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:(Spacecraft attitude control). Showing records 1 – 30 of 44 total matches.

[1] [2]

Search Limiters

Last 2 Years | English Only

Degrees

Levels

▼ Search Limiters


Lehigh University

1. 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 March 21, 2019. 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. 21 Mar 2019.

Vancouver:

Zhu S. Analysis of Spacecraft Attitude Control. [Internet] [Thesis]. Lehigh University; 2016. [cited 2019 Mar 21]. 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

2. 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 March 21, 2019. 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. 21 Mar 2019.

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 2019 Mar 21]. 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

3. 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 March 21, 2019. http://hdl.handle.net/1807/79471.

MLA Handbook (7th Edition):

Serpelloni, Edoardo. “Bang-Bang Practical Stabilization of Rigid Bodies.” 2017. Web. 21 Mar 2019.

Vancouver:

Serpelloni E. Bang-Bang Practical Stabilization of Rigid Bodies. [Internet] [Doctoral dissertation]. University of Toronto; 2017. [cited 2019 Mar 21]. 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


Queensland University of Technology

4. 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 March 21, 2019. 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. 21 Mar 2019.

Vancouver:

Dando AJ. Robust adaptive control of rigid spacecraft attitude maneuvers. [Internet] [Thesis]. Queensland University of Technology; 2008. [cited 2019 Mar 21]. 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


Virginia Tech

5. VanDyke, Matthew Clark. Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite.

Degree: PhD, Aerospace and Ocean 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 March 21, 2019. http://hdl.handle.net/10919/24911.

MLA Handbook (7th Edition):

VanDyke, Matthew Clark. “Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite.” 2014. Web. 21 Mar 2019.

Vancouver:

VanDyke MC. Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2019 Mar 21]. 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


Luleå University of Technology

6. 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 March 21, 2019. 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. 21 Mar 2019.

Vancouver:

Cypriano LA. Study and Design of an Adaptive Control Law for Spacecraft Attitude Control. [Internet] [Thesis]. Luleå University of Technology; 2014. [cited 2019 Mar 21]. 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


University of Florida

7. Leve, Frederick. Development of Spacecraft Orientation Buoyancy Experimental Kiosk.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 DEVELOPMENT OF THE SPACECRAFT ORIENTATION BUOYANCY EXPERIMENTAL KIOSK TESTBED Most satellites are unique and therefore usually take 10 to 15 years to design, fabricate, test,… (more)

Subjects/Keywords: Angular momentum; Artificial satellites; Attitude control; Flywheels; Gimbals; Momentum; Quaternions; Simulations; Spacecraft; Torque; attitude, control, reaction, satellite, spacecraft, testbed

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Leve, F. (2009). Development of Spacecraft Orientation Buoyancy Experimental Kiosk. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0022280

Chicago Manual of Style (16th Edition):

Leve, Frederick. “Development of Spacecraft Orientation Buoyancy Experimental Kiosk.” 2009. Masters Thesis, University of Florida. Accessed March 21, 2019. http://ufdc.ufl.edu/UFE0022280.

MLA Handbook (7th Edition):

Leve, Frederick. “Development of Spacecraft Orientation Buoyancy Experimental Kiosk.” 2009. Web. 21 Mar 2019.

Vancouver:

Leve F. Development of Spacecraft Orientation Buoyancy Experimental Kiosk. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Mar 21]. Available from: http://ufdc.ufl.edu/UFE0022280.

Council of Science Editors:

Leve F. Development of Spacecraft Orientation Buoyancy Experimental Kiosk. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0022280


University of Toronto

8. Stellini, Julian. Magnetic Attitude Control For Spacecraft with Flexible Appendages.

Degree: 2012, University of Toronto

The design of an attitude control system for a flexible spacecraft using magnetic actuation is considered. The nonlinear, linear, and modal equations of motion are… (more)

Subjects/Keywords: aerospace; engineering; magnetic attitude control; attitude control; flexible spacecraft; spacecraft attitude control; control of flexible appendages; spacecraft control; magnetic control; geomagnetic field; aerospace control; aerospace engineering; spacecraft dynamics; dynamics and control; dynamics; control; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Stellini, J. (2012). Magnetic Attitude Control For Spacecraft with Flexible Appendages. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/33545

Chicago Manual of Style (16th Edition):

Stellini, Julian. “Magnetic Attitude Control For Spacecraft with Flexible Appendages.” 2012. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/33545.

MLA Handbook (7th Edition):

Stellini, Julian. “Magnetic Attitude Control For Spacecraft with Flexible Appendages.” 2012. Web. 21 Mar 2019.

Vancouver:

Stellini J. Magnetic Attitude Control For Spacecraft with Flexible Appendages. [Internet] [Masters thesis]. University of Toronto; 2012. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/33545.

Council of Science Editors:

Stellini J. Magnetic Attitude Control For Spacecraft with Flexible Appendages. [Masters Thesis]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/33545


Utah State University

9. Schreiner, John N. A Neural Network Approach to Fault Detection in Spacecraft Attitude Determination and Control Systems.

Degree: MS, Mechanical and Aerospace Engineering, 2015, Utah State University

  This thesis proposes a method of performing fault detection and isolation in spacecraft attitude determination and control systems. The proposed method works by deploying… (more)

Subjects/Keywords: Neural Network; Fault Detection; Spacecraft Attitude; Control Systems; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Schreiner, J. N. (2015). A Neural Network Approach to Fault Detection in Spacecraft Attitude Determination and Control Systems. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/4164

Chicago Manual of Style (16th Edition):

Schreiner, John N. “A Neural Network Approach to Fault Detection in Spacecraft Attitude Determination and Control Systems.” 2015. Masters Thesis, Utah State University. Accessed March 21, 2019. https://digitalcommons.usu.edu/etd/4164.

MLA Handbook (7th Edition):

Schreiner, John N. “A Neural Network Approach to Fault Detection in Spacecraft Attitude Determination and Control Systems.” 2015. Web. 21 Mar 2019.

Vancouver:

Schreiner JN. A Neural Network Approach to Fault Detection in Spacecraft Attitude Determination and Control Systems. [Internet] [Masters thesis]. Utah State University; 2015. [cited 2019 Mar 21]. Available from: https://digitalcommons.usu.edu/etd/4164.

Council of Science Editors:

Schreiner JN. A Neural Network Approach to Fault Detection in Spacecraft Attitude Determination and Control Systems. [Masters Thesis]. Utah State University; 2015. Available from: https://digitalcommons.usu.edu/etd/4164


University of Manchester

10. Hao, Zhou. ORBITAL AERODYNAMIC ATTITUDE CONTROL FOR SPACECRAFT.

Degree: 2018, University of Manchester

 This dissertation introduces novel techniques for exploiting the environmental aerodynamic forces to actively control the attitude of the spacecraft operating in the lower and middle… (more)

Subjects/Keywords: spacecraft; rarefied aerodynamics; ADCS; AOCS; Attitude Control; CubeSat; space mission

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hao, Z. (2018). ORBITAL AERODYNAMIC ATTITUDE CONTROL FOR SPACECRAFT. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:315627

Chicago Manual of Style (16th Edition):

Hao, Zhou. “ORBITAL AERODYNAMIC ATTITUDE CONTROL FOR SPACECRAFT.” 2018. Doctoral Dissertation, University of Manchester. Accessed March 21, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:315627.

MLA Handbook (7th Edition):

Hao, Zhou. “ORBITAL AERODYNAMIC ATTITUDE CONTROL FOR SPACECRAFT.” 2018. Web. 21 Mar 2019.

Vancouver:

Hao Z. ORBITAL AERODYNAMIC ATTITUDE CONTROL FOR SPACECRAFT. [Internet] [Doctoral dissertation]. University of Manchester; 2018. [cited 2019 Mar 21]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:315627.

Council of Science Editors:

Hao Z. ORBITAL AERODYNAMIC ATTITUDE CONTROL FOR SPACECRAFT. [Doctoral Dissertation]. University of Manchester; 2018. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:315627


University of Manchester

11. Hao, Zhou. Orbital aerodynamic attitude control for spacecraft.

Degree: PhD, 2018, University of Manchester

 This dissertation introduces novel techniques for exploiting the environmental aerodynamic forces to actively control the attitude of the spacecraft operating in the lower and middle… (more)

Subjects/Keywords: space mission; CubeSat; Attitude Control; spacecraft; ADCS; rarefied aerodynamics; AOCS

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hao, Z. (2018). Orbital aerodynamic attitude control for spacecraft. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/orbital-aerodynamic-attitude-control-for-spacecraft(b080a1ab-f954-4071-89bd-0d86969aa0ed).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.756900

Chicago Manual of Style (16th Edition):

Hao, Zhou. “Orbital aerodynamic attitude control for spacecraft.” 2018. Doctoral Dissertation, University of Manchester. Accessed March 21, 2019. https://www.research.manchester.ac.uk/portal/en/theses/orbital-aerodynamic-attitude-control-for-spacecraft(b080a1ab-f954-4071-89bd-0d86969aa0ed).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.756900.

MLA Handbook (7th Edition):

Hao, Zhou. “Orbital aerodynamic attitude control for spacecraft.” 2018. Web. 21 Mar 2019.

Vancouver:

Hao Z. Orbital aerodynamic attitude control for spacecraft. [Internet] [Doctoral dissertation]. University of Manchester; 2018. [cited 2019 Mar 21]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/orbital-aerodynamic-attitude-control-for-spacecraft(b080a1ab-f954-4071-89bd-0d86969aa0ed).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.756900.

Council of Science Editors:

Hao Z. Orbital aerodynamic attitude control for spacecraft. [Doctoral Dissertation]. University of Manchester; 2018. Available from: https://www.research.manchester.ac.uk/portal/en/theses/orbital-aerodynamic-attitude-control-for-spacecraft(b080a1ab-f954-4071-89bd-0d86969aa0ed).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.756900


San Jose State University

12. Westfall, Alexander Joseph. Design of an Attitude Control System for Spin-Axis Control of a 3U CubeSat.

Degree: MS, Aerospace Engineering, 2015, San Jose State University

  This paper describes the design process of developing a spin-axis control system for a 3U CubeSat, a relatively small satellite. Design requires the CubeSat… (more)

Subjects/Keywords: ADCS; Aerospace; Attitude Control; CubeSat; Reaction Wheel; Spacecraft

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Westfall, A. J. (2015). Design of an Attitude Control System for Spin-Axis Control of a 3U CubeSat. (Masters Thesis). San Jose State University. Retrieved from https://scholarworks.sjsu.edu/etd_theses/4672

Chicago Manual of Style (16th Edition):

Westfall, Alexander Joseph. “Design of an Attitude Control System for Spin-Axis Control of a 3U CubeSat.” 2015. Masters Thesis, San Jose State University. Accessed March 21, 2019. https://scholarworks.sjsu.edu/etd_theses/4672.

MLA Handbook (7th Edition):

Westfall, Alexander Joseph. “Design of an Attitude Control System for Spin-Axis Control of a 3U CubeSat.” 2015. Web. 21 Mar 2019.

Vancouver:

Westfall AJ. Design of an Attitude Control System for Spin-Axis Control of a 3U CubeSat. [Internet] [Masters thesis]. San Jose State University; 2015. [cited 2019 Mar 21]. Available from: https://scholarworks.sjsu.edu/etd_theses/4672.

Council of Science Editors:

Westfall AJ. Design of an Attitude Control System for Spin-Axis Control of a 3U CubeSat. [Masters Thesis]. San Jose State University; 2015. Available from: https://scholarworks.sjsu.edu/etd_theses/4672


University of Toronto

13. 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 March 21, 2019. http://hdl.handle.net/1807/42688.

MLA Handbook (7th Edition):

Binette, Mark Richard. “An Investigation of Nonlinear Control of Spacecraft Attitude.” 2013. Web. 21 Mar 2019.

Vancouver:

Binette MR. An Investigation of Nonlinear Control of Spacecraft Attitude. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2019 Mar 21]. 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

14. Fragoso Trigo, G. 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. “Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs:.” 2011. Masters Thesis, Delft University of Technology. Accessed March 21, 2019. http://resolver.tudelft.nl/uuid:ac9a05df-7c33-4dae-9d34-5e667e6168ce.

MLA Handbook (7th Edition):

Fragoso Trigo, G. “Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs:.” 2011. Web. 21 Mar 2019.

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 2019 Mar 21]. 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


University of Toronto

15. Cotten, Scott Bradley. Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission.

Degree: 2014, University of Toronto

In the context of space debris mitigation, a major challenge currently facing the space community is the removal of nano and microsatellites from orbit following… (more)

Subjects/Keywords: Magnetic Attitude Control; Microsatellite Technology; Orbital Debris; Spacecraft Deorbiting; Thermal Control of Space Systems; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Cotten, S. B. (2014). Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/68553

Chicago Manual of Style (16th Edition):

Cotten, Scott Bradley. “Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission.” 2014. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/68553.

MLA Handbook (7th Edition):

Cotten, Scott Bradley. “Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission.” 2014. Web. 21 Mar 2019.

Vancouver:

Cotten SB. Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission. [Internet] [Masters thesis]. University of Toronto; 2014. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/68553.

Council of Science Editors:

Cotten SB. Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission. [Masters Thesis]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/68553


University of Toronto

16. Magner, Robert. Extending the Capabilities of Terrestrial Target Tracking Spacecraft.

Degree: 2018, University of Toronto

Autonomous terrestrial target tracking is performed by many communications and Earth observation missions to track ground-fixed targets. The DAUNTLESS platform, under development by the Space… (more)

Subjects/Keywords: attitude and orbital control systems; deorbit; microsatellites; spacecraft dynamics; target tracking; trajectory planning; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Magner, R. (2018). Extending the Capabilities of Terrestrial Target Tracking Spacecraft. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/91365

Chicago Manual of Style (16th Edition):

Magner, Robert. “Extending the Capabilities of Terrestrial Target Tracking Spacecraft.” 2018. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/91365.

MLA Handbook (7th Edition):

Magner, Robert. “Extending the Capabilities of Terrestrial Target Tracking Spacecraft.” 2018. Web. 21 Mar 2019.

Vancouver:

Magner R. Extending the Capabilities of Terrestrial Target Tracking Spacecraft. [Internet] [Masters thesis]. University of Toronto; 2018. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/91365.

Council of Science Editors:

Magner R. Extending the Capabilities of Terrestrial Target Tracking Spacecraft. [Masters Thesis]. University of Toronto; 2018. Available from: http://hdl.handle.net/1807/91365


University of Toronto

17. Greene, Michael R. The Attitude Determination and Control System of the Generic Nanosatellite Bus.

Degree: 2009, University of Toronto

The Generic Nanosatellite Bus (GNB) is a spacecraft platform designed to accommodate the integration of diverse payloads in a common housing of supporting components. The… (more)

Subjects/Keywords: Spacecraft Attitude Determination and Control; Nanosatellite; Sun Sensor; Star Tracker; Reaction Wheel; Magnetorquer Coil; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Greene, M. R. (2009). The Attitude Determination and Control System of the Generic Nanosatellite Bus. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/18942

Chicago Manual of Style (16th Edition):

Greene, Michael R. “The Attitude Determination and Control System of the Generic Nanosatellite Bus.” 2009. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/18942.

MLA Handbook (7th Edition):

Greene, Michael R. “The Attitude Determination and Control System of the Generic Nanosatellite Bus.” 2009. Web. 21 Mar 2019.

Vancouver:

Greene MR. The Attitude Determination and Control System of the Generic Nanosatellite Bus. [Internet] [Masters thesis]. University of Toronto; 2009. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/18942.

Council of Science Editors:

Greene MR. The Attitude Determination and Control System of the Generic Nanosatellite Bus. [Masters Thesis]. University of Toronto; 2009. Available from: http://hdl.handle.net/1807/18942


University of Toronto

18. Vatankhahghadim, Behrad. Hybrid Magnetic Attitude Control of Spacecraft: Optimality, Passivity, and Stability.

Degree: 2016, University of Toronto

Hybrid spacecraft attitude control schemes that combine magnetic torques with impulsive thrusting in an optimal or passive manner are developed. The optimal controller uses a… (more)

Subjects/Keywords: Hybrid Magnetic Attitude Control; Hybrid Stability Analysis; Optimal Control; Passivity-Based Control; Spacecraft Dynamics and Control; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Vatankhahghadim, B. (2016). Hybrid Magnetic Attitude Control of Spacecraft: Optimality, Passivity, and Stability. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/73473

Chicago Manual of Style (16th Edition):

Vatankhahghadim, Behrad. “Hybrid Magnetic Attitude Control of Spacecraft: Optimality, Passivity, and Stability.” 2016. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/73473.

MLA Handbook (7th Edition):

Vatankhahghadim, Behrad. “Hybrid Magnetic Attitude Control of Spacecraft: Optimality, Passivity, and Stability.” 2016. Web. 21 Mar 2019.

Vancouver:

Vatankhahghadim B. Hybrid Magnetic Attitude Control of Spacecraft: Optimality, Passivity, and Stability. [Internet] [Masters thesis]. University of Toronto; 2016. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/73473.

Council of Science Editors:

Vatankhahghadim B. Hybrid Magnetic Attitude Control of Spacecraft: Optimality, Passivity, and Stability. [Masters Thesis]. University of Toronto; 2016. Available from: http://hdl.handle.net/1807/73473


University of Michigan

19. Petersen, Christopher. Advances in Underactuated Spacecraft Control.

Degree: PhD, Aerospace Engineering, 2016, University of Michigan

 This dissertation addresses the control of a spacecraft which either becomes underactuated due to onboard failures or is made underactuated by design. Successfully controlling an… (more)

Subjects/Keywords: Spacecraft Dynamics and Control; Underactuated Control; Attitude Control; Coupled Rotational and Translational Relative Motion; Model Predictive Control; Aerospace Engineering; Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Petersen, C. (2016). Advances in Underactuated Spacecraft Control. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/133430

Chicago Manual of Style (16th Edition):

Petersen, Christopher. “Advances in Underactuated Spacecraft Control.” 2016. Doctoral Dissertation, University of Michigan. Accessed March 21, 2019. http://hdl.handle.net/2027.42/133430.

MLA Handbook (7th Edition):

Petersen, Christopher. “Advances in Underactuated Spacecraft Control.” 2016. Web. 21 Mar 2019.

Vancouver:

Petersen C. Advances in Underactuated Spacecraft Control. [Internet] [Doctoral dissertation]. University of Michigan; 2016. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/2027.42/133430.

Council of Science Editors:

Petersen C. Advances in Underactuated Spacecraft Control. [Doctoral Dissertation]. University of Michigan; 2016. Available from: http://hdl.handle.net/2027.42/133430


Delft University of Technology

20. Acquatella B., P.J. Robust Nonlinear Spacecraft Attitude Control: an Incremental Backstepping Approach :.

Degree: 2011, Delft University of Technology

 In order to meet requirements in terms of robustness, stability, and performance for future generations of advanced attitude control systems, a sensor-based approach using Incremental… (more)

Subjects/Keywords: Spacecraft Attitude Control; Nonlinear Control; Backstepping; Incremental Backstepping; Incremental Nonlinear Dynamic Inversion; Lyapunov-based control; Modified Rodrigues Parameters

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Acquatella B., P. J. (2011). Robust Nonlinear Spacecraft Attitude Control: an Incremental Backstepping Approach :. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a56090a3-bbce-404b-8e4b-d0e9050b518a

Chicago Manual of Style (16th Edition):

Acquatella B., P J. “Robust Nonlinear Spacecraft Attitude Control: an Incremental Backstepping Approach :.” 2011. Masters Thesis, Delft University of Technology. Accessed March 21, 2019. http://resolver.tudelft.nl/uuid:a56090a3-bbce-404b-8e4b-d0e9050b518a.

MLA Handbook (7th Edition):

Acquatella B., P J. “Robust Nonlinear Spacecraft Attitude Control: an Incremental Backstepping Approach :.” 2011. Web. 21 Mar 2019.

Vancouver:

Acquatella B. PJ. Robust Nonlinear Spacecraft Attitude Control: an Incremental Backstepping Approach :. [Internet] [Masters thesis]. Delft University of Technology; 2011. [cited 2019 Mar 21]. Available from: http://resolver.tudelft.nl/uuid:a56090a3-bbce-404b-8e4b-d0e9050b518a.

Council of Science Editors:

Acquatella B. PJ. Robust Nonlinear Spacecraft Attitude Control: an Incremental Backstepping Approach :. [Masters Thesis]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:a56090a3-bbce-404b-8e4b-d0e9050b518a


University of Texas – Austin

21. Srikant, Sukumar. Persistence filters for controller and observer design in singular gain systems.

Degree: Aerospace Engineering, 2011, University of Texas – Austin

 This dissertation develops a general framework for designing stabilizing feedback controllers and observers for dynamics with state/time dependent gains on the control signals and measured… (more)

Subjects/Keywords: Feedback control systems; Magnetic actuation; Magnetic torquers; Feedback controllers; Adaptive control; Singular gain systems; Intermittent control; Spacecraft attitude stabilization; Space vehicles

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Srikant, S. (2011). Persistence filters for controller and observer design in singular gain systems. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2011-05-3118

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):

Srikant, Sukumar. “Persistence filters for controller and observer design in singular gain systems.” 2011. Thesis, University of Texas – Austin. Accessed March 21, 2019. http://hdl.handle.net/2152/ETD-UT-2011-05-3118.

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

MLA Handbook (7th Edition):

Srikant, Sukumar. “Persistence filters for controller and observer design in singular gain systems.” 2011. Web. 21 Mar 2019.

Vancouver:

Srikant S. Persistence filters for controller and observer design in singular gain systems. [Internet] [Thesis]. University of Texas – Austin; 2011. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/2152/ETD-UT-2011-05-3118.

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

Council of Science Editors:

Srikant S. Persistence filters for controller and observer design in singular gain systems. [Thesis]. University of Texas – Austin; 2011. Available from: http://hdl.handle.net/2152/ETD-UT-2011-05-3118

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


Virginia Tech

22. Lennox, Scott Evan. Coupled Attitude And Orbital Control System Using Spacecraft Simulators.

Degree: MS, Aerospace and Ocean Engineering, 2004, Virginia Tech

 Translational and rotational motion are coupled for spacecraft performing formation flying missions. This motion is coupled because orbital control is dependent on the spacecraft attitude(more)

Subjects/Keywords: Orbital Control; Spacecraft; Attitude Control; Coupled Control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lennox, S. E. (2004). Coupled Attitude And Orbital Control System Using Spacecraft Simulators. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/10003

Chicago Manual of Style (16th Edition):

Lennox, Scott Evan. “Coupled Attitude And Orbital Control System Using Spacecraft Simulators.” 2004. Masters Thesis, Virginia Tech. Accessed March 21, 2019. http://hdl.handle.net/10919/10003.

MLA Handbook (7th Edition):

Lennox, Scott Evan. “Coupled Attitude And Orbital Control System Using Spacecraft Simulators.” 2004. Web. 21 Mar 2019.

Vancouver:

Lennox SE. Coupled Attitude And Orbital Control System Using Spacecraft Simulators. [Internet] [Masters thesis]. Virginia Tech; 2004. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/10919/10003.

Council of Science Editors:

Lennox SE. Coupled Attitude And Orbital Control System Using Spacecraft Simulators. [Masters Thesis]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/10003


University of Colorado

23. Stevenson, Daan. Remote Spacecraft Attitude Control by Coulomb Charging.

Degree: PhD, Aerospace Engineering Sciences, 2015, University of Colorado

  The possibility of inter-spacecraft collisions is a serious concern at Geosynchronous altitudes, where many high-value assets operate in proximity to countless debris objects whose… (more)

Subjects/Keywords: electrostatic modeling; high voltage experimentation; spacecraft attitude control; spacecraft charging; Multi-Vehicle Systems and Air Traffic Control; Navigation, Guidance, Control and Dynamics; Space Vehicles

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Stevenson, D. (2015). Remote Spacecraft Attitude Control by Coulomb Charging. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/94

Chicago Manual of Style (16th Edition):

Stevenson, Daan. “Remote Spacecraft Attitude Control by Coulomb Charging.” 2015. Doctoral Dissertation, University of Colorado. Accessed March 21, 2019. http://scholar.colorado.edu/asen_gradetds/94.

MLA Handbook (7th Edition):

Stevenson, Daan. “Remote Spacecraft Attitude Control by Coulomb Charging.” 2015. Web. 21 Mar 2019.

Vancouver:

Stevenson D. Remote Spacecraft Attitude Control by Coulomb Charging. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Mar 21]. Available from: http://scholar.colorado.edu/asen_gradetds/94.

Council of Science Editors:

Stevenson D. Remote Spacecraft Attitude Control by Coulomb Charging. [Doctoral Dissertation]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/94


Virginia Tech

24. Skelton, Claude Eugene II. Mixed Control Moment Gyro and Momentum Wheel Attitude Control Strategies.

Degree: MS, Aerospace and Ocean Engineering, 2003, Virginia Tech

Attitude control laws that use control moment gyros (CMGs) and momentum wheels are derived with nonlinear techniques. The control laws command the CMGs to provide… (more)

Subjects/Keywords: momentum wheel; control moment gyro; spacecraft simulator; attitude control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Skelton, C. E. I. (2003). Mixed Control Moment Gyro and Momentum Wheel Attitude Control Strategies. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/9677

Chicago Manual of Style (16th Edition):

Skelton, Claude Eugene II. “Mixed Control Moment Gyro and Momentum Wheel Attitude Control Strategies.” 2003. Masters Thesis, Virginia Tech. Accessed March 21, 2019. http://hdl.handle.net/10919/9677.

MLA Handbook (7th Edition):

Skelton, Claude Eugene II. “Mixed Control Moment Gyro and Momentum Wheel Attitude Control Strategies.” 2003. Web. 21 Mar 2019.

Vancouver:

Skelton CEI. Mixed Control Moment Gyro and Momentum Wheel Attitude Control Strategies. [Internet] [Masters thesis]. Virginia Tech; 2003. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/10919/9677.

Council of Science Editors:

Skelton CEI. Mixed Control Moment Gyro and Momentum Wheel Attitude Control Strategies. [Masters Thesis]. Virginia Tech; 2003. Available from: http://hdl.handle.net/10919/9677


University of Texas – Austin

25. -7636-3233. An attitude determination and control system for small satellites.

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

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

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

Chicago Manual of Style (16th Edition):

-7636-3233. “An attitude determination and control system for small satellites.” 2015. Thesis, University of Texas – Austin. Accessed March 21, 2019. http://hdl.handle.net/2152/31715.

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

MLA Handbook (7th Edition):

-7636-3233. “An attitude determination and control system for small satellites.” 2015. Web. 21 Mar 2019.

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

Vancouver:

-7636-3233. An attitude determination and control system for small satellites. [Internet] [Thesis]. University of Texas – Austin; 2015. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/2152/31715.

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

Council of Science Editors:

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

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


University of Illinois – Urbana-Champaign

26. Haddox, Patrick. A novel magnetic field approach to simulate spacecraft attitude determination and control.

Degree: MS, 4048, 2014, University of Illinois – Urbana-Champaign

 The University of Illinois is developing a CubeSat bus, known as IlliniSat-2, which will be capable of achieving 3-axis attitude control via magnetic torque coils… (more)

Subjects/Keywords: attitude; determination; control; magnetic field; Helmholtz coil; Helmholtz cage; cubesat; nanosatellite; satellite; spacecraft; systems toolkit (STK); LabVIEW

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Haddox, P. (2014). A novel magnetic field approach to simulate spacecraft attitude determination and control. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/49696

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):

Haddox, Patrick. “A novel magnetic field approach to simulate spacecraft attitude determination and control.” 2014. Thesis, University of Illinois – Urbana-Champaign. Accessed March 21, 2019. http://hdl.handle.net/2142/49696.

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

MLA Handbook (7th Edition):

Haddox, Patrick. “A novel magnetic field approach to simulate spacecraft attitude determination and control.” 2014. Web. 21 Mar 2019.

Vancouver:

Haddox P. A novel magnetic field approach to simulate spacecraft attitude determination and control. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2014. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/2142/49696.

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

Council of Science Editors:

Haddox P. A novel magnetic field approach to simulate spacecraft attitude determination and control. [Thesis]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/49696

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


University of Florida

27. Leve, Frederick. Novel Steering and Control Algorithms for Single-Gimbal Control Moment Gyroscopes.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2010, University of Florida

 NOVEL STEERING AND CONTROL ALGORITHMS FOR SINGLE-GIMBAL CONTROL MOMENT GYROSCOPES The research presented in this manuscript attempts to first systematically solve the SGCMG steering and… (more)

Subjects/Keywords: Acceleration; Angular momentum; Gimbals; Gyroscopes; Jacobians; Momentum; Simulations; Spacecraft; Steering; Torque; attitude, control, elliptic, hyperbolic, singularities, small, steering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Leve, F. (2010). Novel Steering and Control Algorithms for Single-Gimbal Control Moment Gyroscopes. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0042129

Chicago Manual of Style (16th Edition):

Leve, Frederick. “Novel Steering and Control Algorithms for Single-Gimbal Control Moment Gyroscopes.” 2010. Doctoral Dissertation, University of Florida. Accessed March 21, 2019. http://ufdc.ufl.edu/UFE0042129.

MLA Handbook (7th Edition):

Leve, Frederick. “Novel Steering and Control Algorithms for Single-Gimbal Control Moment Gyroscopes.” 2010. Web. 21 Mar 2019.

Vancouver:

Leve F. Novel Steering and Control Algorithms for Single-Gimbal Control Moment Gyroscopes. [Internet] [Doctoral dissertation]. University of Florida; 2010. [cited 2019 Mar 21]. Available from: http://ufdc.ufl.edu/UFE0042129.

Council of Science Editors:

Leve F. Novel Steering and Control Algorithms for Single-Gimbal Control Moment Gyroscopes. [Doctoral Dissertation]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0042129


Virginia Tech

28. Makovec, Kristin Lynne. A Nonlinear Magnetic Controller for Three-Axis Stability of Nanosatellites.

Degree: MS, Aerospace and Ocean Engineering, 2001, Virginia Tech

 The problem of magnetic control for three-axis stability of a spacecraft is examined. Two controllers, a proportional-derivative controller and a constant coefficient linear quadratic regulator,… (more)

Subjects/Keywords: Spacecraft Attitude Dynamics; Magnetic Control; Three-Axis Stability

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Makovec, K. L. (2001). A Nonlinear Magnetic Controller for Three-Axis Stability of Nanosatellites. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34131

Chicago Manual of Style (16th Edition):

Makovec, Kristin Lynne. “A Nonlinear Magnetic Controller for Three-Axis Stability of Nanosatellites.” 2001. Masters Thesis, Virginia Tech. Accessed March 21, 2019. http://hdl.handle.net/10919/34131.

MLA Handbook (7th Edition):

Makovec, Kristin Lynne. “A Nonlinear Magnetic Controller for Three-Axis Stability of Nanosatellites.” 2001. Web. 21 Mar 2019.

Vancouver:

Makovec KL. A Nonlinear Magnetic Controller for Three-Axis Stability of Nanosatellites. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/10919/34131.

Council of Science Editors:

Makovec KL. A Nonlinear Magnetic Controller for Three-Axis Stability of Nanosatellites. [Masters Thesis]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/34131

29. Ahn, Young Tae. Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution.

Degree: PhD, Aerospace Engineering, 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

…desired direction, a spacecraft needs specific attitude control methods that are dependent on… …included. Chapter 2 BACKGROUND A spacecraft attitude control system, as seen in the block… …Spacecraft Attitude Dynamics and Control [1] 2.1 Literature Review Enormous amounts of… …spacecraft attitude control method using a linear quadratic regulator algorithm. Since a… …helped me relax and kept me fresh. Chapter 1 INTRODUCTION A general spacecraft attitude… 

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. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/16015

Chicago Manual of Style (16th Edition):

Ahn, Young Tae. “Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution.” 2012. Doctoral Dissertation, Penn State University. Accessed March 21, 2019. https://etda.libraries.psu.edu/catalog/16015.

MLA Handbook (7th Edition):

Ahn, Young Tae. “Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution.” 2012. Web. 21 Mar 2019.

Vancouver:

Ahn YT. Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution. [Internet] [Doctoral dissertation]. Penn State University; 2012. [cited 2019 Mar 21]. Available from: https://etda.libraries.psu.edu/catalog/16015.

Council of Science Editors:

Ahn YT. Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution. [Doctoral Dissertation]. Penn State University; 2012. Available from: https://etda.libraries.psu.edu/catalog/16015


Indian Institute of Science

30. Joseph, Thomas K. Dynamic Response Of A Satellite With Flexible Appendages And Its Passive Control.

Degree: 2009, Indian Institute of Science

 Most present day spacecrafts have large interconnected solar panels. The dynamic behavior of the spacecraft in orbit can be modeled as a free rigid mass… (more)

Subjects/Keywords: Artificial Satellite - Dynamics; Space Vehicle - Dynamics; Space Vehicles - Control Systems; Artificial Satellites - Attitude Control Systems; Flexible Spacecraft Control; Viscoelastic Layer Damping; Passive Damping Treatment; Astronautics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Joseph, T. K. (2009). Dynamic Response Of A Satellite With Flexible Appendages And Its Passive Control. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/943

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):

Joseph, Thomas K. “Dynamic Response Of A Satellite With Flexible Appendages And Its Passive Control.” 2009. Thesis, Indian Institute of Science. Accessed March 21, 2019. http://hdl.handle.net/2005/943.

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

MLA Handbook (7th Edition):

Joseph, Thomas K. “Dynamic Response Of A Satellite With Flexible Appendages And Its Passive Control.” 2009. Web. 21 Mar 2019.

Vancouver:

Joseph TK. Dynamic Response Of A Satellite With Flexible Appendages And Its Passive Control. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/2005/943.

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

Council of Science Editors:

Joseph TK. Dynamic Response Of A Satellite With Flexible Appendages And Its Passive Control. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/943

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

[1] [2]

.