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You searched for subject:(Attitude Dynamics). Showing records 1 – 30 of 60 total matches.

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Virginia Tech

1. 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

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APA (6th Edition):

VanDyke, M. C. (2014). Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/24911

Chicago Manual of Style (16th Edition):

VanDyke, Matthew Clark. “Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite.” 2014. Doctoral Dissertation, Virginia Tech. Accessed March 08, 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. 08 Mar 2021.

Vancouver:

VanDyke MC. Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2021 Mar 08]. 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

2. 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

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APA (6th Edition):

Ahn, Y. T. (2012). Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/16015

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

Chicago Manual of Style (16th Edition):

Ahn, Young Tae. “Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution.” 2012. Thesis, Penn State University. Accessed March 08, 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. 08 Mar 2021.

Vancouver:

Ahn YT. Attitude Dynamics and Control of a Spacecraft Using Shifting Mass Distribution. [Internet] [Thesis]. Penn State University; 2012. [cited 2021 Mar 08]. 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

3. 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

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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 March 08, 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. 08 Mar 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 Mar 08]. 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

4. Krzysztof, Krzysztof. Attitude toward public sculpture as a group dynamic process adaptation of the Kurt Lewin's force field concept into art theory.

Degree: PhD, 2018, Ulster University

 Would contemporary sculpture in the public space evoke a certain kind of a group dynamic processes? The thesis is dedicated to the role and perception… (more)

Subjects/Keywords: Public Space; Sculpture; Group Dynamics; Attitude

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APA (6th Edition):

Krzysztof, K. (2018). Attitude toward public sculpture as a group dynamic process adaptation of the Kurt Lewin's force field concept into art theory. (Doctoral Dissertation). Ulster University. Retrieved from https://ulster.pure.elsevier.com/en/studentTheses/d6a2976b-ac1d-4bc8-9610-09f6be0867a3 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.793676

Chicago Manual of Style (16th Edition):

Krzysztof, Krzysztof. “Attitude toward public sculpture as a group dynamic process adaptation of the Kurt Lewin's force field concept into art theory.” 2018. Doctoral Dissertation, Ulster University. Accessed March 08, 2021. https://ulster.pure.elsevier.com/en/studentTheses/d6a2976b-ac1d-4bc8-9610-09f6be0867a3 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.793676.

MLA Handbook (7th Edition):

Krzysztof, Krzysztof. “Attitude toward public sculpture as a group dynamic process adaptation of the Kurt Lewin's force field concept into art theory.” 2018. Web. 08 Mar 2021.

Vancouver:

Krzysztof K. Attitude toward public sculpture as a group dynamic process adaptation of the Kurt Lewin's force field concept into art theory. [Internet] [Doctoral dissertation]. Ulster University; 2018. [cited 2021 Mar 08]. Available from: https://ulster.pure.elsevier.com/en/studentTheses/d6a2976b-ac1d-4bc8-9610-09f6be0867a3 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.793676.

Council of Science Editors:

Krzysztof K. Attitude toward public sculpture as a group dynamic process adaptation of the Kurt Lewin's force field concept into art theory. [Doctoral Dissertation]. Ulster University; 2018. Available from: https://ulster.pure.elsevier.com/en/studentTheses/d6a2976b-ac1d-4bc8-9610-09f6be0867a3 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.793676


York University

5. 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

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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 08, 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. 08 Mar 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 Mar 08]. 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

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

Degree: PhD, 2020, University of Toronto

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Hakima, Houman. “A New Approach to Active Removal of Space Debris.” 2020. Doctoral Dissertation, University of Toronto. Accessed March 08, 2021. http://hdl.handle.net/1807/101359.

MLA Handbook (7th Edition):

Hakima, Houman. “A New Approach to Active Removal of Space Debris.” 2020. Web. 08 Mar 2021.

Vancouver:

Hakima H. A New Approach to Active Removal of Space Debris. [Internet] [Doctoral dissertation]. University of Toronto; 2020. [cited 2021 Mar 08]. Available from: http://hdl.handle.net/1807/101359.

Council of Science Editors:

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


University of Colorado

7. Guerrant, Daniel Vernon. Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis.

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

  Solar sails enable or enhance exploration of a variety of destinations both within and without the solar system. The heliogyro solar sail architecture divides… (more)

Subjects/Keywords: attitude control; dynamics; heliogyro; solar sail; structural dynamics; Astrodynamics; Propulsion and Power; Space Vehicles

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APA (6th Edition):

Guerrant, D. V. (2015). Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/101

Chicago Manual of Style (16th Edition):

Guerrant, Daniel Vernon. “Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis.” 2015. Doctoral Dissertation, University of Colorado. Accessed March 08, 2021. https://scholar.colorado.edu/asen_gradetds/101.

MLA Handbook (7th Edition):

Guerrant, Daniel Vernon. “Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis.” 2015. Web. 08 Mar 2021.

Vancouver:

Guerrant DV. Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2021 Mar 08]. Available from: https://scholar.colorado.edu/asen_gradetds/101.

Council of Science Editors:

Guerrant DV. Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/101


Rochester Institute of Technology

8. Scorse, William. Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array.

Degree: Mechanical Engineering, 2011, Rochester Institute of Technology

 In this thesis, a previously developed, novel one-dimensional attitude estimation device is expanded through the development and implementation of an innovative method for estimation of… (more)

Subjects/Keywords: Attitude estimation; Bias estimation; Euler kinematics; Kalman filtering; Rigid body dynamics

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APA (6th Edition):

Scorse, W. (2011). Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/5803

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):

Scorse, William. “Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array.” 2011. Thesis, Rochester Institute of Technology. Accessed March 08, 2021. https://scholarworks.rit.edu/theses/5803.

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

MLA Handbook (7th Edition):

Scorse, William. “Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array.” 2011. Web. 08 Mar 2021.

Vancouver:

Scorse W. Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array. [Internet] [Thesis]. Rochester Institute of Technology; 2011. [cited 2021 Mar 08]. Available from: https://scholarworks.rit.edu/theses/5803.

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

Council of Science Editors:

Scorse W. Two dimensional rate gyro bias estimation for precise pitch and roll attitude determination utilizing a dual arc accelerometer array. [Thesis]. Rochester Institute of Technology; 2011. Available from: https://scholarworks.rit.edu/theses/5803

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

9. Berkane, Soulaimane. Hybrid Attitude Control and Estimation On SO(3).

Degree: 2017, University of Western Ontario

 This thesis presents a general framework for hybrid attitude control and estimation design on the Special Orthogonal group SO(3). First, the attitude stabilization problem on… (more)

Subjects/Keywords: Attitude control; Attitude estimation; Hybrid systems; Special Orthogonal group; Intermittent measurements; synergistic hybrid feedback; Acoustics, Dynamics, and Controls; Aerospace Engineering; Controls and Control Theory; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Berkane, S. (2017). Hybrid Attitude Control and Estimation On SO(3). (Thesis). University of Western Ontario. Retrieved from https://ir.lib.uwo.ca/etd/5083

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):

Berkane, Soulaimane. “Hybrid Attitude Control and Estimation On SO(3).” 2017. Thesis, University of Western Ontario. Accessed March 08, 2021. https://ir.lib.uwo.ca/etd/5083.

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

MLA Handbook (7th Edition):

Berkane, Soulaimane. “Hybrid Attitude Control and Estimation On SO(3).” 2017. Web. 08 Mar 2021.

Vancouver:

Berkane S. Hybrid Attitude Control and Estimation On SO(3). [Internet] [Thesis]. University of Western Ontario; 2017. [cited 2021 Mar 08]. Available from: https://ir.lib.uwo.ca/etd/5083.

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

Council of Science Editors:

Berkane S. Hybrid Attitude Control and Estimation On SO(3). [Thesis]. University of Western Ontario; 2017. Available from: https://ir.lib.uwo.ca/etd/5083

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


Ryerson University

10. Manzoor, Waqas A. A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point.

Degree: 2011, Ryerson University

 This thesis examines the performance of control methods that fall under the optimal, predictive and adaptive classifications, subjected to sensor/actuator faults, and presents approaches to… (more)

Subjects/Keywords: Space vehicles  – Dynamics; Space vehicles  – Attitude control systems; Solar sails; Space trajectories

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APA (6th Edition):

Manzoor, W. A. (2011). A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1814

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):

Manzoor, Waqas A. “A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point.” 2011. Thesis, Ryerson University. Accessed March 08, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A1814.

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

MLA Handbook (7th Edition):

Manzoor, Waqas A. “A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point.” 2011. Web. 08 Mar 2021.

Vancouver:

Manzoor WA. A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point. [Internet] [Thesis]. Ryerson University; 2011. [cited 2021 Mar 08]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1814.

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

Council of Science Editors:

Manzoor WA. A Comparative Study of Formation Control at the Earth-Moon L₂ Libration Point. [Thesis]. Ryerson University; 2011. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1814

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


Ryerson University

11. Vaz, Brendon. Online calibration for star trackers.

Degree: 2013, Ryerson University

 Star trackers are perhaps the most accurate means of measuring a spacecraft's orientation in space and are becoming a popular sensing instrument for attitude determination… (more)

Subjects/Keywords: Star trackers; Star tracking systems; Space vehicles  – Attitude control systems; Space vehicles  – Dynamics

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APA (6th Edition):

Vaz, B. (2013). Online calibration for star trackers. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A2874

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):

Vaz, Brendon. “Online calibration for star trackers.” 2013. Thesis, Ryerson University. Accessed March 08, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A2874.

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

MLA Handbook (7th Edition):

Vaz, Brendon. “Online calibration for star trackers.” 2013. Web. 08 Mar 2021.

Vancouver:

Vaz B. Online calibration for star trackers. [Internet] [Thesis]. Ryerson University; 2013. [cited 2021 Mar 08]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A2874.

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

Council of Science Editors:

Vaz B. Online calibration for star trackers. [Thesis]. Ryerson University; 2013. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A2874

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


University of Toronto

12. 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

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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 08, 2021. http://hdl.handle.net/1807/91365.

MLA Handbook (7th Edition):

Magner, Robert. “Extending the Capabilities of Terrestrial Target Tracking Spacecraft.” 2018. Web. 08 Mar 2021.

Vancouver:

Magner R. Extending the Capabilities of Terrestrial Target Tracking Spacecraft. [Internet] [Masters thesis]. University of Toronto; 2018. [cited 2021 Mar 08]. 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 Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Gerhardt, David Thomas. “Small Satellite Passive Magnetic Attitude Control.” 2014. Doctoral Dissertation, University of Colorado. Accessed March 08, 2021. https://scholar.colorado.edu/asen_gradetds/78.

MLA Handbook (7th Edition):

Gerhardt, David Thomas. “Small Satellite Passive Magnetic Attitude Control.” 2014. Web. 08 Mar 2021.

Vancouver:

Gerhardt DT. Small Satellite Passive Magnetic Attitude Control. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2021 Mar 08]. Available from: https://scholar.colorado.edu/asen_gradetds/78.

Council of Science Editors:

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


University of Toronto

14. Choi, Mirue. Flexible Dynamics and Attitude Control of a Square Solar Sail.

Degree: PhD, 2015, University of Toronto

 This thesis presents a comprehensive analysis of attitude and structural dynamics of a square solar sail. In particular, this research examines the use of corner-attached… (more)

Subjects/Keywords: Attitude Control; Control Allocation; Finite Element Method; Flexible Dynamics; Solar Sail; Wrinkling; 0538

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APA (6th Edition):

Choi, M. (2015). Flexible Dynamics and Attitude Control of a Square Solar Sail. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/69253

Chicago Manual of Style (16th Edition):

Choi, Mirue. “Flexible Dynamics and Attitude Control of a Square Solar Sail.” 2015. Doctoral Dissertation, University of Toronto. Accessed March 08, 2021. http://hdl.handle.net/1807/69253.

MLA Handbook (7th Edition):

Choi, Mirue. “Flexible Dynamics and Attitude Control of a Square Solar Sail.” 2015. Web. 08 Mar 2021.

Vancouver:

Choi M. Flexible Dynamics and Attitude Control of a Square Solar Sail. [Internet] [Doctoral dissertation]. University of Toronto; 2015. [cited 2021 Mar 08]. Available from: http://hdl.handle.net/1807/69253.

Council of Science Editors:

Choi M. Flexible Dynamics and Attitude Control of a Square Solar Sail. [Doctoral Dissertation]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/69253


University of Waterloo

15. Koldychev, Mikhail. Observers on linear Lie groups with linear estimation error dynamics.

Degree: 2012, University of Waterloo

 A major motivation for Lie group observers is their application as sensor fusion algorithms for an inertial measurement unit which can be used to estimate… (more)

Subjects/Keywords: observer; lie group; high-gain observer; inertial measurement; attitude estimation; linear error dynamics

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APA (6th Edition):

Koldychev, M. (2012). Observers on linear Lie groups with linear estimation error dynamics. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/7001

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):

Koldychev, Mikhail. “Observers on linear Lie groups with linear estimation error dynamics.” 2012. Thesis, University of Waterloo. Accessed March 08, 2021. http://hdl.handle.net/10012/7001.

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

MLA Handbook (7th Edition):

Koldychev, Mikhail. “Observers on linear Lie groups with linear estimation error dynamics.” 2012. Web. 08 Mar 2021.

Vancouver:

Koldychev M. Observers on linear Lie groups with linear estimation error dynamics. [Internet] [Thesis]. University of Waterloo; 2012. [cited 2021 Mar 08]. Available from: http://hdl.handle.net/10012/7001.

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

Council of Science Editors:

Koldychev M. Observers on linear Lie groups with linear estimation error dynamics. [Thesis]. University of Waterloo; 2012. Available from: http://hdl.handle.net/10012/7001

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

16. Ashouri Rad, Armin. Three Essays on Dynamics of Online Communities.

Degree: PhD, Industrial and Systems Engineering, 2016, Virginia Tech

 Essay1: Reconstructing Online Behavior through Effort Minimization Data from online interactions increasingly informs our understanding of fundamental patterns of human behavior as well as commercial… (more)

Subjects/Keywords: Dynamics of opinion; opinion space; attitude measuring; online communities; online behaviors; users' activity

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APA (6th Edition):

Ashouri Rad, A. (2016). Three Essays on Dynamics of Online Communities. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71641

Chicago Manual of Style (16th Edition):

Ashouri Rad, Armin. “Three Essays on Dynamics of Online Communities.” 2016. Doctoral Dissertation, Virginia Tech. Accessed March 08, 2021. http://hdl.handle.net/10919/71641.

MLA Handbook (7th Edition):

Ashouri Rad, Armin. “Three Essays on Dynamics of Online Communities.” 2016. Web. 08 Mar 2021.

Vancouver:

Ashouri Rad A. Three Essays on Dynamics of Online Communities. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2021 Mar 08]. Available from: http://hdl.handle.net/10919/71641.

Council of Science Editors:

Ashouri Rad A. Three Essays on Dynamics of Online Communities. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71641


University of Colorado

17. Rizvi, Farheen. Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects.

Degree: MS, Aerospace Engineering Sciences, 2010, University of Colorado

  In this thesis, a control method is developed for the solar sail normal vector to trace a desired circular coning trajectory at orbit rate.… (more)

Subjects/Keywords: attitude dynamics and control; coning control; control methods; Solar sail; Aerospace Engineering; Navigation, Guidance, Control and Dynamics; Space Vehicles

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APA (6th Edition):

Rizvi, F. (2010). Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/8

Chicago Manual of Style (16th Edition):

Rizvi, Farheen. “Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects.” 2010. Masters Thesis, University of Colorado. Accessed March 08, 2021. https://scholar.colorado.edu/asen_gradetds/8.

MLA Handbook (7th Edition):

Rizvi, Farheen. “Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects.” 2010. Web. 08 Mar 2021.

Vancouver:

Rizvi F. Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects. [Internet] [Masters thesis]. University of Colorado; 2010. [cited 2021 Mar 08]. Available from: https://scholar.colorado.edu/asen_gradetds/8.

Council of Science Editors:

Rizvi F. Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects. [Masters Thesis]. University of Colorado; 2010. Available from: https://scholar.colorado.edu/asen_gradetds/8

18. Abdallah, Ayman Muhammad. Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope.

Degree: PhD, Aerospace Engineering, 2015, Old Dominion University

  A new asymmetric level aerodynamic attitude flight envelope is introduced in this dissertation. The aerodynamic attitude envelope is an angle of attack vs. sideslip… (more)

Subjects/Keywords: Aerodynamic attitude flight envelope; Airplanes; Speed; Flight dynamics; Aerodynamics and Fluid Mechanics; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Abdallah, A. M. (2015). Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781339125831 ; https://digitalcommons.odu.edu/mae_etds/107

Chicago Manual of Style (16th Edition):

Abdallah, Ayman Muhammad. “Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope.” 2015. Doctoral Dissertation, Old Dominion University. Accessed March 08, 2021. 9781339125831 ; https://digitalcommons.odu.edu/mae_etds/107.

MLA Handbook (7th Edition):

Abdallah, Ayman Muhammad. “Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope.” 2015. Web. 08 Mar 2021.

Vancouver:

Abdallah AM. Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope. [Internet] [Doctoral dissertation]. Old Dominion University; 2015. [cited 2021 Mar 08]. Available from: 9781339125831 ; https://digitalcommons.odu.edu/mae_etds/107.

Council of Science Editors:

Abdallah AM. Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope. [Doctoral Dissertation]. Old Dominion University; 2015. Available from: 9781339125831 ; https://digitalcommons.odu.edu/mae_etds/107


University of Toronto

19. 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

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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 08, 2021. http://hdl.handle.net/1807/33545.

MLA Handbook (7th Edition):

Stellini, Julian. “Magnetic Attitude Control For Spacecraft with Flexible Appendages.” 2012. Web. 08 Mar 2021.

Vancouver:

Stellini J. Magnetic Attitude Control For Spacecraft with Flexible Appendages. [Internet] [Masters thesis]. University of Toronto; 2012. [cited 2021 Mar 08]. 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


University of Kentucky

20. Bezold, Maxwell. AN ATTITUDE DETERMINATION SYSTEM WITH MEMS GYROSCOPE DRIFT COMPENSATION FOR SMALL SATELLITES.

Degree: 2013, University of Kentucky

 This thesis presents the design of an attitude determination system for small satellites that automatically corrects for attitude drift. Existing attitude determination systems suffer from… (more)

Subjects/Keywords: Extended Kalman Filter; CubeSat; Attitude Determination Stellar Gyro; Attitude Drift; Controls and Control Theory; Navigation, Guidance, Control and Dynamics; Signal Processing; Space Vehicles

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APA (6th Edition):

Bezold, M. (2013). AN ATTITUDE DETERMINATION SYSTEM WITH MEMS GYROSCOPE DRIFT COMPENSATION FOR SMALL SATELLITES. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/ece_etds/29

Chicago Manual of Style (16th Edition):

Bezold, Maxwell. “AN ATTITUDE DETERMINATION SYSTEM WITH MEMS GYROSCOPE DRIFT COMPENSATION FOR SMALL SATELLITES.” 2013. Masters Thesis, University of Kentucky. Accessed March 08, 2021. https://uknowledge.uky.edu/ece_etds/29.

MLA Handbook (7th Edition):

Bezold, Maxwell. “AN ATTITUDE DETERMINATION SYSTEM WITH MEMS GYROSCOPE DRIFT COMPENSATION FOR SMALL SATELLITES.” 2013. Web. 08 Mar 2021.

Vancouver:

Bezold M. AN ATTITUDE DETERMINATION SYSTEM WITH MEMS GYROSCOPE DRIFT COMPENSATION FOR SMALL SATELLITES. [Internet] [Masters thesis]. University of Kentucky; 2013. [cited 2021 Mar 08]. Available from: https://uknowledge.uky.edu/ece_etds/29.

Council of Science Editors:

Bezold M. AN ATTITUDE DETERMINATION SYSTEM WITH MEMS GYROSCOPE DRIFT COMPENSATION FOR SMALL SATELLITES. [Masters Thesis]. University of Kentucky; 2013. Available from: https://uknowledge.uky.edu/ece_etds/29


Rochester Institute of Technology

21. Weisman, Ryan. Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array.

Degree: Mechanical Engineering, 2008, Rochester Institute of Technology

 In this thesis, a novel attitude estimation device is proposed utilizing cost-effective measurement sensors. The device fuses a rate gyroscope with an accelerometer array to… (more)

Subjects/Keywords: Attitude estimation; Bias estimation; Kalman filtering; Rigid body dynamics

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APA (6th Edition):

Weisman, R. (2008). Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/5807

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):

Weisman, Ryan. “Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array.” 2008. Thesis, Rochester Institute of Technology. Accessed March 08, 2021. https://scholarworks.rit.edu/theses/5807.

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

MLA Handbook (7th Edition):

Weisman, Ryan. “Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array.” 2008. Web. 08 Mar 2021.

Vancouver:

Weisman R. Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array. [Internet] [Thesis]. Rochester Institute of Technology; 2008. [cited 2021 Mar 08]. Available from: https://scholarworks.rit.edu/theses/5807.

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

Council of Science Editors:

Weisman R. Robust longitudinal rate gyro bias estimation for reliable pitch attitude observation through utilization of a displaced accelerometer array. [Thesis]. Rochester Institute of Technology; 2008. Available from: https://scholarworks.rit.edu/theses/5807

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

22. Maria Cecilia Pereira de Faria. Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta.

Degree: 2009, Instituto Nacional de Pesquisas Espaciais

Neste trabalho foi realizado um estudo das propriedades dinâmicas de um sistema propulsor que utiliza radiação solar. Foram desenvolvidos modelos de força e torque para… (more)

Subjects/Keywords: vela solar; dinâmica orbital; atitude; controle; baixo empuxo; solar sail; orbital dynamics; attitude; control; low thrust

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APA (6th Edition):

Faria, M. C. P. d. (2009). Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2009/06.17.20.21

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):

Faria, Maria Cecilia Pereira de. “Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta.” 2009. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed March 08, 2021. http://urlib.net/sid.inpe.br/[email protected]/2009/06.17.20.21.

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

MLA Handbook (7th Edition):

Faria, Maria Cecilia Pereira de. “Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta.” 2009. Web. 08 Mar 2021.

Vancouver:

Faria MCPd. Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. [cited 2021 Mar 08]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/06.17.20.21.

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

Council of Science Editors:

Faria MCPd. Dinâmica orbital e controle de orientação de um veículo espacial com uma vela solar composta. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/06.17.20.21

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

23. Fulvio Bianco Prevot. Dynamics of separation between the last stage of launching vehicle and the satellite - separation systems.

Degree: 2009, Instituto Nacional de Pesquisas Espaciais

Este trabalho trata da dinâmica da separação entre o último estágio do veículo lançador e o satélite, considerando a atuação do mecanismo de separação, bem… (more)

Subjects/Keywords: Colisão; Atitude; Sistemas de separação; Separation dynamics; Attitude (inclination); Dinâmica de separação; Análise dinâmica; Collision; Dynamic Analysis; Separation systems

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APA (6th Edition):

Prevot, F. B. (2009). Dynamics of separation between the last stage of launching vehicle and the satellite - separation systems. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2009/07.03.19.22

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):

Prevot, Fulvio Bianco. “Dynamics of separation between the last stage of launching vehicle and the satellite - separation systems.” 2009. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed March 08, 2021. http://urlib.net/sid.inpe.br/[email protected]/2009/07.03.19.22.

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

MLA Handbook (7th Edition):

Prevot, Fulvio Bianco. “Dynamics of separation between the last stage of launching vehicle and the satellite - separation systems.” 2009. Web. 08 Mar 2021.

Vancouver:

Prevot FB. Dynamics of separation between the last stage of launching vehicle and the satellite - separation systems. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. [cited 2021 Mar 08]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/07.03.19.22.

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

Council of Science Editors:

Prevot FB. Dynamics of separation between the last stage of launching vehicle and the satellite - separation systems. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/07.03.19.22

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


University of Michigan

24. 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

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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 08, 2021. http://hdl.handle.net/2027.42/133430.

MLA Handbook (7th Edition):

Petersen, Christopher. “Advances in Underactuated Spacecraft Control.” 2016. Web. 08 Mar 2021.

Vancouver:

Petersen C. Advances in Underactuated Spacecraft Control. [Internet] [Doctoral dissertation]. University of Michigan; 2016. [cited 2021 Mar 08]. 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


University of Michigan

25. Rui, Chunlei. Dynamics and nonlinear attitude control of multibody space systems.

Degree: PhD, Applied Sciences, 1997, University of Michigan

 In this dissertation, we study dynamics and attitude control problems for a multibody system in space. The key feature of this work is the systematic… (more)

Subjects/Keywords: Attitude; Dynamics; Multibody; Nonlinear Control; Space; Spacecraft; Systems

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APA (6th Edition):

Rui, C. (1997). Dynamics and nonlinear attitude control of multibody space systems. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/130814

Chicago Manual of Style (16th Edition):

Rui, Chunlei. “Dynamics and nonlinear attitude control of multibody space systems.” 1997. Doctoral Dissertation, University of Michigan. Accessed March 08, 2021. http://hdl.handle.net/2027.42/130814.

MLA Handbook (7th Edition):

Rui, Chunlei. “Dynamics and nonlinear attitude control of multibody space systems.” 1997. Web. 08 Mar 2021.

Vancouver:

Rui C. Dynamics and nonlinear attitude control of multibody space systems. [Internet] [Doctoral dissertation]. University of Michigan; 1997. [cited 2021 Mar 08]. Available from: http://hdl.handle.net/2027.42/130814.

Council of Science Editors:

Rui C. Dynamics and nonlinear attitude control of multibody space systems. [Doctoral Dissertation]. University of Michigan; 1997. Available from: http://hdl.handle.net/2027.42/130814

26. Guillemot, Valérie. Le référentiel, organisateur du dit « coaching » ? : Etude socio clinique de ses usages : Is the reference table an organizer or what is called coaching ? : A socio-clinical study of its uses.

Degree: Docteur es, Sciences de l'éducation, 2014, Aix Marseille Université

La diversité de l'offre disponible sous le mot « coaching » est source de confusion pour les clients, les commanditaires et les coachs eux-mêmes. Dans… (more)

Subjects/Keywords: Coaching; Accompagnement; Référentiel; Evaluation; Formation; Activité; Dynamiques identitaires; Coaching; Accompanying attitude; Reference table; Education; Assessment; Activity; Dynamics of identity

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APA (6th Edition):

Guillemot, V. (2014). Le référentiel, organisateur du dit « coaching » ? : Etude socio clinique de ses usages : Is the reference table an organizer or what is called coaching ? : A socio-clinical study of its uses. (Doctoral Dissertation). Aix Marseille Université. Retrieved from http://www.theses.fr/2014AIXM3021

Chicago Manual of Style (16th Edition):

Guillemot, Valérie. “Le référentiel, organisateur du dit « coaching » ? : Etude socio clinique de ses usages : Is the reference table an organizer or what is called coaching ? : A socio-clinical study of its uses.” 2014. Doctoral Dissertation, Aix Marseille Université. Accessed March 08, 2021. http://www.theses.fr/2014AIXM3021.

MLA Handbook (7th Edition):

Guillemot, Valérie. “Le référentiel, organisateur du dit « coaching » ? : Etude socio clinique de ses usages : Is the reference table an organizer or what is called coaching ? : A socio-clinical study of its uses.” 2014. Web. 08 Mar 2021.

Vancouver:

Guillemot V. Le référentiel, organisateur du dit « coaching » ? : Etude socio clinique de ses usages : Is the reference table an organizer or what is called coaching ? : A socio-clinical study of its uses. [Internet] [Doctoral dissertation]. Aix Marseille Université 2014. [cited 2021 Mar 08]. Available from: http://www.theses.fr/2014AIXM3021.

Council of Science Editors:

Guillemot V. Le référentiel, organisateur du dit « coaching » ? : Etude socio clinique de ses usages : Is the reference table an organizer or what is called coaching ? : A socio-clinical study of its uses. [Doctoral Dissertation]. Aix Marseille Université 2014. Available from: http://www.theses.fr/2014AIXM3021


University of Toronto

27. Markin, Shael. Multiple Simultaneous Specification Attitude Control of a Mini Flying-wing Unmanned Aerial Vehicle.

Degree: 2010, University of Toronto

The Multiple Simultaneous Specification controller design method is an elegant means of designing a single controller to satisfy multiple convex closed loop performance specifications. In… (more)

Subjects/Keywords: Unmanned Aerial Vehicle; Flying-Wing; Convex; Multiple Simultaneous Specification; Performance; Simulation; Hardware-in-the-loop; Dynamics; Attitude; Aircraft; Autopilot; 0548; 0538

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APA (6th Edition):

Markin, S. (2010). Multiple Simultaneous Specification Attitude Control of a Mini Flying-wing Unmanned Aerial Vehicle. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/25849

Chicago Manual of Style (16th Edition):

Markin, Shael. “Multiple Simultaneous Specification Attitude Control of a Mini Flying-wing Unmanned Aerial Vehicle.” 2010. Masters Thesis, University of Toronto. Accessed March 08, 2021. http://hdl.handle.net/1807/25849.

MLA Handbook (7th Edition):

Markin, Shael. “Multiple Simultaneous Specification Attitude Control of a Mini Flying-wing Unmanned Aerial Vehicle.” 2010. Web. 08 Mar 2021.

Vancouver:

Markin S. Multiple Simultaneous Specification Attitude Control of a Mini Flying-wing Unmanned Aerial Vehicle. [Internet] [Masters thesis]. University of Toronto; 2010. [cited 2021 Mar 08]. Available from: http://hdl.handle.net/1807/25849.

Council of Science Editors:

Markin S. Multiple Simultaneous Specification Attitude Control of a Mini Flying-wing Unmanned Aerial Vehicle. [Masters Thesis]. University of Toronto; 2010. Available from: http://hdl.handle.net/1807/25849


University of Toronto

28. 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

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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 08, 2021. http://hdl.handle.net/1807/73473.

MLA Handbook (7th Edition):

Vatankhahghadim, Behrad. “Hybrid Magnetic Attitude Control of Spacecraft: Optimality, Passivity, and Stability.” 2016. Web. 08 Mar 2021.

Vancouver:

Vatankhahghadim B. Hybrid Magnetic Attitude Control of Spacecraft: Optimality, Passivity, and Stability. [Internet] [Masters thesis]. University of Toronto; 2016. [cited 2021 Mar 08]. 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 Colorado

29. Diaz Ramos, Manuel Francisco. Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control.

Degree: MS, 2017, University of Colorado

 Orientation constrained attitude control is a requirement in most spacecraft missions. A novel technique for attitude control of a spacecraft subjected to an arbitrary number… (more)

Subjects/Keywords: attitude control; constrained control; lyapunov theory; modified rodrigues parameters; bounded-torque control; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Diaz Ramos, M. F. (2017). Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/233

Chicago Manual of Style (16th Edition):

Diaz Ramos, Manuel Francisco. “Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control.” 2017. Masters Thesis, University of Colorado. Accessed March 08, 2021. https://scholar.colorado.edu/asen_gradetds/233.

MLA Handbook (7th Edition):

Diaz Ramos, Manuel Francisco. “Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control.” 2017. Web. 08 Mar 2021.

Vancouver:

Diaz Ramos MF. Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2021 Mar 08]. Available from: https://scholar.colorado.edu/asen_gradetds/233.

Council of Science Editors:

Diaz Ramos MF. Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/233


Cranfield University

30. Guo, Wei. Gain scheduling for a passenger aircraft control system to satisfy handling qualities.

Degree: MSc by Research, 2010, Cranfield University

 This thesis considers the problem of designing gain scheduled flight control system (FCS) for large transport aircraft that satisfy handling qualities criteria. The goal is… (more)

Subjects/Keywords: Gain Scheduling; Flight Control System; Handling Qualities; Rate Command-Attitude Hold; Passenger Aircraft; Flight Dynamics; Boeing 747

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APA (6th Edition):

Guo, W. (2010). Gain scheduling for a passenger aircraft control system to satisfy handling qualities. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/6701

Chicago Manual of Style (16th Edition):

Guo, Wei. “Gain scheduling for a passenger aircraft control system to satisfy handling qualities.” 2010. Masters Thesis, Cranfield University. Accessed March 08, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/6701.

MLA Handbook (7th Edition):

Guo, Wei. “Gain scheduling for a passenger aircraft control system to satisfy handling qualities.” 2010. Web. 08 Mar 2021.

Vancouver:

Guo W. Gain scheduling for a passenger aircraft control system to satisfy handling qualities. [Internet] [Masters thesis]. Cranfield University; 2010. [cited 2021 Mar 08]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/6701.

Council of Science Editors:

Guo W. Gain scheduling for a passenger aircraft control system to satisfy handling qualities. [Masters Thesis]. Cranfield University; 2010. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/6701

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