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You searched for subject:(Attitude determination). Showing records 1 – 30 of 84 total matches.

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Purdue University

1. Bruce, Adam Lloyd. Statistical Characterization of Attitude Determination Algorithms Using Two Noisy Vector Measurements.

Degree: MSin Aeronautics and Astronautics, Aeronautics and Astronautics, 2016, Purdue University

Using Monte Carlo simulations, we analyze the statistical characteristics of three Advisors/Committee Members: Carolin Frueh, David Filmer, Stephen Collicott.

Subjects/Keywords: attitude determination

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APA (6th Edition):

Bruce, A. L. (2016). Statistical Characterization of Attitude Determination Algorithms Using Two Noisy Vector Measurements. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/1236

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):

Bruce, Adam Lloyd. “Statistical Characterization of Attitude Determination Algorithms Using Two Noisy Vector Measurements.” 2016. Thesis, Purdue University. Accessed November 25, 2020. https://docs.lib.purdue.edu/open_access_theses/1236.

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

MLA Handbook (7th Edition):

Bruce, Adam Lloyd. “Statistical Characterization of Attitude Determination Algorithms Using Two Noisy Vector Measurements.” 2016. Web. 25 Nov 2020.

Vancouver:

Bruce AL. Statistical Characterization of Attitude Determination Algorithms Using Two Noisy Vector Measurements. [Internet] [Thesis]. Purdue University; 2016. [cited 2020 Nov 25]. Available from: https://docs.lib.purdue.edu/open_access_theses/1236.

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

Council of Science Editors:

Bruce AL. Statistical Characterization of Attitude Determination Algorithms Using Two Noisy Vector Measurements. [Thesis]. Purdue University; 2016. Available from: https://docs.lib.purdue.edu/open_access_theses/1236

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


Virginia Tech

2. 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 November 25, 2020. http://hdl.handle.net/10919/49102.

MLA Handbook (7th Edition):

Keil, Elizabeth Marie. “Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit.” 2014. Web. 25 Nov 2020.

Vancouver:

Keil EM. Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Nov 25]. 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 Houston

3. Arcot, Mrinalini. Attitude determination of GPS satellite vehicles.

Degree: MS, Engineering Technology, 2014, University of Houston

 There is an increasing demand for navigation systems that has led to rapid development of Global Positioning System (GPS) across industries. Apart from position and… (more)

Subjects/Keywords: GPS; Attitudes; LAMBDA; Integer ambiguity; Attitude determination

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APA (6th Edition):

Arcot, M. (2014). Attitude determination of GPS satellite vehicles. (Masters Thesis). University of Houston. Retrieved from http://hdl.handle.net/10657/1455

Chicago Manual of Style (16th Edition):

Arcot, Mrinalini. “Attitude determination of GPS satellite vehicles.” 2014. Masters Thesis, University of Houston. Accessed November 25, 2020. http://hdl.handle.net/10657/1455.

MLA Handbook (7th Edition):

Arcot, Mrinalini. “Attitude determination of GPS satellite vehicles.” 2014. Web. 25 Nov 2020.

Vancouver:

Arcot M. Attitude determination of GPS satellite vehicles. [Internet] [Masters thesis]. University of Houston; 2014. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10657/1455.

Council of Science Editors:

Arcot M. Attitude determination of GPS satellite vehicles. [Masters Thesis]. University of Houston; 2014. Available from: http://hdl.handle.net/10657/1455

4. Carlsson, Jesper. Enhancement of Positioning and Attitude Estimation Using Raw GPS Data in an Extended Kalman Filter.

Degree: The Institute of Technology, 2014, Linköping UniversityLinköping University

  A Global Positioning System (GPS) can be used to estimate an objects position,given that the object has a GPS antenna. However, the system requires… (more)

Subjects/Keywords: GPS; attitude determination; pseudorange; tight coupling

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

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APA (6th Edition):

Carlsson, J. (2014). Enhancement of Positioning and Attitude Estimation Using Raw GPS Data in an Extended Kalman Filter. (Thesis). Linköping UniversityLinköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-109336

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):

Carlsson, Jesper. “Enhancement of Positioning and Attitude Estimation Using Raw GPS Data in an Extended Kalman Filter.” 2014. Thesis, Linköping UniversityLinköping University. Accessed November 25, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-109336.

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

MLA Handbook (7th Edition):

Carlsson, Jesper. “Enhancement of Positioning and Attitude Estimation Using Raw GPS Data in an Extended Kalman Filter.” 2014. Web. 25 Nov 2020.

Vancouver:

Carlsson J. Enhancement of Positioning and Attitude Estimation Using Raw GPS Data in an Extended Kalman Filter. [Internet] [Thesis]. Linköping UniversityLinköping University; 2014. [cited 2020 Nov 25]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-109336.

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

Council of Science Editors:

Carlsson J. Enhancement of Positioning and Attitude Estimation Using Raw GPS Data in an Extended Kalman Filter. [Thesis]. Linköping UniversityLinköping University; 2014. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-109336

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


University of Toronto

5. Johnston-Lemke, Bryan. High Performance Attitude Determination and Control for Nanosatellite Missions.

Degree: 2011, University of Toronto

Small satellites are growing in popularity because they offer an effective option that enables missions otherwise too schedule or cost limited. However, many possible missions… (more)

Subjects/Keywords: Attitude Control; Attitude Determination; Satellite; Nanosatellite; Astronomy; Formation Flying; 0538

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APA (6th Edition):

Johnston-Lemke, B. (2011). High Performance Attitude Determination and Control for Nanosatellite Missions. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/30644

Chicago Manual of Style (16th Edition):

Johnston-Lemke, Bryan. “High Performance Attitude Determination and Control for Nanosatellite Missions.” 2011. Masters Thesis, University of Toronto. Accessed November 25, 2020. http://hdl.handle.net/1807/30644.

MLA Handbook (7th Edition):

Johnston-Lemke, Bryan. “High Performance Attitude Determination and Control for Nanosatellite Missions.” 2011. Web. 25 Nov 2020.

Vancouver:

Johnston-Lemke B. High Performance Attitude Determination and Control for Nanosatellite Missions. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1807/30644.

Council of Science Editors:

Johnston-Lemke B. High Performance Attitude Determination and Control for Nanosatellite Missions. [Masters Thesis]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/30644


Luleå University of Technology

6. Svedevall, Anders. Development of attitude determination sensors for miniature satellites.

Degree: 2014, Luleå University of Technology

Attitude determination is an important subsystem of any satellite application. Several different approaches are available to determine the orientation of a spacecraft. By using… (more)

Subjects/Keywords: Technology; Teknik; Sun sensor; attitude determination; pico satellite; attitude control; PSD sensor

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APA (6th Edition):

Svedevall, A. (2014). Development of attitude determination sensors for miniature satellites. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-52057

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):

Svedevall, Anders. “Development of attitude determination sensors for miniature satellites.” 2014. Thesis, Luleå University of Technology. Accessed November 25, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-52057.

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

MLA Handbook (7th Edition):

Svedevall, Anders. “Development of attitude determination sensors for miniature satellites.” 2014. Web. 25 Nov 2020.

Vancouver:

Svedevall A. Development of attitude determination sensors for miniature satellites. [Internet] [Thesis]. Luleå University of Technology; 2014. [cited 2020 Nov 25]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-52057.

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

Council of Science Editors:

Svedevall A. Development of attitude determination sensors for miniature satellites. [Thesis]. Luleå University of Technology; 2014. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-52057

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


Stellenbosch University

7. Janse van Vuuren, Gerhard Hermann. The design and simulation analysis of an attitude determination and control system for a small earth observation satellite.

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

ENGLISH ABSTRACT: The ability of satellites to actively control their attitude has changed the way we live. Navigation systems, satellite television, and weather forecasting, for… (more)

Subjects/Keywords: Attitude determination and control system (ADCS); Small earth observation satellite; UCTD

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APA (6th Edition):

Janse van Vuuren, G. H. (2015). The design and simulation analysis of an attitude determination and control system for a small earth observation satellite. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/96979

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):

Janse van Vuuren, Gerhard Hermann. “The design and simulation analysis of an attitude determination and control system for a small earth observation satellite.” 2015. Thesis, Stellenbosch University. Accessed November 25, 2020. http://hdl.handle.net/10019.1/96979.

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

MLA Handbook (7th Edition):

Janse van Vuuren, Gerhard Hermann. “The design and simulation analysis of an attitude determination and control system for a small earth observation satellite.” 2015. Web. 25 Nov 2020.

Vancouver:

Janse van Vuuren GH. The design and simulation analysis of an attitude determination and control system for a small earth observation satellite. [Internet] [Thesis]. Stellenbosch University; 2015. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10019.1/96979.

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

Council of Science Editors:

Janse van Vuuren GH. The design and simulation analysis of an attitude determination and control system for a small earth observation satellite. [Thesis]. Stellenbosch University; 2015. Available from: http://hdl.handle.net/10019.1/96979

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


University of Toronto

8. Ang, Paris Yen-Jun. Antenna Measurement and Design for the CanX-7 Nanosatellite and the Development of a Global Navigation Satellite System Based Attitude Determination System.

Degree: 2015, University of Toronto

This thesis describes and presents solutions to various challenges small satellites may encounter during design and operation, particularly in the areas of communications and attitude(more)

Subjects/Keywords: Antenna; Attitude Determination; Communications; GPS; Microsatellite; Satellite; 0538

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APA (6th Edition):

Ang, P. Y. (2015). Antenna Measurement and Design for the CanX-7 Nanosatellite and the Development of a Global Navigation Satellite System Based Attitude Determination System. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/70235

Chicago Manual of Style (16th Edition):

Ang, Paris Yen-Jun. “Antenna Measurement and Design for the CanX-7 Nanosatellite and the Development of a Global Navigation Satellite System Based Attitude Determination System.” 2015. Masters Thesis, University of Toronto. Accessed November 25, 2020. http://hdl.handle.net/1807/70235.

MLA Handbook (7th Edition):

Ang, Paris Yen-Jun. “Antenna Measurement and Design for the CanX-7 Nanosatellite and the Development of a Global Navigation Satellite System Based Attitude Determination System.” 2015. Web. 25 Nov 2020.

Vancouver:

Ang PY. Antenna Measurement and Design for the CanX-7 Nanosatellite and the Development of a Global Navigation Satellite System Based Attitude Determination System. [Internet] [Masters thesis]. University of Toronto; 2015. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1807/70235.

Council of Science Editors:

Ang PY. Antenna Measurement and Design for the CanX-7 Nanosatellite and the Development of a Global Navigation Satellite System Based Attitude Determination System. [Masters Thesis]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/70235


University of Toronto

9. 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 November 25, 2020. http://hdl.handle.net/1807/33557.

MLA Handbook (7th Edition):

Tarantini, Vincent. “Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite.” 2012. Web. 25 Nov 2020.

Vancouver:

Tarantini V. Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite. [Internet] [Masters thesis]. University of Toronto; 2012. [cited 2020 Nov 25]. 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


University of Toronto

10. Fournier, Marc. Attitude Determination and Control Hardware Development for Small Satellites.

Degree: 2011, University of Toronto

The development of a small spacecraft attitude determination and control subsystem is described. This subsystem is part of The Space Flight Laboratory's Generic Nanosatellite Bus.… (more)

Subjects/Keywords: Attitude Determination and Control Hardware Development for Small Satellites; 0538

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APA (6th Edition):

Fournier, M. (2011). Attitude Determination and Control Hardware Development for Small Satellites. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/29545

Chicago Manual of Style (16th Edition):

Fournier, Marc. “Attitude Determination and Control Hardware Development for Small Satellites.” 2011. Masters Thesis, University of Toronto. Accessed November 25, 2020. http://hdl.handle.net/1807/29545.

MLA Handbook (7th Edition):

Fournier, Marc. “Attitude Determination and Control Hardware Development for Small Satellites.” 2011. Web. 25 Nov 2020.

Vancouver:

Fournier M. Attitude Determination and Control Hardware Development for Small Satellites. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1807/29545.

Council of Science Editors:

Fournier M. Attitude Determination and Control Hardware Development for Small Satellites. [Masters Thesis]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/29545


Luleå University of Technology

11. Schwarz, Tobias. Prototyping of a Star Tracker for Pico-Satellites.

Degree: 2015, Luleå University of Technology

Attitude control is an essential subsystem of most spacecraft buses, therefore attitude determination plays a very important role as it is the feedback system… (more)

Subjects/Keywords: Technology; star tracker; star sensor; pico satellite; cubesat; attitude determination; Teknik

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APA (6th Edition):

Schwarz, T. (2015). Prototyping of a Star Tracker for Pico-Satellites. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-41922

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):

Schwarz, Tobias. “Prototyping of a Star Tracker for Pico-Satellites.” 2015. Thesis, Luleå University of Technology. Accessed November 25, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-41922.

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

MLA Handbook (7th Edition):

Schwarz, Tobias. “Prototyping of a Star Tracker for Pico-Satellites.” 2015. Web. 25 Nov 2020.

Vancouver:

Schwarz T. Prototyping of a Star Tracker for Pico-Satellites. [Internet] [Thesis]. Luleå University of Technology; 2015. [cited 2020 Nov 25]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-41922.

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

Council of Science Editors:

Schwarz T. Prototyping of a Star Tracker for Pico-Satellites. [Thesis]. Luleå University of Technology; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-41922

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


Luleå University of Technology

12. Kurz, Oliver. Design and implementation of an attitude determination system for the Cubesat UWE-2 (Hardware based).

Degree: 2008, Luleå University of Technology

The described Master thesis project describes the design and development of an \acl{ADS} for the Cubesat UWE-2. This report will give insight about the… (more)

Subjects/Keywords: Technology; attitude determination; picosatellite; Teknik

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APA (6th Edition):

Kurz, O. (2008). Design and implementation of an attitude determination system for the Cubesat UWE-2 (Hardware based). (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-54675

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):

Kurz, Oliver. “Design and implementation of an attitude determination system for the Cubesat UWE-2 (Hardware based).” 2008. Thesis, Luleå University of Technology. Accessed November 25, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-54675.

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

MLA Handbook (7th Edition):

Kurz, Oliver. “Design and implementation of an attitude determination system for the Cubesat UWE-2 (Hardware based).” 2008. Web. 25 Nov 2020.

Vancouver:

Kurz O. Design and implementation of an attitude determination system for the Cubesat UWE-2 (Hardware based). [Internet] [Thesis]. Luleå University of Technology; 2008. [cited 2020 Nov 25]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-54675.

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

Council of Science Editors:

Kurz O. Design and implementation of an attitude determination system for the Cubesat UWE-2 (Hardware based). [Thesis]. Luleå University of Technology; 2008. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-54675

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


Iowa State University

13. Gartner, Keegan. Improved rate and angle estimation through higher accuracy planar motion models.

Degree: 2011, Iowa State University

 A large number of attitude estimation algorithms assume sensor placement along the axis of rotation. These models assume that all measured accelerations are due to… (more)

Subjects/Keywords: Attitude Determination; INS; Kalman Filter; Sensor Fusion; Signal Processing; Mechanical Engineering

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APA (6th Edition):

Gartner, K. (2011). Improved rate and angle estimation through higher accuracy planar motion models. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/10359

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):

Gartner, Keegan. “Improved rate and angle estimation through higher accuracy planar motion models.” 2011. Thesis, Iowa State University. Accessed November 25, 2020. https://lib.dr.iastate.edu/etd/10359.

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

MLA Handbook (7th Edition):

Gartner, Keegan. “Improved rate and angle estimation through higher accuracy planar motion models.” 2011. Web. 25 Nov 2020.

Vancouver:

Gartner K. Improved rate and angle estimation through higher accuracy planar motion models. [Internet] [Thesis]. Iowa State University; 2011. [cited 2020 Nov 25]. Available from: https://lib.dr.iastate.edu/etd/10359.

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

Council of Science Editors:

Gartner K. Improved rate and angle estimation through higher accuracy planar motion models. [Thesis]. Iowa State University; 2011. Available from: https://lib.dr.iastate.edu/etd/10359

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


Delft University of Technology

14. Pasqualetto Cassinis, Lorenzo (author). Modeling and Analysis of Delfi-C3 Telemetry: Earth Orbit Parameters Estimation and AttitudeModel Improvements.

Degree: 2017, Delft University of Technology

 This thesis reports on the reconstruction of key orbital elements of the Earth’s orbit around the Sun from a miniaturized temperature sensor onboard of theDelfi-C3… (more)

Subjects/Keywords: Delfi-C3; Thermal behaviour; Attitude Determination; Estimation Theory

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APA (6th Edition):

Pasqualetto Cassinis, L. (. (2017). Modeling and Analysis of Delfi-C3 Telemetry: Earth Orbit Parameters Estimation and AttitudeModel Improvements. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d9c4499f-1dc0-4733-9428-8911568988e2

Chicago Manual of Style (16th Edition):

Pasqualetto Cassinis, Lorenzo (author). “Modeling and Analysis of Delfi-C3 Telemetry: Earth Orbit Parameters Estimation and AttitudeModel Improvements.” 2017. Masters Thesis, Delft University of Technology. Accessed November 25, 2020. http://resolver.tudelft.nl/uuid:d9c4499f-1dc0-4733-9428-8911568988e2.

MLA Handbook (7th Edition):

Pasqualetto Cassinis, Lorenzo (author). “Modeling and Analysis of Delfi-C3 Telemetry: Earth Orbit Parameters Estimation and AttitudeModel Improvements.” 2017. Web. 25 Nov 2020.

Vancouver:

Pasqualetto Cassinis L(. Modeling and Analysis of Delfi-C3 Telemetry: Earth Orbit Parameters Estimation and AttitudeModel Improvements. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Nov 25]. Available from: http://resolver.tudelft.nl/uuid:d9c4499f-1dc0-4733-9428-8911568988e2.

Council of Science Editors:

Pasqualetto Cassinis L(. Modeling and Analysis of Delfi-C3 Telemetry: Earth Orbit Parameters Estimation and AttitudeModel Improvements. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:d9c4499f-1dc0-4733-9428-8911568988e2


Delft University of Technology

15. Naulais, C. (author). General Aviation Radar System for Navigation and Attitude Determination: Deriving aircraft states using multiple on board FMCW radars.

Degree: 2015, Delft University of Technology

 General Aviation aircraft mostly fly with Visual Flight Rules (VFR). These are rules in aviation that permit the pilot to fly on sight if the… (more)

Subjects/Keywords: general aviation; VFR; FMCW radar; navigation; attitude determination

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APA (6th Edition):

Naulais, C. (. (2015). General Aviation Radar System for Navigation and Attitude Determination: Deriving aircraft states using multiple on board FMCW radars. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e264bd6c-cdc9-46de-b9ee-e6019b30d95f

Chicago Manual of Style (16th Edition):

Naulais, C (author). “General Aviation Radar System for Navigation and Attitude Determination: Deriving aircraft states using multiple on board FMCW radars.” 2015. Masters Thesis, Delft University of Technology. Accessed November 25, 2020. http://resolver.tudelft.nl/uuid:e264bd6c-cdc9-46de-b9ee-e6019b30d95f.

MLA Handbook (7th Edition):

Naulais, C (author). “General Aviation Radar System for Navigation and Attitude Determination: Deriving aircraft states using multiple on board FMCW radars.” 2015. Web. 25 Nov 2020.

Vancouver:

Naulais C(. General Aviation Radar System for Navigation and Attitude Determination: Deriving aircraft states using multiple on board FMCW radars. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Nov 25]. Available from: http://resolver.tudelft.nl/uuid:e264bd6c-cdc9-46de-b9ee-e6019b30d95f.

Council of Science Editors:

Naulais C(. General Aviation Radar System for Navigation and Attitude Determination: Deriving aircraft states using multiple on board FMCW radars. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:e264bd6c-cdc9-46de-b9ee-e6019b30d95f


Delft University of Technology

16. Gomes, A. (author). Laser-Based Control of Rotary-Wing UAVs.

Degree: 2015, Delft University of Technology

Unmanned Aerial Vehicles (UAVs) present a high technological development rate nowadays. These vehicles can be used to perform dangerous and costly inspection procedures in structures… (more)

Subjects/Keywords: UAVs; LiDAR sensor; geometry fitting; attitude determination; Lyapunov stability; trajectory tracking

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APA (6th Edition):

Gomes, A. (. (2015). Laser-Based Control of Rotary-Wing UAVs. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4bef5dc5-d6ef-4e4e-99db-90b7e44624f3

Chicago Manual of Style (16th Edition):

Gomes, A (author). “Laser-Based Control of Rotary-Wing UAVs.” 2015. Masters Thesis, Delft University of Technology. Accessed November 25, 2020. http://resolver.tudelft.nl/uuid:4bef5dc5-d6ef-4e4e-99db-90b7e44624f3.

MLA Handbook (7th Edition):

Gomes, A (author). “Laser-Based Control of Rotary-Wing UAVs.” 2015. Web. 25 Nov 2020.

Vancouver:

Gomes A(. Laser-Based Control of Rotary-Wing UAVs. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Nov 25]. Available from: http://resolver.tudelft.nl/uuid:4bef5dc5-d6ef-4e4e-99db-90b7e44624f3.

Council of Science Editors:

Gomes A(. Laser-Based Control of Rotary-Wing UAVs. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:4bef5dc5-d6ef-4e4e-99db-90b7e44624f3


Delft University of Technology

17. Lagaune, B.F. (author). Determination of the attitude state of space debris objects based on Satellite Laser Ranging, using Envisat as a test case.

Degree: 2016, Delft University of Technology

The attitude state of the passive Envisat satellite (ESA) has been estimated before using various techniques like Satellite Laser Ranging, radar and using light-curves. This… (more)

Subjects/Keywords: SLR; attitude; estimation; determination; Envisat; space debris; simulation; GEODYN; tumbling

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APA (6th Edition):

Lagaune, B. F. (. (2016). Determination of the attitude state of space debris objects based on Satellite Laser Ranging, using Envisat as a test case. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:245b8941-08f3-4322-a442-d50e174e3c05

Chicago Manual of Style (16th Edition):

Lagaune, B F (author). “Determination of the attitude state of space debris objects based on Satellite Laser Ranging, using Envisat as a test case.” 2016. Masters Thesis, Delft University of Technology. Accessed November 25, 2020. http://resolver.tudelft.nl/uuid:245b8941-08f3-4322-a442-d50e174e3c05.

MLA Handbook (7th Edition):

Lagaune, B F (author). “Determination of the attitude state of space debris objects based on Satellite Laser Ranging, using Envisat as a test case.” 2016. Web. 25 Nov 2020.

Vancouver:

Lagaune BF(. Determination of the attitude state of space debris objects based on Satellite Laser Ranging, using Envisat as a test case. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2020 Nov 25]. Available from: http://resolver.tudelft.nl/uuid:245b8941-08f3-4322-a442-d50e174e3c05.

Council of Science Editors:

Lagaune BF(. Determination of the attitude state of space debris objects based on Satellite Laser Ranging, using Envisat as a test case. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:245b8941-08f3-4322-a442-d50e174e3c05


University of Minnesota

18. Laughlin, Kail. Single-Vector Aiding of an IMU for CubeSat Attitude Determination.

Degree: MS, Aerospace Engineering and Mechanics, 2020, University of Minnesota

 This thesis examines CubeSat attitude determination using the Earth’s magnetic field (EMF) vector aiding a low-cost IMU. CubeSats provide relatively cost-effective methods of performing scientific… (more)

Subjects/Keywords: Attitude Determination; CubeSat; Estimation; Gyro; Kalman Filtering; Magnetometer

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APA (6th Edition):

Laughlin, K. (2020). Single-Vector Aiding of an IMU for CubeSat Attitude Determination. (Masters Thesis). University of Minnesota. Retrieved from http://hdl.handle.net/11299/216304

Chicago Manual of Style (16th Edition):

Laughlin, Kail. “Single-Vector Aiding of an IMU for CubeSat Attitude Determination.” 2020. Masters Thesis, University of Minnesota. Accessed November 25, 2020. http://hdl.handle.net/11299/216304.

MLA Handbook (7th Edition):

Laughlin, Kail. “Single-Vector Aiding of an IMU for CubeSat Attitude Determination.” 2020. Web. 25 Nov 2020.

Vancouver:

Laughlin K. Single-Vector Aiding of an IMU for CubeSat Attitude Determination. [Internet] [Masters thesis]. University of Minnesota; 2020. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/11299/216304.

Council of Science Editors:

Laughlin K. Single-Vector Aiding of an IMU for CubeSat Attitude Determination. [Masters Thesis]. University of Minnesota; 2020. Available from: http://hdl.handle.net/11299/216304


University of Texas – Austin

19. -5382-4570. Analyzing and monitoring GRACE-FO star camera performance in a changing environment.

Degree: MSin Engineering, Aerospace Engineering, 2020, University of Texas – Austin

 The Gravity Recovery and Climate Experiment Follow-On (GRACE-FO) mission is an Earth-observing pair of satellites whose primary objective is to provide a time-variable map of… (more)

Subjects/Keywords: GRACE-FO; Satellite; Attitude determination; Star camera; Orientation

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APA (6th Edition):

-5382-4570. (2020). Analyzing and monitoring GRACE-FO star camera performance in a changing environment. (Masters Thesis). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/10143

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-5382-4570. “Analyzing and monitoring GRACE-FO star camera performance in a changing environment.” 2020. Masters Thesis, University of Texas – Austin. Accessed November 25, 2020. http://dx.doi.org/10.26153/tsw/10143.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-5382-4570. “Analyzing and monitoring GRACE-FO star camera performance in a changing environment.” 2020. Web. 25 Nov 2020.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-5382-4570. Analyzing and monitoring GRACE-FO star camera performance in a changing environment. [Internet] [Masters thesis]. University of Texas – Austin; 2020. [cited 2020 Nov 25]. Available from: http://dx.doi.org/10.26153/tsw/10143.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-5382-4570. Analyzing and monitoring GRACE-FO star camera performance in a changing environment. [Masters Thesis]. University of Texas – Austin; 2020. Available from: http://dx.doi.org/10.26153/tsw/10143

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


University of Texas – Austin

20. McBryde, Christopher Ryan. A star tracker design for CubeSats.

Degree: MSin Engineering, Aerospace Engineering, 2012, University of Texas – Austin

 This research outlines a low-cost, low-power, arc-minute accurate star tracker that is designed for use on a CubeSat. The device is being developed at the… (more)

Subjects/Keywords: Star tracker; Star camera; CubeSat; Attitude determination; Satellite; Small satellite

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APA (6th Edition):

McBryde, C. R. (2012). A star tracker design for CubeSats. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2012-05-4608

Chicago Manual of Style (16th Edition):

McBryde, Christopher Ryan. “A star tracker design for CubeSats.” 2012. Masters Thesis, University of Texas – Austin. Accessed November 25, 2020. http://hdl.handle.net/2152/ETD-UT-2012-05-4608.

MLA Handbook (7th Edition):

McBryde, Christopher Ryan. “A star tracker design for CubeSats.” 2012. Web. 25 Nov 2020.

Vancouver:

McBryde CR. A star tracker design for CubeSats. [Internet] [Masters thesis]. University of Texas – Austin; 2012. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/2152/ETD-UT-2012-05-4608.

Council of Science Editors:

McBryde CR. A star tracker design for CubeSats. [Masters Thesis]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/ETD-UT-2012-05-4608


Utah State University

21. Ryan, Keegan P. Experimental Testing of the Accuracy of Attitude Determination Solutions for a Spin-Stabilized Spacecraft.

Degree: MS, Mechanical and Aerospace Engineering, 2011, Utah State University

  Spin-stabilized spacecraft generally rely on sun and three-axis magnetic field sensor measurements for attitude determination. This study experimentally determines the total accuracy of attitude(more)

Subjects/Keywords: Attitude; Determination; Experimental; Ground; Spacecraft; Test; Mechanical Engineering

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APA (6th Edition):

Ryan, K. P. (2011). Experimental Testing of the Accuracy of Attitude Determination Solutions for a Spin-Stabilized Spacecraft. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/1007

Chicago Manual of Style (16th Edition):

Ryan, Keegan P. “Experimental Testing of the Accuracy of Attitude Determination Solutions for a Spin-Stabilized Spacecraft.” 2011. Masters Thesis, Utah State University. Accessed November 25, 2020. https://digitalcommons.usu.edu/etd/1007.

MLA Handbook (7th Edition):

Ryan, Keegan P. “Experimental Testing of the Accuracy of Attitude Determination Solutions for a Spin-Stabilized Spacecraft.” 2011. Web. 25 Nov 2020.

Vancouver:

Ryan KP. Experimental Testing of the Accuracy of Attitude Determination Solutions for a Spin-Stabilized Spacecraft. [Internet] [Masters thesis]. Utah State University; 2011. [cited 2020 Nov 25]. Available from: https://digitalcommons.usu.edu/etd/1007.

Council of Science Editors:

Ryan KP. Experimental Testing of the Accuracy of Attitude Determination Solutions for a Spin-Stabilized Spacecraft. [Masters Thesis]. Utah State University; 2011. Available from: https://digitalcommons.usu.edu/etd/1007


University of Toronto

22. Lukaszynski, Pawel. Attitude Control Hardware and Software for Nanosatellites.

Degree: 2013, University of Toronto

The analysis, verification and emulation of attitude control hardware for nanosatellite spacecraft is described. The overall focus is on hardware that pertains to a multitude… (more)

Subjects/Keywords: nanosatellites; reaction wheel; hysteresis rod; acceptance test; hardware emulation in software; attitude determination and control; attitude determination; attitude control; torque jitter; 0538

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APA (6th Edition):

Lukaszynski, P. (2013). Attitude Control Hardware and Software for Nanosatellites. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/43095

Chicago Manual of Style (16th Edition):

Lukaszynski, Pawel. “Attitude Control Hardware and Software for Nanosatellites.” 2013. Masters Thesis, University of Toronto. Accessed November 25, 2020. http://hdl.handle.net/1807/43095.

MLA Handbook (7th Edition):

Lukaszynski, Pawel. “Attitude Control Hardware and Software for Nanosatellites.” 2013. Web. 25 Nov 2020.

Vancouver:

Lukaszynski P. Attitude Control Hardware and Software for Nanosatellites. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1807/43095.

Council of Science Editors:

Lukaszynski P. Attitude Control Hardware and Software for Nanosatellites. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/43095


York University

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Wright, Thomas Jonathan. “Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites.” 2015. Masters Thesis, York University. Accessed November 25, 2020. http://hdl.handle.net/10315/28288.

MLA Handbook (7th Edition):

Wright, Thomas Jonathan. “Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites.” 2015. Web. 25 Nov 2020.

Vancouver:

Wright TJ. Development of Magnetometer-Based Orbit and Attitude Determination for Nanosatellites. [Internet] [Masters thesis]. York University; 2015. [cited 2020 Nov 25]. 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


Delft University of Technology

24. Giorgi, G. GNSS Carrier Phase-based Attitude Determination: Estimation and Applications.

Degree: 2011, Delft University of Technology

Attitude determination through the use of Global Navigation Satellite System (GNSS) signals is one of the many applications of satellite-based navigation. Multiple GNSS antennas installed… (more)

Subjects/Keywords: GNSS; GPS; Attitude; Compass; Attitude determination; Ambiguity resolution

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APA (6th Edition):

Giorgi, G. (2011). GNSS Carrier Phase-based Attitude Determination: Estimation and Applications. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; urn:NBN:nl:ui:24-uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; urn:NBN:nl:ui:24-uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; http://resolver.tudelft.nl/uuid:25070509-2292-42ed-8ba9-bf070fdbb793

Chicago Manual of Style (16th Edition):

Giorgi, G. “GNSS Carrier Phase-based Attitude Determination: Estimation and Applications.” 2011. Doctoral Dissertation, Delft University of Technology. Accessed November 25, 2020. http://resolver.tudelft.nl/uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; urn:NBN:nl:ui:24-uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; urn:NBN:nl:ui:24-uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; http://resolver.tudelft.nl/uuid:25070509-2292-42ed-8ba9-bf070fdbb793.

MLA Handbook (7th Edition):

Giorgi, G. “GNSS Carrier Phase-based Attitude Determination: Estimation and Applications.” 2011. Web. 25 Nov 2020.

Vancouver:

Giorgi G. GNSS Carrier Phase-based Attitude Determination: Estimation and Applications. [Internet] [Doctoral dissertation]. Delft University of Technology; 2011. [cited 2020 Nov 25]. Available from: http://resolver.tudelft.nl/uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; urn:NBN:nl:ui:24-uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; urn:NBN:nl:ui:24-uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; http://resolver.tudelft.nl/uuid:25070509-2292-42ed-8ba9-bf070fdbb793.

Council of Science Editors:

Giorgi G. GNSS Carrier Phase-based Attitude Determination: Estimation and Applications. [Doctoral Dissertation]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; urn:NBN:nl:ui:24-uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; urn:NBN:nl:ui:24-uuid:25070509-2292-42ed-8ba9-bf070fdbb793 ; http://resolver.tudelft.nl/uuid:25070509-2292-42ed-8ba9-bf070fdbb793


Massey University

25. Makarov, Kirill. Design of attitude determination and control system for KIWISAT amateur satellite.

Degree: Masters of Engineering, Mechatronics, 2015, Massey University

 This thesis is to present the design of “ADAC” system for “KiwiSat” cube satellite. An array of sensors were used: CMOS low resolution camera, sun… (more)

Subjects/Keywords: Artificial satellites; Attitude control systems; Attitude determination and control system (ADAC); KiwiSat; Sensors; Research Subject Categories::TECHNOLOGY::Other technology::Space engineering

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APA (6th Edition):

Makarov, K. (2015). Design of attitude determination and control system for KIWISAT amateur satellite. (Masters Thesis). Massey University. Retrieved from http://hdl.handle.net/10179/6857

Chicago Manual of Style (16th Edition):

Makarov, Kirill. “Design of attitude determination and control system for KIWISAT amateur satellite.” 2015. Masters Thesis, Massey University. Accessed November 25, 2020. http://hdl.handle.net/10179/6857.

MLA Handbook (7th Edition):

Makarov, Kirill. “Design of attitude determination and control system for KIWISAT amateur satellite.” 2015. Web. 25 Nov 2020.

Vancouver:

Makarov K. Design of attitude determination and control system for KIWISAT amateur satellite. [Internet] [Masters thesis]. Massey University; 2015. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10179/6857.

Council of Science Editors:

Makarov K. Design of attitude determination and control system for KIWISAT amateur satellite. [Masters Thesis]. Massey University; 2015. Available from: http://hdl.handle.net/10179/6857


University of Illinois – Urbana-Champaign

26. Vedant, -. Improved qualification and algorithms for illinisat-2 attitude determination and control.

Degree: MS, Aerospace Engineering, 2018, University of Illinois – Urbana-Champaign

 The University of Illinois has developed the IlliniSat-2 CubeSat bus, a generic scalable and modular design, utilizing commercially available off the shelf (COTS) parts. The… (more)

Subjects/Keywords: Attitude Determination and Control; Control Systems; Dynamic Programming; Trajectory Planning; Underactuated Control

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APA (6th Edition):

Vedant, -. (2018). Improved qualification and algorithms for illinisat-2 attitude determination and control. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/101238

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):

Vedant, -. “Improved qualification and algorithms for illinisat-2 attitude determination and control.” 2018. Thesis, University of Illinois – Urbana-Champaign. Accessed November 25, 2020. http://hdl.handle.net/2142/101238.

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

MLA Handbook (7th Edition):

Vedant, -. “Improved qualification and algorithms for illinisat-2 attitude determination and control.” 2018. Web. 25 Nov 2020.

Vancouver:

Vedant -. Improved qualification and algorithms for illinisat-2 attitude determination and control. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2018. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/2142/101238.

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

Council of Science Editors:

Vedant -. Improved qualification and algorithms for illinisat-2 attitude determination and control. [Thesis]. University of Illinois – Urbana-Champaign; 2018. Available from: http://hdl.handle.net/2142/101238

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


University of Colorado

27. Gerhardt, David Thomas. Small Satellite Passive Magnetic Attitude Control.

Degree: PhD, Aerospace Engineering Sciences, 2014, University of Colorado

  Passive Magnetic Attitude Control (PMAC) is capable of aligning a satellite within 5 degrees of the local magnetic field at low resource cost, making… (more)

Subjects/Keywords: Attitude; Determination; Magnetic; Measurement; Passive; Simulation; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Gerhardt, D. T. (2014). Small Satellite Passive Magnetic Attitude Control. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/78

Chicago Manual of Style (16th Edition):

Gerhardt, David Thomas. “Small Satellite Passive Magnetic Attitude Control.” 2014. Doctoral Dissertation, University of Colorado. Accessed November 25, 2020. https://scholar.colorado.edu/asen_gradetds/78.

MLA Handbook (7th Edition):

Gerhardt, David Thomas. “Small Satellite Passive Magnetic Attitude Control.” 2014. Web. 25 Nov 2020.

Vancouver:

Gerhardt DT. Small Satellite Passive Magnetic Attitude Control. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2020 Nov 25]. Available from: https://scholar.colorado.edu/asen_gradetds/78.

Council of Science Editors:

Gerhardt DT. Small Satellite Passive Magnetic Attitude Control. [Doctoral Dissertation]. University of Colorado; 2014. Available from: https://scholar.colorado.edu/asen_gradetds/78


Delft University of Technology

28. Beckers, Bo (author). Image navigation for SPECTROLITE: Using an imaging spectrometer as high performance attitude sensor.

Degree: 2017, Delft University of Technology

Subjects/Keywords: ADCS; attitude determination; spectrometer; image navigation

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APA (6th Edition):

Beckers, B. (. (2017). Image navigation for SPECTROLITE: Using an imaging spectrometer as high performance attitude sensor. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e5793cf5-e7b3-4c1a-a84c-803b875fadaa

Chicago Manual of Style (16th Edition):

Beckers, Bo (author). “Image navigation for SPECTROLITE: Using an imaging spectrometer as high performance attitude sensor.” 2017. Masters Thesis, Delft University of Technology. Accessed November 25, 2020. http://resolver.tudelft.nl/uuid:e5793cf5-e7b3-4c1a-a84c-803b875fadaa.

MLA Handbook (7th Edition):

Beckers, Bo (author). “Image navigation for SPECTROLITE: Using an imaging spectrometer as high performance attitude sensor.” 2017. Web. 25 Nov 2020.

Vancouver:

Beckers B(. Image navigation for SPECTROLITE: Using an imaging spectrometer as high performance attitude sensor. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Nov 25]. Available from: http://resolver.tudelft.nl/uuid:e5793cf5-e7b3-4c1a-a84c-803b875fadaa.

Council of Science Editors:

Beckers B(. Image navigation for SPECTROLITE: Using an imaging spectrometer as high performance attitude sensor. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:e5793cf5-e7b3-4c1a-a84c-803b875fadaa


University of Texas – Austin

29. -7636-3233. An attitude determination and control system for small satellites.

Degree: MSin Engineering, Aerospace Engineering, 2015, University of Texas – Austin

 A flexible, robust attitude determination and control (ADC) system is presented for small satellite platforms. Using commercial-off-the-shelf sensors, reaction wheels, and magnetorquers which fit within… (more)

Subjects/Keywords: Attitude; Determination; Control; Estimation; CubeSat; Satellite; ADC; Guidance; Convex optimization; Constrained attitude guidance; Attitude constraint; Texas Spacecraft Laboratory; TSL; Bevo-2; ARMADILLO

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

APA (6th Edition):

-7636-3233. (2015). An attitude determination and control system for small satellites. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/31715

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-7636-3233. “An attitude determination and control system for small satellites.” 2015. Masters Thesis, University of Texas – Austin. Accessed November 25, 2020. http://hdl.handle.net/2152/31715.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-7636-3233. “An attitude determination and control system for small satellites.” 2015. Web. 25 Nov 2020.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-7636-3233. An attitude determination and control system for small satellites. [Internet] [Masters thesis]. University of Texas – Austin; 2015. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/2152/31715.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-7636-3233. An attitude determination and control system for small satellites. [Masters Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/31715

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


Cornell University

30. 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

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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 November 25, 2020. 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. 25 Nov 2020.

Vancouver:

Jung H. ESTIMATION PROBLEMS FOR SATELLITE ORBIT AND ATTITUDE DETERMINATION AND FOR GPS-BASED REMOTE IONOSPHERIC SENSING. [Internet] [Thesis]. Cornell University; 2005. [cited 2020 Nov 25]. 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

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