual Quaternions.” 2018. Web. 07 Mar 2021.

Vancouver:

Trullas Ballester M(. Asteroid Mission Guidance and Control using Dual Quaternions. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:49257a61-5d9e-402d-acde-e82ef5fa6ed8.

Council of Science Editors:

Trullas Ballester M(. Asteroid Mission Guidance and Control using Dual Quaternions. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:49257a61-5d9e-402d-acde-e82ef5fa6ed8


Delft University of Technology

4. Crepy-Marglais, Jean-Daniel (author). Development of a Robust and Combined Controller for On-Orbit Servicing Missions.

Degree: 2018, Delft University of Technology

Nowadays, a satellite is considered as out of range forever once it is launched. This may soon no longer hold thanks to on-orbit servicing. However,… (more)

Subjects/Keywords: space robotics; on-orbit servicing; Control; H-infinity control; Attitude control; Robotics; loop shaping; combined control; robust control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Crepy-Marglais, J. (. (2018). Development of a Robust and Combined Controller for On-Orbit Servicing Missions. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f163745c-e9d9-4b22-9e5b-1f4d3790ebf6

Chicago Manual of Style (16th Edition):

Crepy-Marglais, Jean-Daniel (author). “Development of a Robust and Combined Controller for On-Orbit Servicing Missions.” 2018. Masters Thesis, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:f163745c-e9d9-4b22-9e5b-1f4d3790ebf6.

MLA Handbook (7th Edition):

Crepy-Marglais, Jean-Daniel (author). “Development of a Robust and Combined Controller for On-Orbit Servicing Missions.” 2018. Web. 07 Mar 2021.

Vancouver:

Crepy-Marglais J(. Development of a Robust and Combined Controller for On-Orbit Servicing Missions. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:f163745c-e9d9-4b22-9e5b-1f4d3790ebf6.

Council of Science Editors:

Crepy-Marglais J(. Development of a Robust and Combined Controller for On-Orbit Servicing Missions. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:f163745c-e9d9-4b22-9e5b-1f4d3790ebf6


University of Toronto

5. Hakima, Houman. A New Approach to Active Removal of Space Debris.

Degree: PhD, 2020, University of Toronto

 As a result of human space activities for over sixty years, there exist numerous man-made debris objects in the Earth orbits. Such objects not only… (more)

Subjects/Keywords: Active Debris Removal; Attitude and Orbit Control; Attitude Dynamics; Deorbiter CubeSat; Orbital Dynamics; Space Debris; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hakima, H. (2020). A New Approach to Active Removal of Space Debris. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/101359

Chicago Manual of Style (16th Edition):

Hakima, Houman. “A New Approach to Active Removal of Space Debris.” 2020. Doctoral Dissertation, University of Toronto. Accessed March 07, 2021. http://hdl.handle.net/1807/101359.

MLA Handbook (7th Edition):

Hakima, Houman. “A New Approach to Active Removal of Space Debris.” 2020. Web. 07 Mar 2021.

Vancouver:

Hakima H. A New Approach to Active Removal of Space Debris. [Internet] [Doctoral dissertation]. University of Toronto; 2020. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1807/101359.

Council of Science Editors:

Hakima H. A New Approach to Active Removal of Space Debris. [Doctoral Dissertation]. University of Toronto; 2020. Available from: http://hdl.handle.net/1807/101359


Virginia Tech

6. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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 07, 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. 07 Mar 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 Mar 07]. 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

7. Quinsac, Gary. From commercials off-the-shelf to expected propulsion in nanosatellites : Utilisation de composants sur étagère pour la propulsion des nanosatellites : à quel prix ?.

Degree: Docteur es, Astronomie et Astrophysique, 2019, Paris Sciences et Lettres (ComUE)

L’apparition du standard CubeSat a profondément modifié le domaine des nano/microsatellites, notamment en promouvant la standardisation, des développements plus courts et des lancements partagés. L’intérêt… (more)

Subjects/Keywords: CubeSat; Nanosatellite; Propulsion; Attitude; Orbite; Scao; Cubesat; Nanosatellite; Propulsion; Attitude; Orbit; Aocs; 520

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Quinsac, G. (2019). From commercials off-the-shelf to expected propulsion in nanosatellites : Utilisation de composants sur étagère pour la propulsion des nanosatellites : à quel prix ?. (Doctoral Dissertation). Paris Sciences et Lettres (ComUE). Retrieved from http://www.theses.fr/2019PSLEO004

Chicago Manual of Style (16th Edition):

Quinsac, Gary. “From commercials off-the-shelf to expected propulsion in nanosatellites : Utilisation de composants sur étagère pour la propulsion des nanosatellites : à quel prix ?.” 2019. Doctoral Dissertation, Paris Sciences et Lettres (ComUE). Accessed March 07, 2021. http://www.theses.fr/2019PSLEO004.

MLA Handbook (7th Edition):

Quinsac, Gary. “From commercials off-the-shelf to expected propulsion in nanosatellites : Utilisation de composants sur étagère pour la propulsion des nanosatellites : à quel prix ?.” 2019. Web. 07 Mar 2021.

Vancouver:

Quinsac G. From commercials off-the-shelf to expected propulsion in nanosatellites : Utilisation de composants sur étagère pour la propulsion des nanosatellites : à quel prix ?. [Internet] [Doctoral dissertation]. Paris Sciences et Lettres (ComUE); 2019. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2019PSLEO004.

Council of Science Editors:

Quinsac G. From commercials off-the-shelf to expected propulsion in nanosatellites : Utilisation de composants sur étagère pour la propulsion des nanosatellites : à quel prix ?. [Doctoral Dissertation]. Paris Sciences et Lettres (ComUE); 2019. Available from: http://www.theses.fr/2019PSLEO004


Linköping University

8. Elfving, Jonas. Attitude and Orbit Control for Small Satellites.

Degree: Electrical Engineering, 2002, Linköping University

  A satellite in orbit about a planet needs some means of attitude control in order to, for instance, get as much sun into its… (more)

Subjects/Keywords: Reglerteknik; satellites; attitude; orbit; control; Kalman estimation filters; quaternions; stabilization; pointing accuracy; Reglerteknik; Automatic control; Reglerteknik

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Elfving, J. (2002). Attitude and Orbit Control for Small Satellites. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-1407

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):

Elfving, Jonas. “Attitude and Orbit Control for Small Satellites.” 2002. Thesis, Linköping University. Accessed March 07, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-1407.

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

MLA Handbook (7th Edition):

Elfving, Jonas. “Attitude and Orbit Control for Small Satellites.” 2002. Web. 07 Mar 2021.

Vancouver:

Elfving J. Attitude and Orbit Control for Small Satellites. [Internet] [Thesis]. Linköping University; 2002. [cited 2021 Mar 07]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-1407.

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

Council of Science Editors:

Elfving J. Attitude and Orbit Control for Small Satellites. [Thesis]. Linköping University; 2002. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-1407

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

9. Flodin, Linus. Attitude and Orbit Control During Deorbit of Tethered Space Debris.

Degree: Aeronautical and Vehicle Engineering, 2015, KTH

Due to the unsustainable space debris environment in Low Earth Orbit, debris objects must be removed to ensure future safe satellite operations. One proposed… (more)

Subjects/Keywords: space debris mitigation; deorbit; tethered satellites; mathematical modeling; attitude and orbit control system; LQG control; PID control; switched control

…converted to the SCB frame to be properly saturated. B. Attitude control The main purpose of the… …Figure 13. The discrete time PID controller used for attitude control. Chaser FME x Ftether… …feedforward control is required both in the relative position controller and in the attitude… …in the simulator. 2) Attitude control: Feedforward in the attitude controller is… …engines used for deorbit burns, the chaser is equipped with a Reaction Control System (RCS… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Flodin, L. (2015). Attitude and Orbit Control During Deorbit of Tethered Space Debris. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-166824

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):

Flodin, Linus. “Attitude and Orbit Control During Deorbit of Tethered Space Debris.” 2015. Thesis, KTH. Accessed March 07, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-166824.

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

MLA Handbook (7th Edition):

Flodin, Linus. “Attitude and Orbit Control During Deorbit of Tethered Space Debris.” 2015. Web. 07 Mar 2021.

Vancouver:

Flodin L. Attitude and Orbit Control During Deorbit of Tethered Space Debris. [Internet] [Thesis]. KTH; 2015. [cited 2021 Mar 07]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-166824.

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

Council of Science Editors:

Flodin L. Attitude and Orbit Control During Deorbit of Tethered Space Debris. [Thesis]. KTH; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-166824

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

10. Adriano Marto Reis. Simulação distribuída em tempo-real de um sistema de controle de atitude e órbita para a plataforma multi-missão utilizando a arquitetura HLA.

Degree: 2009, Instituto Nacional de Pesquisas Espaciais

Neste trabalho apresenta-se o estudo e o desenvolvimento de uma simulação distribuída em Tempo Real de um Sistema de Controle de Atitude e de Órbita… (more)

Subjects/Keywords: simulação distribuída; simulação em tempo real; high level architecture (HLA); controle de atitude; órbita; plataforma multi-missão; distributed simulation; real time simulation; high level archicture (HLA); attitude control; orbit; multi-mission platform

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Reis, A. M. (2009). Simulação distribuída em tempo-real de um sistema de controle de atitude e órbita para a plataforma multi-missão utilizando a arquitetura HLA. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2009/03.02.22.17

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):

Reis, Adriano Marto. “Simulação distribuída em tempo-real de um sistema de controle de atitude e órbita para a plataforma multi-missão utilizando a arquitetura HLA.” 2009. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed March 07, 2021. http://urlib.net/sid.inpe.br/[email protected]/2009/03.02.22.17.

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

MLA Handbook (7th Edition):

Reis, Adriano Marto. “Simulação distribuída em tempo-real de um sistema de controle de atitude e órbita para a plataforma multi-missão utilizando a arquitetura HLA.” 2009. Web. 07 Mar 2021.

Vancouver:

Reis AM. Simulação distribuída em tempo-real de um sistema de controle de atitude e órbita para a plataforma multi-missão utilizando a arquitetura HLA. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. [cited 2021 Mar 07]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/03.02.22.17.

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

Council of Science Editors:

Reis AM. Simulação distribuída em tempo-real de um sistema de controle de atitude e órbita para a plataforma multi-missão utilizando a arquitetura HLA. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/03.02.22.17

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


Cal Poly

11. Bowen, John Arthur. On-Board Orbit Determination and 3-Axis Attitude Determination for Picosatellite Applications.

Degree: MS, Aerospace Engineering, 2009, Cal Poly

 This thesis outlines an orbit determination and 3-axis attitude determination system for use on orbit as applicable to 1U CubeSats and other picosatellites. The constraints… (more)

Subjects/Keywords: orbit determination; attitude determination; CubeSat; picosatellite; IGRF; TRIAD; Navigation, Guidance, Control and Dynamics; Space Vehicles

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bowen, J. A. (2009). On-Board Orbit Determination and 3-Axis Attitude Determination for Picosatellite Applications. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/131 ; 10.15368/theses.2009.114

Chicago Manual of Style (16th Edition):

Bowen, John Arthur. “On-Board Orbit Determination and 3-Axis Attitude Determination for Picosatellite Applications.” 2009. Masters Thesis, Cal Poly. Accessed March 07, 2021. https://digitalcommons.calpoly.edu/theses/131 ; 10.15368/theses.2009.114.

MLA Handbook (7th Edition):

Bowen, John Arthur. “On-Board Orbit Determination and 3-Axis Attitude Determination for Picosatellite Applications.” 2009. Web. 07 Mar 2021.

Vancouver:

Bowen JA. On-Board Orbit Determination and 3-Axis Attitude Determination for Picosatellite Applications. [Internet] [Masters thesis]. Cal Poly; 2009. [cited 2021 Mar 07]. Available from: https://digitalcommons.calpoly.edu/theses/131 ; 10.15368/theses.2009.114.

Council of Science Editors:

Bowen JA. On-Board Orbit Determination and 3-Axis Attitude Determination for Picosatellite Applications. [Masters Thesis]. Cal Poly; 2009. Available from: https://digitalcommons.calpoly.edu/theses/131 ; 10.15368/theses.2009.114


Stellenbosch University

12. Kearney, Mike-Alec. A thermal simulation tool for CubeSats for dynamic in-orbit scenarios, verified with flight data from the nSight-1 mission.

Degree: MEng, Mechanical and Mechatronic Engineering, 2020, Stellenbosch University

ENGLISH ABSTRACT: Thermal analysis is one of the aspects of designing CubeSats that has historically received less attention than more directly mission critical aspects such… (more)

Subjects/Keywords: Cubesats; Artificial satellites  – Attitude; Thermal analysis  – Simulation methods; Temperature measurements; nSight-1  – Orbit; UCTD

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Kearney, M. (2020). A thermal simulation tool for CubeSats for dynamic in-orbit scenarios, verified with flight data from the nSight-1 mission. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/108309

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):

Kearney, Mike-Alec. “A thermal simulation tool for CubeSats for dynamic in-orbit scenarios, verified with flight data from the nSight-1 mission.” 2020. Thesis, Stellenbosch University. Accessed March 07, 2021. http://hdl.handle.net/10019.1/108309.

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

MLA Handbook (7th Edition):

Kearney, Mike-Alec. “A thermal simulation tool for CubeSats for dynamic in-orbit scenarios, verified with flight data from the nSight-1 mission.” 2020. Web. 07 Mar 2021.

Vancouver:

Kearney M. A thermal simulation tool for CubeSats for dynamic in-orbit scenarios, verified with flight data from the nSight-1 mission. [Internet] [Thesis]. Stellenbosch University; 2020. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10019.1/108309.

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

Council of Science Editors:

Kearney M. A thermal simulation tool for CubeSats for dynamic in-orbit scenarios, verified with flight data from the nSight-1 mission. [Thesis]. Stellenbosch University; 2020. Available from: http://hdl.handle.net/10019.1/108309

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

13. Carmen Miranda de Lira Silva. Estimação conjunta de órbita e atitude de satélites artificiais estabilizados por rotação utilizando observações do magnetômetro e sensor solar.

Degree: 2005, Instituto Nacional de Pesquisas Espaciais (INPE)

Neste trabalho desenvolve-se e testa-se, sistematicamente, um procedimento de estimação conjunta de órbita e atitude destinado a satélites artificiais estabilizados por rotação em órbitas baixas.… (more)

Subjects/Keywords: satélite artificiais; magnetômetros; sensor solar; órbita; atitude; filtro kalman; artificial satellites; magnetometer; solar sensors; orbit; attitude; filter of Kalman

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Silva, C. M. d. L. (2005). Estimação conjunta de órbita e atitude de satélites artificiais estabilizados por rotação utilizando observações do magnetômetro e sensor solar. (Thesis). Instituto Nacional de Pesquisas Espaciais (INPE). Retrieved from http://urlib.net/sid.inpe.br/jeferson/2005/06.15.17.32

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):

Silva, Carmen Miranda de Lira. “Estimação conjunta de órbita e atitude de satélites artificiais estabilizados por rotação utilizando observações do magnetômetro e sensor solar.” 2005. Thesis, Instituto Nacional de Pesquisas Espaciais (INPE). Accessed March 07, 2021. http://urlib.net/sid.inpe.br/jeferson/2005/06.15.17.32.

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

MLA Handbook (7th Edition):

Silva, Carmen Miranda de Lira. “Estimação conjunta de órbita e atitude de satélites artificiais estabilizados por rotação utilizando observações do magnetômetro e sensor solar.” 2005. Web. 07 Mar 2021.

Vancouver:

Silva CMdL. Estimação conjunta de órbita e atitude de satélites artificiais estabilizados por rotação utilizando observações do magnetômetro e sensor solar. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais (INPE); 2005. [cited 2021 Mar 07]. Available from: http://urlib.net/sid.inpe.br/jeferson/2005/06.15.17.32.

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

Council of Science Editors:

Silva CMdL. Estimação conjunta de órbita e atitude de satélites artificiais estabilizados por rotação utilizando observações do magnetômetro e sensor solar. [Thesis]. Instituto Nacional de Pesquisas Espaciais (INPE); 2005. Available from: http://urlib.net/sid.inpe.br/jeferson/2005/06.15.17.32

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


York University

14. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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 March 07, 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. 07 Mar 2021.

Vancouver:

Wright TJ. Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites. [Internet] [Masters thesis]. York University; 2015. [cited 2021 Mar 07]. 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

15. Garcia, Erick Flores. Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos.

Degree: Space Technology, 2017, Luleå University of Technology

  Asteroid missions are gaining interest from the scientific community and many new missions are planned. The Didymos binary asteroid is a Near-Earth Object and… (more)

Subjects/Keywords: Solar System; Small celestial bodies; CubeSat; Attitude Determination Control Systems; Orbit Disturbances; Other Electrical Engineering, Electronic Engineering, Information Engineering; Annan elektroteknik och elektronik

…qn Abbreviations ADCS Attitude Determination and Control System AIDA Asteroid Impact and… …attitude accuracy and orbit stability to successfully complete its objective. A preliminary study… …maneuvering, observational filtering, spacecraft guidance and attitude control for deep space… …consists of determining the orbit and attitude of a spacecraft at any time, as well as the… …and attitude control of a spacecraft. [27, 9] An example, capable of supporting… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Garcia, E. F. (2017). Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-62007

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):

Garcia, Erick Flores. “Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos.” 2017. Thesis, Luleå University of Technology. Accessed March 07, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-62007.

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

MLA Handbook (7th Edition):

Garcia, Erick Flores. “Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos.” 2017. Web. 07 Mar 2021.

Vancouver:

Garcia EF. Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos. [Internet] [Thesis]. Luleå University of Technology; 2017. [cited 2021 Mar 07]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-62007.

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

Council of Science Editors:

Garcia EF. Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos. [Thesis]. Luleå University of Technology; 2017. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-62007

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


Cornell University

16. Jung, Hee. ESTIMATION PROBLEMS FOR SATELLITE ORBIT AND ATTITUDE DETERMINATION AND FOR GPS-BASED REMOTE IONOSPHERIC SENSING.

Degree: 2005, Cornell University

 Three separate applications of estimation problems in satellite navigation and attitude determination and in ionospheric scintillation monitoring have been solved numerically. The first application is… (more)

Subjects/Keywords: Optimal Estimation; GPS; Orbit Determination; Attitude Determination; Extended Kalman Filter; Semi-Codeless Algorithm

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Jung, H. (2005). ESTIMATION PROBLEMS FOR SATELLITE ORBIT AND ATTITUDE DETERMINATION AND FOR GPS-BASED REMOTE IONOSPHERIC SENSING. (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/2097

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):

Jung, Hee. “ESTIMATION PROBLEMS FOR SATELLITE ORBIT AND ATTITUDE DETERMINATION AND FOR GPS-BASED REMOTE IONOSPHERIC SENSING.” 2005. Thesis, Cornell University. Accessed March 07, 2021. http://hdl.handle.net/1813/2097.

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

MLA Handbook (7th Edition):

Jung, Hee. “ESTIMATION PROBLEMS FOR SATELLITE ORBIT AND ATTITUDE DETERMINATION AND FOR GPS-BASED REMOTE IONOSPHERIC SENSING.” 2005. Web. 07 Mar 2021.

Vancouver:

Jung H. ESTIMATION PROBLEMS FOR SATELLITE ORBIT AND ATTITUDE DETERMINATION AND FOR GPS-BASED REMOTE IONOSPHERIC SENSING. [Internet] [Thesis]. Cornell University; 2005. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1813/2097.

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

Council of Science Editors:

Jung H. ESTIMATION PROBLEMS FOR SATELLITE ORBIT AND ATTITUDE DETERMINATION AND FOR GPS-BASED REMOTE IONOSPHERIC SENSING. [Thesis]. Cornell University; 2005. Available from: http://hdl.handle.net/1813/2097

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


Delft University of Technology

17. Chaves Jimenez, A. On the Coupling of Orbit and Attitude Determination of Satellite Formations from Atmospheric Drag: Observability and Estimation Performance.

Degree: 2020, Delft University of Technology

 Spacecraft orbit and attitude dynamics have been classically seen as two separated subjects, since the effect of attitude in orbit dynamics was deemed too small… (more)

Subjects/Keywords: Orbit attitude coupling; estimation; spacecraft relative dynamics; Observability Gramian; Extended Kalman Filter

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chaves Jimenez, A. (2020). On the Coupling of Orbit and Attitude Determination of Satellite Formations from Atmospheric Drag: Observability and Estimation Performance. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; urn:NBN:nl:ui:24-uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; c333497d-05ac-422f-9688-31246a6fa7b1 ; 10.4233/uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; urn:isbn:978-94-028-2095-9 ; urn:NBN:nl:ui:24-uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; http://resolver.tudelft.nl/uuid:c333497d-05ac-422f-9688-31246a6fa7b1

Chicago Manual of Style (16th Edition):

Chaves Jimenez, A. “On the Coupling of Orbit and Attitude Determination of Satellite Formations from Atmospheric Drag: Observability and Estimation Performance.” 2020. Doctoral Dissertation, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; urn:NBN:nl:ui:24-uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; c333497d-05ac-422f-9688-31246a6fa7b1 ; 10.4233/uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; urn:isbn:978-94-028-2095-9 ; urn:NBN:nl:ui:24-uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; http://resolver.tudelft.nl/uuid:c333497d-05ac-422f-9688-31246a6fa7b1.

MLA Handbook (7th Edition):

Chaves Jimenez, A. “On the Coupling of Orbit and Attitude Determination of Satellite Formations from Atmospheric Drag: Observability and Estimation Performance.” 2020. Web. 07 Mar 2021.

Vancouver:

Chaves Jimenez A. On the Coupling of Orbit and Attitude Determination of Satellite Formations from Atmospheric Drag: Observability and Estimation Performance. [Internet] [Doctoral dissertation]. Delft University of Technology; 2020. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; urn:NBN:nl:ui:24-uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; c333497d-05ac-422f-9688-31246a6fa7b1 ; 10.4233/uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; urn:isbn:978-94-028-2095-9 ; urn:NBN:nl:ui:24-uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; http://resolver.tudelft.nl/uuid:c333497d-05ac-422f-9688-31246a6fa7b1.

Council of Science Editors:

Chaves Jimenez A. On the Coupling of Orbit and Attitude Determination of Satellite Formations from Atmospheric Drag: Observability and Estimation Performance. [Doctoral Dissertation]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; urn:NBN:nl:ui:24-uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; c333497d-05ac-422f-9688-31246a6fa7b1 ; 10.4233/uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; urn:isbn:978-94-028-2095-9 ; urn:NBN:nl:ui:24-uuid:c333497d-05ac-422f-9688-31246a6fa7b1 ; http://resolver.tudelft.nl/uuid:c333497d-05ac-422f-9688-31246a6fa7b1


Delft University of Technology

18. Andrés de la Fuente, J.I. Enhanced modelling of LAGEOS non-gravitational perturbations.

Degree: 2007, Delft University of Technology

Subjects/Keywords: attitude dynamics; plasma physics; radiation theory; heat transfer; perturbation theory; orbit determination

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Andrés de la Fuente, J. I. (2007). Enhanced modelling of LAGEOS non-gravitational perturbations. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; urn:NBN:nl:ui:24-uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; urn:NBN:nl:ui:24-uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; http://resolver.tudelft.nl/uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62

Chicago Manual of Style (16th Edition):

Andrés de la Fuente, J I. “Enhanced modelling of LAGEOS non-gravitational perturbations.” 2007. Doctoral Dissertation, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; urn:NBN:nl:ui:24-uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; urn:NBN:nl:ui:24-uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; http://resolver.tudelft.nl/uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62.

MLA Handbook (7th Edition):

Andrés de la Fuente, J I. “Enhanced modelling of LAGEOS non-gravitational perturbations.” 2007. Web. 07 Mar 2021.

Vancouver:

Andrés de la Fuente JI. Enhanced modelling of LAGEOS non-gravitational perturbations. [Internet] [Doctoral dissertation]. Delft University of Technology; 2007. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; urn:NBN:nl:ui:24-uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; urn:NBN:nl:ui:24-uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; http://resolver.tudelft.nl/uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62.

Council of Science Editors:

Andrés de la Fuente JI. Enhanced modelling of LAGEOS non-gravitational perturbations. [Doctoral Dissertation]. Delft University of Technology; 2007. Available from: http://resolver.tudelft.nl/uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; urn:NBN:nl:ui:24-uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; urn:NBN:nl:ui:24-uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62 ; http://resolver.tudelft.nl/uuid:bc15128e-6bfe-4992-962e-3c5f0a22ac62


York University

19. Dave, Siddharth Ghanshyam. Design and Prototype of a Phased-Array Antenna for Nanosatellite Radar and Communication Applications.

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

 Reconfigurable software defined radios are capable of altering radio frequency parameters of a transceiver to add functionality and improve performance. Initially static by design, reconfigurable… (more)

Subjects/Keywords: Engineering; Alternating Current; Attitude Control System; Analog to Digital Converter; Antenna Under Test; Digital to Analog Converter; Decibels; Direct Current; Electromagnetic waves; Field Programmable Gate Array; Global Positioning System; High Frequency Simulation Software; Integrated Circuits; Intermediate Frequency; Low Earth Orbit; Left Hand Circular Polarization; Linear Polarization; Micro-electromechanical Systems; Phased Array Antenna; Printed Circuit Board; Reference Antenna; Radio Frequency; Right Hand Circular Polarization; Resident Space Objects; Space based Space Surveillance; Software-defined Radio; Satellite Laser Ranging; Sub-miniature version A connector; Signal to Noise Ratio; Space Surveillance Network; Ultra High Frequencies; Very High Frequency; Vector Network Analyzer; Reconfigurability; Micro-strip; Substrate; Array; Feed network; Centre Frequency; Relative Dielectric Permittivity; Speed of Light; Wave Factor; Wavelength; Conductivity; Impedance Function; Impedance; Voltage; Current; Length of Micro-strip; Width of Micro-strip

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Dave, S. G. (2018). Design and Prototype of a Phased-Array Antenna for Nanosatellite Radar and Communication Applications. (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/35523

Chicago Manual of Style (16th Edition):

Dave, Siddharth Ghanshyam. “Design and Prototype of a Phased-Array Antenna for Nanosatellite Radar and Communication Applications.” 2018. Masters Thesis, York University. Accessed March 07, 2021. http://hdl.handle.net/10315/35523.

MLA Handbook (7th Edition):

Dave, Siddharth Ghanshyam. “Design and Prototype of a Phased-Array Antenna for Nanosatellite Radar and Communication Applications.” 2018. Web. 07 Mar 2021.

Vancouver:

Dave SG. Design and Prototype of a Phased-Array Antenna for Nanosatellite Radar and Communication Applications. [Internet] [Masters thesis]. York University; 2018. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10315/35523.

Council of Science Editors:

Dave SG. Design and Prototype of a Phased-Array Antenna for Nanosatellite Radar and Communication Applications. [Masters Thesis]. York University; 2018. Available from: http://hdl.handle.net/10315/35523

20. Hawe, Benjamin. Analysis of Passive Attitude Stabilisation and Deorbiting of Satellites in Low Earth Orbit.

Degree: Electrical and Space Engineering, 2016, Luleå University of Technology

  Orbital debris poses a serious threat to ongoing operations in space.  Recognising this threat, the European Commission has funded the three-year Technology for Self… (more)

Subjects/Keywords: electrodynamic; electrodynamic tether; EDT; drag augmentation; drag sail; drag balloon; passive attitude stabilisation; passive; attitude; stability; low earth orbit; LEO; deorbit; de-orbit; Post Mission Disposal; TeSeR; Aerospace Engineering; Rymd- och flygteknik

…the author’s internship within the Attitude and Orbit Control Systems/Guidance Navigation… …suggesting that active current control circuitry is required to prevent in-orbit-plane libration… …attitude stabilisation of the test satellite, the possibility to actively control the satellite… …4.3. EDTs Figure 5 shows the attitude of the satellite in an 800 km orbit with a 500 metre… …satellite in an 800 km equatorial orbit with a 500 metre EDT. Figure 6: Attitude of satellite in… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hawe, B. (2016). Analysis of Passive Attitude Stabilisation and Deorbiting of Satellites in Low Earth Orbit. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-60323

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):

Hawe, Benjamin. “Analysis of Passive Attitude Stabilisation and Deorbiting of Satellites in Low Earth Orbit.” 2016. Thesis, Luleå University of Technology. Accessed March 07, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-60323.

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

MLA Handbook (7th Edition):

Hawe, Benjamin. “Analysis of Passive Attitude Stabilisation and Deorbiting of Satellites in Low Earth Orbit.” 2016. Web. 07 Mar 2021.

Vancouver:

Hawe B. Analysis of Passive Attitude Stabilisation and Deorbiting of Satellites in Low Earth Orbit. [Internet] [Thesis]. Luleå University of Technology; 2016. [cited 2021 Mar 07]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-60323.

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

Council of Science Editors:

Hawe B. Analysis of Passive Attitude Stabilisation and Deorbiting of Satellites in Low Earth Orbit. [Thesis]. Luleå University of Technology; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-60323

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

.