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Delft University of Technology
1. van Hengel, Anita (author). Magnetorquer Design and Attitude Control for SHAPE.
Degree: 2018, Delft University of Technology
URL: http://resolver.tudelft.nl/uuid:dc8b7355-cf46-410c-94c3-cc85570b94a7
Subjects/Keywords: Attitude control; SHAPE; Magnetorquer
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
van Hengel, A. (. (2018). Magnetorquer Design and Attitude Control for SHAPE. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:dc8b7355-cf46-410c-94c3-cc85570b94a7
Chicago Manual of Style (16th Edition):
van Hengel, Anita (author). “Magnetorquer Design and Attitude Control for SHAPE.” 2018. Masters Thesis, Delft University of Technology. Accessed April 22, 2021. http://resolver.tudelft.nl/uuid:dc8b7355-cf46-410c-94c3-cc85570b94a7.
MLA Handbook (7th Edition):
van Hengel, Anita (author). “Magnetorquer Design and Attitude Control for SHAPE.” 2018. Web. 22 Apr 2021.
Vancouver:
van Hengel A(. Magnetorquer Design and Attitude Control for SHAPE. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Apr 22]. Available from: http://resolver.tudelft.nl/uuid:dc8b7355-cf46-410c-94c3-cc85570b94a7.
Council of Science Editors:
van Hengel A(. Magnetorquer Design and Attitude Control for SHAPE. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:dc8b7355-cf46-410c-94c3-cc85570b94a7
Delft University of Technology
2. Slinger, B.J.M.M. (author). Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion.
Degree: 2016, Delft University of Technology
URL: http://resolver.tudelft.nl/uuid:9eba1543-6f55-4708-9d68-09446a95d6d4
Subjects/Keywords: INDI helicopter uav control attitude
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Slinger, B. J. M. M. (. (2016). Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:9eba1543-6f55-4708-9d68-09446a95d6d4
Chicago Manual of Style (16th Edition):
Slinger, B J M M (author). “Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion.” 2016. Masters Thesis, Delft University of Technology. Accessed April 22, 2021. http://resolver.tudelft.nl/uuid:9eba1543-6f55-4708-9d68-09446a95d6d4.
MLA Handbook (7th Edition):
Slinger, B J M M (author). “Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion.” 2016. Web. 22 Apr 2021.
Vancouver:
Slinger BJMM(. Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Apr 22]. Available from: http://resolver.tudelft.nl/uuid:9eba1543-6f55-4708-9d68-09446a95d6d4.
Council of Science Editors:
Slinger BJMM(. Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:9eba1543-6f55-4708-9d68-09446a95d6d4
University of Minnesota
3. Kukowski, Timothy. Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite.
Degree: MS, Aerospace Engineering and Mechanics, 2020, University of Minnesota
URL: http://hdl.handle.net/11299/213061
Subjects/Keywords: attitude; control; cubesat; magnetic; magnetorquers
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Kukowski, T. (2020). Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite. (Masters Thesis). University of Minnesota. Retrieved from http://hdl.handle.net/11299/213061
Chicago Manual of Style (16th Edition):
Kukowski, Timothy. “Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite.” 2020. Masters Thesis, University of Minnesota. Accessed April 22, 2021. http://hdl.handle.net/11299/213061.
MLA Handbook (7th Edition):
Kukowski, Timothy. “Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite.” 2020. Web. 22 Apr 2021.
Vancouver:
Kukowski T. Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite. [Internet] [Masters thesis]. University of Minnesota; 2020. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/11299/213061.
Council of Science Editors:
Kukowski T. Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite. [Masters Thesis]. University of Minnesota; 2020. Available from: http://hdl.handle.net/11299/213061
Lehigh University
4. Zhu, Shiqiao. Analysis of Spacecraft Attitude Control.
Degree: MS, Mechanical Engineering, 2016, Lehigh University
URL: https://preserve.lehigh.edu/etd/2915
Subjects/Keywords: alalysis of spacecraft attitude control; analysis control; attitude; attitude control; attitude of spacecraft; spacecraft control; Engineering; Mechanical Engineering
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APA (6th Edition):
Zhu, S. (2016). Analysis of Spacecraft Attitude Control. (Thesis). Lehigh University. Retrieved from https://preserve.lehigh.edu/etd/2915
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Chicago Manual of Style (16th Edition):
Zhu, Shiqiao. “Analysis of Spacecraft Attitude Control.” 2016. Thesis, Lehigh University. Accessed April 22, 2021. https://preserve.lehigh.edu/etd/2915.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
MLA Handbook (7th Edition):
Zhu, Shiqiao. “Analysis of Spacecraft Attitude Control.” 2016. Web. 22 Apr 2021.
Vancouver:
Zhu S. Analysis of Spacecraft Attitude Control. [Internet] [Thesis]. Lehigh University; 2016. [cited 2021 Apr 22]. Available from: https://preserve.lehigh.edu/etd/2915.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Council of Science Editors:
Zhu S. Analysis of Spacecraft Attitude Control. [Thesis]. Lehigh University; 2016. Available from: https://preserve.lehigh.edu/etd/2915
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Kwame Nkrumah University of Science and Technology
5. Danso, Adu Eric. Knowledge, attitude and practices towards malaria.
Degree: 2021, Kwame Nkrumah University of Science and Technology
URL: http://dspace.knust.edu.gh:8080/jspui/handle/123456789/13313
Subjects/Keywords: Knowledge, attitude; Malaria control; Akuapim
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APA (6th Edition):
Danso, A. E. (2021). Knowledge, attitude and practices towards malaria. (Thesis). Kwame Nkrumah University of Science and Technology. Retrieved from http://dspace.knust.edu.gh:8080/jspui/handle/123456789/13313
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):
Danso, Adu Eric. “Knowledge, attitude and practices towards malaria.” 2021. Thesis, Kwame Nkrumah University of Science and Technology. Accessed April 22, 2021. http://dspace.knust.edu.gh:8080/jspui/handle/123456789/13313.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
MLA Handbook (7th Edition):
Danso, Adu Eric. “Knowledge, attitude and practices towards malaria.” 2021. Web. 22 Apr 2021.
Vancouver:
Danso AE. Knowledge, attitude and practices towards malaria. [Internet] [Thesis]. Kwame Nkrumah University of Science and Technology; 2021. [cited 2021 Apr 22]. Available from: http://dspace.knust.edu.gh:8080/jspui/handle/123456789/13313.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Council of Science Editors:
Danso AE. Knowledge, attitude and practices towards malaria. [Thesis]. Kwame Nkrumah University of Science and Technology; 2021. Available from: http://dspace.knust.edu.gh:8080/jspui/handle/123456789/13313
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
York University
6. Agarwal, Anirudh. Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages.
Degree: MSc -MS, Earth & Space Science, 2019, York University
URL: http://hdl.handle.net/10315/35911
Subjects/Keywords: Aerospace engineering; Spacecraft dynamics; Control systems; Acceleration feedback; PIDA; PID; Attitude control; Classical control; Spacecraft attitude control; Single axis attitude control
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Agarwal, A. (2019). Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages. (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/35911
Chicago Manual of Style (16th Edition):
Agarwal, Anirudh. “Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages.” 2019. Masters Thesis, York University. Accessed April 22, 2021. http://hdl.handle.net/10315/35911.
MLA Handbook (7th Edition):
Agarwal, Anirudh. “Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages.” 2019. Web. 22 Apr 2021.
Vancouver:
Agarwal A. Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages. [Internet] [Masters thesis]. York University; 2019. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/10315/35911.
Council of Science Editors:
Agarwal A. Proportional-Derivative-Acceleration Feedback Controller Design for Single Axis Attitude Control of Rigid Spacecraft with Flexible Appendages. [Masters Thesis]. York University; 2019. Available from: http://hdl.handle.net/10315/35911
University of Toronto
7. Dutia, Jiten. Magnetic Attitude Control of Microsatellites In Geocentric Orbits.
Degree: 2013, University of Toronto
URL: http://hdl.handle.net/1807/35117
Subjects/Keywords: hybrid attitude control; magnetic attitudde control; 0538
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Dutia, J. (2013). Magnetic Attitude Control of Microsatellites In Geocentric Orbits. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/35117
Chicago Manual of Style (16th Edition):
Dutia, Jiten. “Magnetic Attitude Control of Microsatellites In Geocentric Orbits.” 2013. Masters Thesis, University of Toronto. Accessed April 22, 2021. http://hdl.handle.net/1807/35117.
MLA Handbook (7th Edition):
Dutia, Jiten. “Magnetic Attitude Control of Microsatellites In Geocentric Orbits.” 2013. Web. 22 Apr 2021.
Vancouver:
Dutia J. Magnetic Attitude Control of Microsatellites In Geocentric Orbits. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/1807/35117.
Council of Science Editors:
Dutia J. Magnetic Attitude Control of Microsatellites In Geocentric Orbits. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/35117
University of Toronto
8. Ibrahim, Najmus. Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.
Degree: 2013, University of Toronto
URL: http://hdl.handle.net/1807/42965
Subjects/Keywords: satellite; attitude; attitude and orbit control; microsatellite; control; estimation; tracking; 0538
Record Details
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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 April 22, 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. 22 Apr 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 Apr 22]. 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 Texas – Austin
9. Mendes De Almeida Neto, Marcelino. Quaternion regression and finite-time controllers for attitude dynamics.
Degree: PhD, Aerospace Engineering, 2020, University of Texas – Austin
URL: http://dx.doi.org/10.26153/tsw/7431
Subjects/Keywords: Quaternion; Attitude control; Attitude estimation; Slam; Quaternion regression; Finite time control
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APA (6th Edition):
Mendes De Almeida Neto, M. (2020). Quaternion regression and finite-time controllers for attitude dynamics. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/7431
Chicago Manual of Style (16th Edition):
Mendes De Almeida Neto, Marcelino. “Quaternion regression and finite-time controllers for attitude dynamics.” 2020. Doctoral Dissertation, University of Texas – Austin. Accessed April 22, 2021. http://dx.doi.org/10.26153/tsw/7431.
MLA Handbook (7th Edition):
Mendes De Almeida Neto, Marcelino. “Quaternion regression and finite-time controllers for attitude dynamics.” 2020. Web. 22 Apr 2021.
Vancouver:
Mendes De Almeida Neto M. Quaternion regression and finite-time controllers for attitude dynamics. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2020. [cited 2021 Apr 22]. Available from: http://dx.doi.org/10.26153/tsw/7431.
Council of Science Editors:
Mendes De Almeida Neto M. Quaternion regression and finite-time controllers for attitude dynamics. [Doctoral Dissertation]. University of Texas – Austin; 2020. Available from: http://dx.doi.org/10.26153/tsw/7431
University of Toronto
10. Serpelloni, Edoardo. Bang-Bang Practical Stabilization of Rigid Bodies.
Degree: PhD, 2017, University of Toronto
URL: http://hdl.handle.net/1807/79471
Subjects/Keywords: Attitude Control; Bang-Bang Control; Double-Integrator Control; Spacecraft Control; 0544
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Serpelloni, E. (2017). Bang-Bang Practical Stabilization of Rigid Bodies. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/79471
Chicago Manual of Style (16th Edition):
Serpelloni, Edoardo. “Bang-Bang Practical Stabilization of Rigid Bodies.” 2017. Doctoral Dissertation, University of Toronto. Accessed April 22, 2021. http://hdl.handle.net/1807/79471.
MLA Handbook (7th Edition):
Serpelloni, Edoardo. “Bang-Bang Practical Stabilization of Rigid Bodies.” 2017. Web. 22 Apr 2021.
Vancouver:
Serpelloni E. Bang-Bang Practical Stabilization of Rigid Bodies. [Internet] [Doctoral dissertation]. University of Toronto; 2017. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/1807/79471.
Council of Science Editors:
Serpelloni E. Bang-Bang Practical Stabilization of Rigid Bodies. [Doctoral Dissertation]. University of Toronto; 2017. Available from: http://hdl.handle.net/1807/79471
Virginia Tech
11. VanDyke, Matthew Clark. Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite.
Degree: PhD, Aerospace Engineering, 2014, Virginia Tech
URL: http://hdl.handle.net/10919/24911
Subjects/Keywords: Gyrostat-Satellite; Relative Equilibrium; Spacecraft Dynamics; Attitude Control; Attitude Guidance; Gravitational Torque; Attitude Maneuvers
Record Details
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APA (6th Edition):
VanDyke, M. C. (2014). Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/24911
Chicago Manual of Style (16th Edition):
VanDyke, Matthew Clark. “Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite.” 2014. Doctoral Dissertation, Virginia Tech. Accessed April 22, 2021. http://hdl.handle.net/10919/24911.
MLA Handbook (7th Edition):
VanDyke, Matthew Clark. “Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite.” 2014. Web. 22 Apr 2021.
Vancouver:
VanDyke MC. Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/10919/24911.
Council of Science Editors:
VanDyke MC. Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/24911
Penn State University
12. Ahn, Young Tae. Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution.
Degree: 2012, Penn State University
URL: https://submit-etda.libraries.psu.edu/catalog/16015
Subjects/Keywords: spacecraft attitude dynamics; attitude control; combinatorial optimization theory
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APA (6th Edition):
Ahn, Y. T. (2012). Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/16015
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):
Ahn, Young Tae. “Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution.” 2012. Thesis, Penn State University. Accessed April 22, 2021. https://submit-etda.libraries.psu.edu/catalog/16015.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
MLA Handbook (7th Edition):
Ahn, Young Tae. “Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution.” 2012. Web. 22 Apr 2021.
Vancouver:
Ahn YT. Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution. [Internet] [Thesis]. Penn State University; 2012. [cited 2021 Apr 22]. Available from: https://submit-etda.libraries.psu.edu/catalog/16015.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Council of Science Editors:
Ahn YT. Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution. [Thesis]. Penn State University; 2012. Available from: https://submit-etda.libraries.psu.edu/catalog/16015
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
University of Toronto
13. Johnston-Lemke, Bryan. High Performance Attitude Determination and Control for Nanosatellite Missions.
Degree: 2011, University of Toronto
URL: http://hdl.handle.net/1807/30644
Subjects/Keywords: Attitude Control; Attitude Determination; Satellite; Nanosatellite; Astronomy; Formation Flying; 0538
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 April 22, 2021. http://hdl.handle.net/1807/30644.
MLA Handbook (7th Edition):
Johnston-Lemke, Bryan. “High Performance Attitude Determination and Control for Nanosatellite Missions.” 2011. Web. 22 Apr 2021.
Vancouver:
Johnston-Lemke B. High Performance Attitude Determination and Control for Nanosatellite Missions. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2021 Apr 22]. 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
University of Toronto
14. Shen, Young-Young. Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites.
Degree: 2015, University of Toronto
URL: http://hdl.handle.net/1807/70675
Subjects/Keywords: Attitude; Control; Microsatellite; Nanosatellite; Satellite; Small; 0538
Record Details
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APA (6th Edition):
Shen, Y. (2015). Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/70675
Chicago Manual of Style (16th Edition):
Shen, Young-Young. “Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites.” 2015. Masters Thesis, University of Toronto. Accessed April 22, 2021. http://hdl.handle.net/1807/70675.
MLA Handbook (7th Edition):
Shen, Young-Young. “Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites.” 2015. Web. 22 Apr 2021.
Vancouver:
Shen Y. Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites. [Internet] [Masters thesis]. University of Toronto; 2015. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/1807/70675.
Council of Science Editors:
Shen Y. Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites. [Masters Thesis]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/70675
University of Toronto
15. Findlay, Everett. Investigation of Active Vibration Suppression of a Flexible Satellite using Magnetic Attitude Control.
Degree: 2011, University of Toronto
URL: http://hdl.handle.net/1807/30593
Subjects/Keywords: magnetic attitude control; multibody dynamics; 0538
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Findlay, E. (2011). Investigation of Active Vibration Suppression of a Flexible Satellite using Magnetic Attitude Control. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/30593
Chicago Manual of Style (16th Edition):
Findlay, Everett. “Investigation of Active Vibration Suppression of a Flexible Satellite using Magnetic Attitude Control.” 2011. Masters Thesis, University of Toronto. Accessed April 22, 2021. http://hdl.handle.net/1807/30593.
MLA Handbook (7th Edition):
Findlay, Everett. “Investigation of Active Vibration Suppression of a Flexible Satellite using Magnetic Attitude Control.” 2011. Web. 22 Apr 2021.
Vancouver:
Findlay E. Investigation of Active Vibration Suppression of a Flexible Satellite using Magnetic Attitude Control. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/1807/30593.
Council of Science Editors:
Findlay E. Investigation of Active Vibration Suppression of a Flexible Satellite using Magnetic Attitude Control. [Masters Thesis]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/30593
University of Illinois – Urbana-Champaign
16. Zhao, Hongrui. Development of a low-cost multi-camera star tracker for small satellites.
Degree: MS, Aerospace Engineering, 2020, University of Illinois – Urbana-Champaign
URL: http://hdl.handle.net/2142/108522
Subjects/Keywords: Star Tracker; Attitude Determination and Control
Record Details
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APA (6th Edition):
Zhao, H. (2020). Development of a low-cost multi-camera star tracker for small satellites. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/108522
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):
Zhao, Hongrui. “Development of a low-cost multi-camera star tracker for small satellites.” 2020. Thesis, University of Illinois – Urbana-Champaign. Accessed April 22, 2021. http://hdl.handle.net/2142/108522.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
MLA Handbook (7th Edition):
Zhao, Hongrui. “Development of a low-cost multi-camera star tracker for small satellites.” 2020. Web. 22 Apr 2021.
Vancouver:
Zhao H. Development of a low-cost multi-camera star tracker for small satellites. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2020. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2142/108522.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Council of Science Editors:
Zhao H. Development of a low-cost multi-camera star tracker for small satellites. [Thesis]. University of Illinois – Urbana-Champaign; 2020. Available from: http://hdl.handle.net/2142/108522
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Utah State University
17. Bennett, Steven Russell. Control and Stability of Upper Stage Launch Vehicle With Hybrid Arc-Ignition Attitude Control System.
Degree: MS, Mechanical and Aerospace Engineering, 2019, Utah State University
URL: https://digitalcommons.usu.edu/etd/7518
Subjects/Keywords: Hybrid; Attitude; Control; Rocket; Slosh; Aerospace Engineering
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APA (6th Edition):
Bennett, S. R. (2019). Control and Stability of Upper Stage Launch Vehicle With Hybrid Arc-Ignition Attitude Control System. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/7518
Chicago Manual of Style (16th Edition):
Bennett, Steven Russell. “Control and Stability of Upper Stage Launch Vehicle With Hybrid Arc-Ignition Attitude Control System.” 2019. Masters Thesis, Utah State University. Accessed April 22, 2021. https://digitalcommons.usu.edu/etd/7518.
MLA Handbook (7th Edition):
Bennett, Steven Russell. “Control and Stability of Upper Stage Launch Vehicle With Hybrid Arc-Ignition Attitude Control System.” 2019. Web. 22 Apr 2021.
Vancouver:
Bennett SR. Control and Stability of Upper Stage Launch Vehicle With Hybrid Arc-Ignition Attitude Control System. [Internet] [Masters thesis]. Utah State University; 2019. [cited 2021 Apr 22]. Available from: https://digitalcommons.usu.edu/etd/7518.
Council of Science Editors:
Bennett SR. Control and Stability of Upper Stage Launch Vehicle With Hybrid Arc-Ignition Attitude Control System. [Masters Thesis]. Utah State University; 2019. Available from: https://digitalcommons.usu.edu/etd/7518
Brigham Young University
18. Argyle, Matthew Elliott. Modeling and Control of a Tailsitter with a Ducted Fan.
Degree: PhD, 2016, Brigham Young University
URL: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6928&context=etd
Subjects/Keywords: attitude control; attitude error; guidance and control; tailsitter; TECS; VTOL; Electrical and Computer Engineering
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Argyle, M. E. (2016). Modeling and Control of a Tailsitter with a Ducted Fan. (Doctoral Dissertation). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6928&context=etd
Chicago Manual of Style (16th Edition):
Argyle, Matthew Elliott. “Modeling and Control of a Tailsitter with a Ducted Fan.” 2016. Doctoral Dissertation, Brigham Young University. Accessed April 22, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6928&context=etd.
MLA Handbook (7th Edition):
Argyle, Matthew Elliott. “Modeling and Control of a Tailsitter with a Ducted Fan.” 2016. Web. 22 Apr 2021.
Vancouver:
Argyle ME. Modeling and Control of a Tailsitter with a Ducted Fan. [Internet] [Doctoral dissertation]. Brigham Young University; 2016. [cited 2021 Apr 22]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6928&context=etd.
Council of Science Editors:
Argyle ME. Modeling and Control of a Tailsitter with a Ducted Fan. [Doctoral Dissertation]. Brigham Young University; 2016. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6928&context=etd
Delft University of Technology
19. Maltha, Rutger (author). GOCE Spacecraft Attitude Control: A magnetic attitude controller simulator.
Degree: 2018, Delft University of Technology
URL: http://resolver.tudelft.nl/uuid:16c8d9b6-1d07-46fa-9a4f-4c445bd9e3dc
Subjects/Keywords: Genetic algorithm; INDI; Attitude control; GOCE; Spacecraft torque models; Magnetic attitude control; NDI
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Maltha, R. (. (2018). GOCE Spacecraft Attitude Control: A magnetic attitude controller simulator. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:16c8d9b6-1d07-46fa-9a4f-4c445bd9e3dc
Chicago Manual of Style (16th Edition):
Maltha, Rutger (author). “GOCE Spacecraft Attitude Control: A magnetic attitude controller simulator.” 2018. Masters Thesis, Delft University of Technology. Accessed April 22, 2021. http://resolver.tudelft.nl/uuid:16c8d9b6-1d07-46fa-9a4f-4c445bd9e3dc.
MLA Handbook (7th Edition):
Maltha, Rutger (author). “GOCE Spacecraft Attitude Control: A magnetic attitude controller simulator.” 2018. Web. 22 Apr 2021.
Vancouver:
Maltha R(. GOCE Spacecraft Attitude Control: A magnetic attitude controller simulator. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Apr 22]. Available from: http://resolver.tudelft.nl/uuid:16c8d9b6-1d07-46fa-9a4f-4c445bd9e3dc.
Council of Science Editors:
Maltha R(. GOCE Spacecraft Attitude Control: A magnetic attitude controller simulator. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:16c8d9b6-1d07-46fa-9a4f-4c445bd9e3dc
University of California – Berkeley
20. Wang, Yizhou. Attitude Control and Estimation.
Degree: Mechanical Engineering, 2015, University of California – Berkeley
URL: http://www.escholarship.org/uc/item/59b5d7hh
Subjects/Keywords: Mechanical engineering; Aerospace engineering; Adaptive control; Attitude control; Attitude estimation; IMU; Particle filter; Sliding mode control
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Wang, Y. (2015). Attitude Control and Estimation. (Thesis). University of California – Berkeley. Retrieved from http://www.escholarship.org/uc/item/59b5d7hh
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):
Wang, Yizhou. “Attitude Control and Estimation.” 2015. Thesis, University of California – Berkeley. Accessed April 22, 2021. http://www.escholarship.org/uc/item/59b5d7hh.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
MLA Handbook (7th Edition):
Wang, Yizhou. “Attitude Control and Estimation.” 2015. Web. 22 Apr 2021.
Vancouver:
Wang Y. Attitude Control and Estimation. [Internet] [Thesis]. University of California – Berkeley; 2015. [cited 2021 Apr 22]. Available from: http://www.escholarship.org/uc/item/59b5d7hh.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Council of Science Editors:
Wang Y. Attitude Control and Estimation. [Thesis]. University of California – Berkeley; 2015. Available from: http://www.escholarship.org/uc/item/59b5d7hh
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
University of Toronto
21. 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
URL: http://hdl.handle.net/1807/33557
Subjects/Keywords: De-orbit; Drag sail; Thermal control; Attitude determination and control; 0538
Record Details
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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 April 22, 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. 22 Apr 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 Apr 22]. 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 Connecticut
22. Liu, Yuqian. Control and Navigation of Autonomous Underwater Vehicles.
Degree: MS, Mechanical Engineering, 2014, University of Connecticut
URL: https://opencommons.uconn.edu/gs_theses/549
Subjects/Keywords: Autonomous Underwater Vehicles; Attitude Control; Adaptive Control; Fixed-point Navigation; Autopilot
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Liu, Y. (2014). Control and Navigation of Autonomous Underwater Vehicles. (Masters Thesis). University of Connecticut. Retrieved from https://opencommons.uconn.edu/gs_theses/549
Chicago Manual of Style (16th Edition):
Liu, Yuqian. “Control and Navigation of Autonomous Underwater Vehicles.” 2014. Masters Thesis, University of Connecticut. Accessed April 22, 2021. https://opencommons.uconn.edu/gs_theses/549.
MLA Handbook (7th Edition):
Liu, Yuqian. “Control and Navigation of Autonomous Underwater Vehicles.” 2014. Web. 22 Apr 2021.
Vancouver:
Liu Y. Control and Navigation of Autonomous Underwater Vehicles. [Internet] [Masters thesis]. University of Connecticut; 2014. [cited 2021 Apr 22]. Available from: https://opencommons.uconn.edu/gs_theses/549.
Council of Science Editors:
Liu Y. Control and Navigation of Autonomous Underwater Vehicles. [Masters Thesis]. University of Connecticut; 2014. Available from: https://opencommons.uconn.edu/gs_theses/549
Luleå University of Technology
23. Cypriano, Lucas Almeida. Study and Design of an Adaptive Control Law for Spacecraft Attitude Control.
Degree: 2014, Luleå University of Technology
URL: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-50766
Subjects/Keywords: Technology; Adaptive Control; RCAC; Attitude Control; ADCS; AOCS; Spacecraft; Teknik
Record Details
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APA (6th Edition):
Cypriano, L. A. (2014). Study and Design of an Adaptive Control Law for Spacecraft Attitude Control. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-50766
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):
Cypriano, Lucas Almeida. “Study and Design of an Adaptive Control Law for Spacecraft Attitude Control.” 2014. Thesis, Luleå University of Technology. Accessed April 22, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-50766.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
MLA Handbook (7th Edition):
Cypriano, Lucas Almeida. “Study and Design of an Adaptive Control Law for Spacecraft Attitude Control.” 2014. Web. 22 Apr 2021.
Vancouver:
Cypriano LA. Study and Design of an Adaptive Control Law for Spacecraft Attitude Control. [Internet] [Thesis]. Luleå University of Technology; 2014. [cited 2021 Apr 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-50766.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Council of Science Editors:
Cypriano LA. Study and Design of an Adaptive Control Law for Spacecraft Attitude Control. [Thesis]. Luleå University of Technology; 2014. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-50766
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Delft University of Technology
24. Habets, J.M.G. (author). Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft.
Degree: 2015, Delft University of Technology
URL: http://resolver.tudelft.nl/uuid:f1bc854a-36f9-4401-a892-2313e4022ea8
Subjects/Keywords: attitude control; space debris; adaptive control; evolving systems; ENVISAT
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Habets, J. M. G. (. (2015). Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f1bc854a-36f9-4401-a892-2313e4022ea8
Chicago Manual of Style (16th Edition):
Habets, J M G (author). “Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft.” 2015. Masters Thesis, Delft University of Technology. Accessed April 22, 2021. http://resolver.tudelft.nl/uuid:f1bc854a-36f9-4401-a892-2313e4022ea8.
MLA Handbook (7th Edition):
Habets, J M G (author). “Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft.” 2015. Web. 22 Apr 2021.
Vancouver:
Habets JMG(. Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Apr 22]. Available from: http://resolver.tudelft.nl/uuid:f1bc854a-36f9-4401-a892-2313e4022ea8.
Council of Science Editors:
Habets JMG(. Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:f1bc854a-36f9-4401-a892-2313e4022ea8
25. Yang, Sungpil. Robustness properties of quaternion-based attitude control systems.
Degree: PhD, Aerospace Engineering, 2016, University of Texas – Austin
URL: http://hdl.handle.net/2152/38095
Subjects/Keywords: Attitude control; Quaternion kinematics; Robustness; Adaptive control; Uncertainties; Delay; Disturbances
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Yang, S. (2016). Robustness properties of quaternion-based attitude control systems. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/38095
Chicago Manual of Style (16th Edition):
Yang, Sungpil. “Robustness properties of quaternion-based attitude control systems.” 2016. Doctoral Dissertation, University of Texas – Austin. Accessed April 22, 2021. http://hdl.handle.net/2152/38095.
MLA Handbook (7th Edition):
Yang, Sungpil. “Robustness properties of quaternion-based attitude control systems.” 2016. Web. 22 Apr 2021.
Vancouver:
Yang S. Robustness properties of quaternion-based attitude control systems. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2016. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2152/38095.
Council of Science Editors:
Yang S. Robustness properties of quaternion-based attitude control systems. [Doctoral Dissertation]. University of Texas – Austin; 2016. Available from: http://hdl.handle.net/2152/38095
Luleå University of Technology
26. Svedevall, Anders. Development of attitude determination sensors for miniature satellites.
Degree: 2014, Luleå University of Technology
URL: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-52057
Subjects/Keywords: Technology; Teknik; Sun sensor; attitude determination; pico satellite; attitude control; PSD sensor
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 April 22, 2021. 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. 22 Apr 2021.
Vancouver:
Svedevall A. Development of attitude determination sensors for miniature satellites. [Internet] [Thesis]. Luleå University of Technology; 2014. [cited 2021 Apr 22]. 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
University of Illinois – Urbana-Champaign
27. Vedant, -. Improved qualification and algorithms for illinisat-2 attitude determination and control.
Degree: MS, Aerospace Engineering, 2018, University of Illinois – Urbana-Champaign
URL: http://hdl.handle.net/2142/101238
Subjects/Keywords: Attitude Determination and Control; Control Systems; Dynamic Programming; Trajectory Planning; Underactuated Control
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
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 April 22, 2021. 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. 22 Apr 2021.
Vancouver:
Vedant -. Improved qualification and algorithms for illinisat-2 attitude determination and control. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2018. [cited 2021 Apr 22]. 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 Toronto
28. Binette, Mark Richard. An Investigation of Nonlinear Control of Spacecraft Attitude.
Degree: 2013, University of Toronto
URL: http://hdl.handle.net/1807/42688
Subjects/Keywords: H-infinity control theory; modified Rodrigues parameters; spacecraft attitude control; control theory; 0538
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Binette, M. R. (2013). An Investigation of Nonlinear Control of Spacecraft Attitude. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/42688
Chicago Manual of Style (16th Edition):
Binette, Mark Richard. “An Investigation of Nonlinear Control of Spacecraft Attitude.” 2013. Masters Thesis, University of Toronto. Accessed April 22, 2021. http://hdl.handle.net/1807/42688.
MLA Handbook (7th Edition):
Binette, Mark Richard. “An Investigation of Nonlinear Control of Spacecraft Attitude.” 2013. Web. 22 Apr 2021.
Vancouver:
Binette MR. An Investigation of Nonlinear Control of Spacecraft Attitude. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/1807/42688.
Council of Science Editors:
Binette MR. An Investigation of Nonlinear Control of Spacecraft Attitude. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/42688
Delft University of Technology
29. Fragoso Trigo, G. (author). Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs.
Degree: 2011, Delft University of Technology
URL: http://resolver.tudelft.nl/uuid:ac9a05df-7c33-4dae-9d34-5e667e6168ce
Subjects/Keywords: Spacecraft Attitude Control; Robust Control; Adaptive Control; Backstepping; Immersion and Invariance; Modified Rodrigues Parameters
Record Details
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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager
APA (6th Edition):
Fragoso Trigo, G. (. (2011). Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ac9a05df-7c33-4dae-9d34-5e667e6168ce
Chicago Manual of Style (16th Edition):
Fragoso Trigo, G (author). “Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs.” 2011. Masters Thesis, Delft University of Technology. Accessed April 22, 2021. http://resolver.tudelft.nl/uuid:ac9a05df-7c33-4dae-9d34-5e667e6168ce.
MLA Handbook (7th Edition):
Fragoso Trigo, G (author). “Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs.” 2011. Web. 22 Apr 2021.
Vancouver:
Fragoso Trigo G(. Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs. [Internet] [Masters thesis]. Delft University of Technology; 2011. [cited 2021 Apr 22]. Available from: http://resolver.tudelft.nl/uuid:ac9a05df-7c33-4dae-9d34-5e667e6168ce.
Council of Science Editors:
Fragoso Trigo G(. Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs. [Masters Thesis]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:ac9a05df-7c33-4dae-9d34-5e667e6168ce
Queensland University of Technology
30. Dando, Aaron John. Robust adaptive control of rigid spacecraft attitude maneuvers.
Degree: 2008, Queensland University of Technology
URL: https://eprints.qut.edu.au/16695/
Subjects/Keywords: spacecraft attitude control system; spacecraft attitude manevers; spacecraft attitude estimation; Lyapunov stability theory; adaptive control theory; optimal control theory; state estimation theory
Record Details
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APA (6th Edition):
Dando, A. J. (2008). Robust adaptive control of rigid spacecraft attitude maneuvers. (Thesis). Queensland University of Technology. Retrieved from https://eprints.qut.edu.au/16695/
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):
Dando, Aaron John. “Robust adaptive control of rigid spacecraft attitude maneuvers.” 2008. Thesis, Queensland University of Technology. Accessed April 22, 2021. https://eprints.qut.edu.au/16695/.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
MLA Handbook (7th Edition):
Dando, Aaron John. “Robust adaptive control of rigid spacecraft attitude maneuvers.” 2008. Web. 22 Apr 2021.
Vancouver:
Dando AJ. Robust adaptive control of rigid spacecraft attitude maneuvers. [Internet] [Thesis]. Queensland University of Technology; 2008. [cited 2021 Apr 22]. Available from: https://eprints.qut.edu.au/16695/.
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
Council of Science Editors:
Dando AJ. Robust adaptive control of rigid spacecraft attitude maneuvers. [Thesis]. Queensland University of Technology; 2008. Available from: https://eprints.qut.edu.au/16695/
Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation