Advanced search options

Advanced Search Options 🞨

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

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(Attitude Control). Showing records 1 – 30 of 344 total matches.

[1] [2] [3] [4] [5] … [12]

Search Limiters

Last 2 Years | English Only

Degrees

Levels

Languages

Country

▼ Search Limiters


Delft University of Technology

1. van Hengel, Anita (author). Magnetorquer Design and Attitude Control for SHAPE.

Degree: 2018, Delft University of Technology

Designing and modelling a magnetorquer, and developing an attitude control loop, with magnetorquers as only actuators, for the Stable and Highly Accurate Pointing Earth-Imager (SHAPE),… (more)

Subjects/Keywords: Attitude control; SHAPE; Magnetorquer

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

This paper presents an attitude controller for a small helicopter Unmanned Aerial Vehicle (UAV) based on Incremental Nonlinear Dynamic Inversion (INDI). INDI is a sensor-based… (more)

Subjects/Keywords: INDI helicopter uav control attitude

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

 SOCRATES and IMPRESS are two cubesats designed and built by the University of Minnesota's Small Satellite Team. These satellites have similar build and function by… (more)

Subjects/Keywords: attitude; control; cubesat; magnetic; magnetorquers

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

 The thesis studies about repositioning the spacecraft to obtain a moving target problem. We model the spacecraft as a rigid body with axis torque controlling… (more)

Subjects/Keywords: alalysis of spacecraft attitude control; analysis control; attitude; attitude control; attitude of spacecraft; spacecraft control; Engineering; Mechanical Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

A clear understanding of the knowledge, attitudes and practices of a particular community can inform the design of Behaviour Change Communication (BCC) campaigns to influence… (more)

Subjects/Keywords: Knowledge, attitude; Malaria control; Akuapim

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

 This study designs and analyzes a new type of controller that helps improve the performance of single axis attitude control of flexible appendages attached to… (more)

Subjects/Keywords: Aerospace engineering; Spacecraft dynamics; Control systems; Acceleration feedback; PIDA; PID; Attitude control; Classical control; Spacecraft attitude control; Single axis attitude control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

Attitude control of spacecraft in low Earth orbits can be achieved by exploiting the torques generated by the geomagnetic field. Recent research has demonstrated that… (more)

Subjects/Keywords: hybrid attitude control; magnetic attitudde control; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Ibrahim, Najmus. “Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.” 2013. Masters Thesis, University of Toronto. Accessed 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

 This dissertation presents two major research contributions to the field of attitude dynamics and control. The first topic comprises of estimating the angular velocity of… (more)

Subjects/Keywords: Quaternion; Attitude control; Attitude estimation; Slam; Quaternion regression; Finite time control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

 In this thesis, we study the problem of designing a practical stabilizer for a rigid body equipped with a set of actuators generating only constant… (more)

Subjects/Keywords: Attitude Control; Bang-Bang Control; Double-Integrator Control; Spacecraft Control; 0544

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

 This dissertation investigates attitude transition maneuvers of a gyrosat-satellite between relative equilibria. The primary challenge in transitioning between relative equilibria is the proper adjustment of… (more)

Subjects/Keywords: Gyrostat-Satellite; Relative Equilibrium; Spacecraft Dynamics; Attitude Control; Attitude Guidance; Gravitational Torque; Attitude Maneuvers

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

 Spacecraft need specific attitude control methods that depend on the mission type or special tasks. The dynamics and the attitude control of a spacecraft with… (more)

Subjects/Keywords: spacecraft attitude dynamics; attitude control; combinatorial optimization theory

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

In a spacecraft development cycle, components must undergo a rigorous regime of testing, known as acceptance testing, to ensure that they can operate in the… (more)

Subjects/Keywords: Attitude; Control; Microsatellite; Nanosatellite; Satellite; Small; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

The problem of attitude control of a flexible satellite using magnetic attitude control is investigated. The work is motivated by JC2Sat - a joint CSA… (more)

Subjects/Keywords: magnetic attitude control; multibody dynamics; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

 This thesis presents a novel small satellite star tracker that uses an array of low-cost, off the shelf imaging sensors to achieve high accuracy attitude(more)

Subjects/Keywords: Star Tracker; Attitude Determination and Control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

  The Utah State University Propulsion Research Laboratory (USUPRL) has recently made significant developments in the area of hybrid rocket systems. This type of propulsion… (more)

Subjects/Keywords: Hybrid; Attitude; Control; Rocket; Slosh; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

  There are two traditional aircraft categories: fixed-wing which have a long endurance and a high cruise airspeed and rotorcraft which can take-off and land… (more)

Subjects/Keywords: attitude control; attitude error; guidance and control; tailsitter; TECS; VTOL; Electrical and Computer Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

 Given the difficulty that is normally associated with tuning highly nonlinear control systems, such as seen in LEO spacecraft, it is interesting to evaluate how… (more)

Subjects/Keywords: Genetic algorithm; INDI; Attitude control; GOCE; Spacecraft torque models; Magnetic attitude control; NDI

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

 The attitude control problem, or the control of a spacecraft's orientation with respect to a frame of reference, is a challenging problem in space missions… (more)

Subjects/Keywords: Mechanical engineering; Aerospace engineering; Adaptive control; Attitude control; Attitude estimation; IMU; Particle filter; Sliding mode control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Tarantini, Vincent. “Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite.” 2012. Masters Thesis, University of Toronto. Accessed 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

  This thesis presents an efficient attitude control design, which combined L1 adaptive control and backstepping control together. Based on this attitude controller, a design… (more)

Subjects/Keywords: Autonomous Underwater Vehicles; Attitude Control; Adaptive Control; Fixed-point Navigation; Autopilot

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

In this thesis the problem of spacecraft attitude control is investigated. The spacecraft dynamics are modeled as a rigid body system controlled by 4… (more)

Subjects/Keywords: Technology; Adaptive Control; RCAC; Attitude Control; ADCS; AOCS; Spacecraft; Teknik

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

 Space debris has become a major issue for the space industry over the last couple of years. The increasing number of uncontrolled objects in space… (more)

Subjects/Keywords: attitude control; space debris; adaptive control; evolving systems; ENVISAT

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

 Both stabilizing and tracking solutions of the rigid-body attitude control problem, using various attitude representations, are now well understood. Based on the sensor availability, numerous… (more)

Subjects/Keywords: Attitude control; Quaternion kinematics; Robustness; Adaptive control; Uncertainties; Delay; Disturbances

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

The design of controllers subject to the nonlinear H-infinity criterion is explored. The plants to be controlled are the attitude motion of spacecraft, subject to… (more)

Subjects/Keywords: H-infinity control theory; modified Rodrigues parameters; spacecraft attitude control; control theory; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

In the context of the initiative Formation for Atmospheric Science and Technology demonstration (FAST), this dissertation describes the design and comparison of several nonlinear attitude(more)

Subjects/Keywords: Spacecraft Attitude Control; Robust Control; Adaptive Control; Backstepping; Immersion and Invariance; Modified Rodrigues Parameters

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

 In this thesis novel feedback attitude control algorithms and attitude estimation algorithms are developed for a three-axis stabilised spacecraft attitude control system. The spacecraft models… (more)

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 DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

[1] [2] [3] [4] [5] … [12]

.