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You searched for subject:(Single axis attitude control). Showing records 1 – 30 of 52514 total matches.

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1. 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 · 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


Virginia Tech

2. 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

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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


NSYSU

3. Wang, Hao-yu. An Image-Based Self-Balance System to Suppress Water Spill for a Moving Cup.

Degree: Master, Mechanical and Electro-Mechanical Engineering, 2017, NSYSU

 When a human walks with a cup of coffee, he usually tries to suppress the sloshing in the cup with his wrist by monitoring the… (more)

Subjects/Keywords: Single-axis robotic arm; Machine vision; Prediction of sloshing liquid surface; Fuzzy control; Sloshing dynamic model

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APA (6th Edition):

Wang, H. (2017). An Image-Based Self-Balance System to Suppress Water Spill for a Moving Cup. (Thesis). NSYSU. Retrieved from http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0713117-222839

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

Chicago Manual of Style (16th Edition):

Wang, Hao-yu. “An Image-Based Self-Balance System to Suppress Water Spill for a Moving Cup.” 2017. Thesis, NSYSU. Accessed March 21, 2019. http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0713117-222839.

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

MLA Handbook (7th Edition):

Wang, Hao-yu. “An Image-Based Self-Balance System to Suppress Water Spill for a Moving Cup.” 2017. Web. 21 Mar 2019.

Vancouver:

Wang H. An Image-Based Self-Balance System to Suppress Water Spill for a Moving Cup. [Internet] [Thesis]. NSYSU; 2017. [cited 2019 Mar 21]. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0713117-222839.

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

Council of Science Editors:

Wang H. An Image-Based Self-Balance System to Suppress Water Spill for a Moving Cup. [Thesis]. NSYSU; 2017. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0713117-222839

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


North-West University

4. Gresse, Cindy. The role of a leisure-based programme on the relationship and attitudes of divorced single-parent families / C. Gresse.

Degree: 2013, North-West University

 Divorce can be seen as one of the major causes of single-parent households (Janzen & Harris, 1997:134). Among the obvious difficulties families face as a… (more)

Subjects/Keywords: Leisure; relationship; attitude; divorce; single parenting; children

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APA (6th Edition):

Gresse, C. (2013). The role of a leisure-based programme on the relationship and attitudes of divorced single-parent families / C. Gresse. (Thesis). North-West University. Retrieved from http://hdl.handle.net/10394/9661

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):

Gresse, Cindy. “The role of a leisure-based programme on the relationship and attitudes of divorced single-parent families / C. Gresse. ” 2013. Thesis, North-West University. Accessed March 21, 2019. http://hdl.handle.net/10394/9661.

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

MLA Handbook (7th Edition):

Gresse, Cindy. “The role of a leisure-based programme on the relationship and attitudes of divorced single-parent families / C. Gresse. ” 2013. Web. 21 Mar 2019.

Vancouver:

Gresse C. The role of a leisure-based programme on the relationship and attitudes of divorced single-parent families / C. Gresse. [Internet] [Thesis]. North-West University; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/10394/9661.

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

Council of Science Editors:

Gresse C. The role of a leisure-based programme on the relationship and attitudes of divorced single-parent families / C. Gresse. [Thesis]. North-West University; 2013. Available from: http://hdl.handle.net/10394/9661

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


Lehigh University

5. 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

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APA (6th Edition):

Zhu, S. (2016). Analysis of Spacecraft Attitude Control. (Thesis). Lehigh University. Retrieved from https://preserve.lehigh.edu/etd/2915

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

Chicago Manual of Style (16th Edition):

Zhu, Shiqiao. “Analysis of Spacecraft Attitude Control.” 2016. Thesis, Lehigh University. Accessed 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


University of Toronto

6. Philip, Adam Neil. Attitude Sensing, Actuation, and Control of the BRITE and CanX-4&5 Satellites.

Degree: 2008, University of Toronto

An attitude control system for the BRITE and CanX-4&5 nanosatellites is developed. BRITE and CanX-4&5 are research satellites based on the Space Flight Laboratory’s Generic… (more)

Subjects/Keywords: Attitude; Control; Satellite; Sensing; 0538

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APA (6th Edition):

Philip, A. N. (2008). Attitude Sensing, Actuation, and Control of the BRITE and CanX-4&5 Satellites. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/17213

Chicago Manual of Style (16th Edition):

Philip, Adam Neil. “Attitude Sensing, Actuation, and Control of the BRITE and CanX-4&5 Satellites.” 2008. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/17213.

MLA Handbook (7th Edition):

Philip, Adam Neil. “Attitude Sensing, Actuation, and Control of the BRITE and CanX-4&5 Satellites.” 2008. Web. 21 Mar 2019.

Vancouver:

Philip AN. Attitude Sensing, Actuation, and Control of the BRITE and CanX-4&5 Satellites. [Internet] [Masters thesis]. University of Toronto; 2008. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/17213.

Council of Science Editors:

Philip AN. Attitude Sensing, Actuation, and Control of the BRITE and CanX-4&5 Satellites. [Masters Thesis]. University of Toronto; 2008. Available from: http://hdl.handle.net/1807/17213


University of Toronto

7. Seth, Nitin. Hybrid Magnetic Attitude Controller for Low Earth Orbit Satellites using the Time-varying Linear Quadratic Regulator.

Degree: 2009, University of Toronto

The following is a study of an attitude control system (ACS) for a low earth orbit nanosatellite. Control actuation is applied using three reaction wheels… (more)

Subjects/Keywords: Attitude Control; LQR; 0538

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APA (6th Edition):

Seth, N. (2009). Hybrid Magnetic Attitude Controller for Low Earth Orbit Satellites using the Time-varying Linear Quadratic Regulator. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/17711

Chicago Manual of Style (16th Edition):

Seth, Nitin. “Hybrid Magnetic Attitude Controller for Low Earth Orbit Satellites using the Time-varying Linear Quadratic Regulator.” 2009. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/17711.

MLA Handbook (7th Edition):

Seth, Nitin. “Hybrid Magnetic Attitude Controller for Low Earth Orbit Satellites using the Time-varying Linear Quadratic Regulator.” 2009. Web. 21 Mar 2019.

Vancouver:

Seth N. Hybrid Magnetic Attitude Controller for Low Earth Orbit Satellites using the Time-varying Linear Quadratic Regulator. [Internet] [Masters thesis]. University of Toronto; 2009. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/17711.

Council of Science Editors:

Seth N. Hybrid Magnetic Attitude Controller for Low Earth Orbit Satellites using the Time-varying Linear Quadratic Regulator. [Masters Thesis]. University of Toronto; 2009. Available from: http://hdl.handle.net/1807/17711


University of Toronto

8. Dutia, Jiten. Magnetic Attitude Control of Microsatellites In Geocentric Orbits.

Degree: 2013, University of Toronto

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

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

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APA (6th Edition):

Dutia, J. (2013). Magnetic Attitude Control of Microsatellites In Geocentric Orbits. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/35117

Chicago Manual of Style (16th Edition):

Dutia, Jiten. “Magnetic Attitude Control of Microsatellites In Geocentric Orbits.” 2013. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/35117.

MLA Handbook (7th Edition):

Dutia, Jiten. “Magnetic Attitude Control of Microsatellites In Geocentric Orbits.” 2013. Web. 21 Mar 2019.

Vancouver:

Dutia J. Magnetic Attitude Control of Microsatellites In Geocentric Orbits. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/35117.

Council of Science Editors:

Dutia J. Magnetic Attitude Control of Microsatellites In Geocentric Orbits. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/35117


University of Toronto

9. Ibrahim, Najmus. Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.

Degree: 2013, University of Toronto

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Ibrahim, Najmus. “Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.” 2013. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/42965.

MLA Handbook (7th Edition):

Ibrahim, Najmus. “Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking.” 2013. Web. 21 Mar 2019.

Vancouver:

Ibrahim N. Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/42965.

Council of Science Editors:

Ibrahim N. Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/42965


Delft University of Technology

10. Barendswaard, S. Investigating the Difference Between Single and Dual Axis Manual Control:.

Degree: 2016, Delft University of Technology

 Aircraft manual control tasks require simultane- ous control of multiple degrees-of-freedom. Unfortunately, most multi-axis human-operator modeling is limited to the modeling of multiple fully-independent axis.… (more)

Subjects/Keywords: manual control cybernetics; system identification; Fourier Coefficient Method; multi-axis control

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APA (6th Edition):

Barendswaard, S. (2016). Investigating the Difference Between Single and Dual Axis Manual Control:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ca862c9c-250d-42be-8fb1-b8bb8e637d1c

Chicago Manual of Style (16th Edition):

Barendswaard, S. “Investigating the Difference Between Single and Dual Axis Manual Control:.” 2016. Masters Thesis, Delft University of Technology. Accessed March 21, 2019. http://resolver.tudelft.nl/uuid:ca862c9c-250d-42be-8fb1-b8bb8e637d1c.

MLA Handbook (7th Edition):

Barendswaard, S. “Investigating the Difference Between Single and Dual Axis Manual Control:.” 2016. Web. 21 Mar 2019.

Vancouver:

Barendswaard S. Investigating the Difference Between Single and Dual Axis Manual Control:. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2019 Mar 21]. Available from: http://resolver.tudelft.nl/uuid:ca862c9c-250d-42be-8fb1-b8bb8e637d1c.

Council of Science Editors:

Barendswaard S. Investigating the Difference Between Single and Dual Axis Manual Control:. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:ca862c9c-250d-42be-8fb1-b8bb8e637d1c


Wright State University

11. Jenkins, Joseph C. THE EFFECT OF CONFIGURAL DISPLAYS ON PILOT SITUATION AWARENESS IN HELMET-MOUNTED DISPLAYS.

Degree: PhD, Engineering PhD, 2007, Wright State University

 Jenkins, Joseph Christopher, Ph.D., Engineering, Wright State University, 2007. The Effect of Configural Displays on Pilot Situation Awareness in Helmet-Mounted Displays. The current research utilized… (more)

Subjects/Keywords: Configural displays; Situation Awareness; Emergent features; Helmet-Mounted Displays; Attitude Awareness; Off-axis Symbology

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APA (6th Edition):

Jenkins, J. C. (2007). THE EFFECT OF CONFIGURAL DISPLAYS ON PILOT SITUATION AWARENESS IN HELMET-MOUNTED DISPLAYS. (Doctoral Dissertation). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1187882021

Chicago Manual of Style (16th Edition):

Jenkins, Joseph C. “THE EFFECT OF CONFIGURAL DISPLAYS ON PILOT SITUATION AWARENESS IN HELMET-MOUNTED DISPLAYS.” 2007. Doctoral Dissertation, Wright State University. Accessed March 21, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=wright1187882021.

MLA Handbook (7th Edition):

Jenkins, Joseph C. “THE EFFECT OF CONFIGURAL DISPLAYS ON PILOT SITUATION AWARENESS IN HELMET-MOUNTED DISPLAYS.” 2007. Web. 21 Mar 2019.

Vancouver:

Jenkins JC. THE EFFECT OF CONFIGURAL DISPLAYS ON PILOT SITUATION AWARENESS IN HELMET-MOUNTED DISPLAYS. [Internet] [Doctoral dissertation]. Wright State University; 2007. [cited 2019 Mar 21]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1187882021.

Council of Science Editors:

Jenkins JC. THE EFFECT OF CONFIGURAL DISPLAYS ON PILOT SITUATION AWARENESS IN HELMET-MOUNTED DISPLAYS. [Doctoral Dissertation]. Wright State University; 2007. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1187882021


University of Toronto

12. 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

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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


University of Ontario Institute of Technology

13. Fatima, Mariam. Development of an actuation system for a specialized fixture: providing two degrees of freedom for single point incremental forming.

Degree: 2013, University of Ontario Institute of Technology

 In this thesis, an actuation system is developed for a Two-Axis Gyroscopic (TAG) adapter. This adapter is a fixture with two auxiliary axes which is… (more)

Subjects/Keywords: Single point incremental forming (SPIF); Toolpath; Five-axis mill; Inverse kinematics; Frame of reference

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APA (6th Edition):

Fatima, M. (2013). Development of an actuation system for a specialized fixture: providing two degrees of freedom for single point incremental forming. (Thesis). University of Ontario Institute of Technology. Retrieved from http://hdl.handle.net/10155/311

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):

Fatima, Mariam. “Development of an actuation system for a specialized fixture: providing two degrees of freedom for single point incremental forming.” 2013. Thesis, University of Ontario Institute of Technology. Accessed March 21, 2019. http://hdl.handle.net/10155/311.

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

MLA Handbook (7th Edition):

Fatima, Mariam. “Development of an actuation system for a specialized fixture: providing two degrees of freedom for single point incremental forming.” 2013. Web. 21 Mar 2019.

Vancouver:

Fatima M. Development of an actuation system for a specialized fixture: providing two degrees of freedom for single point incremental forming. [Internet] [Thesis]. University of Ontario Institute of Technology; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/10155/311.

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

Council of Science Editors:

Fatima M. Development of an actuation system for a specialized fixture: providing two degrees of freedom for single point incremental forming. [Thesis]. University of Ontario Institute of Technology; 2013. Available from: http://hdl.handle.net/10155/311

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


University of Arizona

14. Ayala Pelaez, Silvana. Bifacial Solar Panels System Design, Modeling, and Performance .

Degree: 2019, University of Arizona

 Bifacial photovoltaic (PV) cell technology is currently poised to change solar modules and systems. They provide higher energy yield from its ability to capture both… (more)

Subjects/Keywords: bifaciality; bifacial PV module; irradiance; performance modeling; ray tracing; single-axis tracking

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APA (6th Edition):

Ayala Pelaez, S. (2019). Bifacial Solar Panels System Design, Modeling, and Performance . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/631283

Chicago Manual of Style (16th Edition):

Ayala Pelaez, Silvana. “Bifacial Solar Panels System Design, Modeling, and Performance .” 2019. Doctoral Dissertation, University of Arizona. Accessed March 21, 2019. http://hdl.handle.net/10150/631283.

MLA Handbook (7th Edition):

Ayala Pelaez, Silvana. “Bifacial Solar Panels System Design, Modeling, and Performance .” 2019. Web. 21 Mar 2019.

Vancouver:

Ayala Pelaez S. Bifacial Solar Panels System Design, Modeling, and Performance . [Internet] [Doctoral dissertation]. University of Arizona; 2019. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/10150/631283.

Council of Science Editors:

Ayala Pelaez S. Bifacial Solar Panels System Design, Modeling, and Performance . [Doctoral Dissertation]. University of Arizona; 2019. Available from: http://hdl.handle.net/10150/631283


Virginia Tech

15. 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

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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 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


The Ohio State University

16. Gobbalipur Ranganath, Jayanth. Multi-axis probing system for nano-metrology.

Degree: PhD, Mechanical Engineering, 2009, The Ohio State University

  Atomic force microscopy has been the primary workhorse for imaging and manipulating samples with sub-nanometer resolution and pico-Newton scale force resolution. It has found… (more)

Subjects/Keywords: Mechanical Engineering; nano-metrology; multi-axis compliant manipulator; magnetic actuation; real-time tip orientation control; two-axis scanning; two-axis tip-sample interaction control

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

APA (6th Edition):

Gobbalipur Ranganath, J. (2009). Multi-axis probing system for nano-metrology. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1229908979

Chicago Manual of Style (16th Edition):

Gobbalipur Ranganath, Jayanth. “Multi-axis probing system for nano-metrology.” 2009. Doctoral Dissertation, The Ohio State University. Accessed March 21, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1229908979.

MLA Handbook (7th Edition):

Gobbalipur Ranganath, Jayanth. “Multi-axis probing system for nano-metrology.” 2009. Web. 21 Mar 2019.

Vancouver:

Gobbalipur Ranganath J. Multi-axis probing system for nano-metrology. [Internet] [Doctoral dissertation]. The Ohio State University; 2009. [cited 2019 Mar 21]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1229908979.

Council of Science Editors:

Gobbalipur Ranganath J. Multi-axis probing system for nano-metrology. [Doctoral Dissertation]. The Ohio State University; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1229908979


University of Toronto

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

Degree: 2011, University of Toronto

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

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

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Johnston-Lemke, Bryan. “High Performance Attitude Determination and Control for Nanosatellite Missions.” 2011. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/30644.

MLA Handbook (7th Edition):

Johnston-Lemke, Bryan. “High Performance Attitude Determination and Control for Nanosatellite Missions.” 2011. Web. 21 Mar 2019.

Vancouver:

Johnston-Lemke B. High Performance Attitude Determination and Control for Nanosatellite Missions. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/30644.

Council of Science Editors:

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


University of Toronto

18. 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 21, 2019. 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. 21 Mar 2019.

Vancouver:

Findlay E. Investigation of Active Vibration Suppression of a Flexible Satellite using Magnetic Attitude Control. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/30593.

Council of Science Editors:

Findlay E. Investigation of Active Vibration Suppression of a Flexible Satellite using Magnetic Attitude Control. [Masters Thesis]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/30593


University of Toronto

19. Shen, Young-Young. Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites.

Degree: 2015, University of Toronto

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

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

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APA (6th Edition):

Shen, Y. (2015). Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/70675

Chicago Manual of Style (16th Edition):

Shen, Young-Young. “Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites.” 2015. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/70675.

MLA Handbook (7th Edition):

Shen, Young-Young. “Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites.” 2015. Web. 21 Mar 2019.

Vancouver:

Shen Y. Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites. [Internet] [Masters thesis]. University of Toronto; 2015. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/70675.

Council of Science Editors:

Shen Y. Attitude Determination and Control Hardware Acceptance Testing for Next Generation Microsatellites. [Masters Thesis]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/70675


Montana Tech

20. Van Ackeren, Gerald A. Leisure attitudes of single adults.

Degree: MS, 1977, Montana Tech

Subjects/Keywords: Leisure.; Attitude (Psychology); Single people.

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APA (6th Edition):

Van Ackeren, G. A. (1977). Leisure attitudes of single adults. (Masters Thesis). Montana Tech. Retrieved from https://scholarworks.umt.edu/etd/5445

Chicago Manual of Style (16th Edition):

Van Ackeren, Gerald A. “Leisure attitudes of single adults.” 1977. Masters Thesis, Montana Tech. Accessed March 21, 2019. https://scholarworks.umt.edu/etd/5445.

MLA Handbook (7th Edition):

Van Ackeren, Gerald A. “Leisure attitudes of single adults.” 1977. Web. 21 Mar 2019.

Vancouver:

Van Ackeren GA. Leisure attitudes of single adults. [Internet] [Masters thesis]. Montana Tech; 1977. [cited 2019 Mar 21]. Available from: https://scholarworks.umt.edu/etd/5445.

Council of Science Editors:

Van Ackeren GA. Leisure attitudes of single adults. [Masters Thesis]. Montana Tech; 1977. Available from: https://scholarworks.umt.edu/etd/5445

21. 赤井, 孝行; アカイ, タカユキ. 5軸制御マシニングセンターの運動精度と加工精度向上に関する研究 : 5ジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニカンスル ケンキュウ; ゴジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニ カンスル ケンキュウ; Study on improvement of motion accuracy and machining accuracy of 5-axis machining center.

Degree: 博士(工学), 2015, Doshisha University / 同志社大学

5軸制御マシニングセンターの運動精度の向上に向けた新たなキャリブレーション手法の開発に取り組んだ.また、直進および旋回軸の各種の運動誤差要因を診断する手法を構築した.さらにサーボ系の位置フィードバックで,サーボ系に起因する運動誤差の診断法も提案した.旋回軸にDDモータ方式を採用することで機械全体のサーボ特性を大きく改善できることも解明した.最後に,複雑形状の実加工により開発機で高い加工精度を確認することができた.

A new calibration method to improve the motion accuracy of a 5-axis control machining center has been developed. A method to diagnose various causes… (more)

Subjects/Keywords: キーワード,keyword; 5軸制御,5 axis control

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

APA (6th Edition):

赤井, 孝行; アカイ, . (2015). 5軸制御マシニングセンターの運動精度と加工精度向上に関する研究 : 5ジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニカンスル ケンキュウ; ゴジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニ カンスル ケンキュウ; Study on improvement of motion accuracy and machining accuracy of 5-axis machining center. (Thesis). Doshisha University / 同志社大学. Retrieved from https://doors.doshisha.ac.jp/duar/repository/ir/17596/?lang=0 ; http://dx.doi.org/10.14988/di.2017.0000016239

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):

赤井, 孝行; アカイ, タカユキ. “5軸制御マシニングセンターの運動精度と加工精度向上に関する研究 : 5ジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニカンスル ケンキュウ; ゴジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニ カンスル ケンキュウ; Study on improvement of motion accuracy and machining accuracy of 5-axis machining center.” 2015. Thesis, Doshisha University / 同志社大学. Accessed March 21, 2019. https://doors.doshisha.ac.jp/duar/repository/ir/17596/?lang=0 ; http://dx.doi.org/10.14988/di.2017.0000016239.

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

MLA Handbook (7th Edition):

赤井, 孝行; アカイ, タカユキ. “5軸制御マシニングセンターの運動精度と加工精度向上に関する研究 : 5ジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニカンスル ケンキュウ; ゴジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニ カンスル ケンキュウ; Study on improvement of motion accuracy and machining accuracy of 5-axis machining center.” 2015. Web. 21 Mar 2019.

Vancouver:

赤井, 孝行; アカイ . 5軸制御マシニングセンターの運動精度と加工精度向上に関する研究 : 5ジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニカンスル ケンキュウ; ゴジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニ カンスル ケンキュウ; Study on improvement of motion accuracy and machining accuracy of 5-axis machining center. [Internet] [Thesis]. Doshisha University / 同志社大学; 2015. [cited 2019 Mar 21]. Available from: https://doors.doshisha.ac.jp/duar/repository/ir/17596/?lang=0 ; http://dx.doi.org/10.14988/di.2017.0000016239.

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

Council of Science Editors:

赤井, 孝行; アカイ . 5軸制御マシニングセンターの運動精度と加工精度向上に関する研究 : 5ジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニカンスル ケンキュウ; ゴジク セイギョ マシニング センター ノ ウンドウ セイド ト カコウ セイド コウジョウ ニ カンスル ケンキュウ; Study on improvement of motion accuracy and machining accuracy of 5-axis machining center. [Thesis]. Doshisha University / 同志社大学; 2015. Available from: https://doors.doshisha.ac.jp/duar/repository/ir/17596/?lang=0 ; http://dx.doi.org/10.14988/di.2017.0000016239

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


University of Waterloo

22. Skensved, Erik. Air Jets for Lift Control in Low Reynolds Number Flow.

Degree: 2010, University of Waterloo

 The environmental and monetary cost of energy has renewed interest in horizontal-axis wind turbines (HAWT). One problem with HAWT design is turbulent winds, which cause… (more)

Subjects/Keywords: horizontal-axis wind turbine; low Reynolds number; jet flap; aerodynamic control

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

APA (6th Edition):

Skensved, E. (2010). Air Jets for Lift Control in Low Reynolds Number Flow. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/5116

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):

Skensved, Erik. “Air Jets for Lift Control in Low Reynolds Number Flow.” 2010. Thesis, University of Waterloo. Accessed March 21, 2019. http://hdl.handle.net/10012/5116.

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

MLA Handbook (7th Edition):

Skensved, Erik. “Air Jets for Lift Control in Low Reynolds Number Flow.” 2010. Web. 21 Mar 2019.

Vancouver:

Skensved E. Air Jets for Lift Control in Low Reynolds Number Flow. [Internet] [Thesis]. University of Waterloo; 2010. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/10012/5116.

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

Council of Science Editors:

Skensved E. Air Jets for Lift Control in Low Reynolds Number Flow. [Thesis]. University of Waterloo; 2010. Available from: http://hdl.handle.net/10012/5116

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


Brunel University

23. Jeyalingam, Jonne. Towards the noise reduction of synthetic jet actuators using lobed orifices.

Degree: PhD, 2018, Brunel University

 With increasing strain on the civil aviation industry to meet strict targets to reduce the adverse effects aviation has on the environment by 2050, significant… (more)

Subjects/Keywords: Fluid mechanics; Active flow control; Aeroacoustics; Axis-switching

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APA (6th Edition):

Jeyalingam, J. (2018). Towards the noise reduction of synthetic jet actuators using lobed orifices. (Doctoral Dissertation). Brunel University. Retrieved from http://bura.brunel.ac.uk/handle/2438/17118 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.765048

Chicago Manual of Style (16th Edition):

Jeyalingam, Jonne. “Towards the noise reduction of synthetic jet actuators using lobed orifices.” 2018. Doctoral Dissertation, Brunel University. Accessed March 21, 2019. http://bura.brunel.ac.uk/handle/2438/17118 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.765048.

MLA Handbook (7th Edition):

Jeyalingam, Jonne. “Towards the noise reduction of synthetic jet actuators using lobed orifices.” 2018. Web. 21 Mar 2019.

Vancouver:

Jeyalingam J. Towards the noise reduction of synthetic jet actuators using lobed orifices. [Internet] [Doctoral dissertation]. Brunel University; 2018. [cited 2019 Mar 21]. Available from: http://bura.brunel.ac.uk/handle/2438/17118 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.765048.

Council of Science Editors:

Jeyalingam J. Towards the noise reduction of synthetic jet actuators using lobed orifices. [Doctoral Dissertation]. Brunel University; 2018. Available from: http://bura.brunel.ac.uk/handle/2438/17118 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.765048


Brigham Young University

24. Argyle, Matthew Elliott. Modeling and Control of a Tailsitter with a Ducted Fan.

Degree: PhD, 2016, Brigham Young University

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

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

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APA (6th Edition):

Argyle, M. E. (2016). Modeling and Control of a Tailsitter with a Ducted Fan. (Doctoral Dissertation). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6928&context=etd

Chicago Manual of Style (16th Edition):

Argyle, Matthew Elliott. “Modeling and Control of a Tailsitter with a Ducted Fan.” 2016. Doctoral Dissertation, Brigham Young University. Accessed March 21, 2019. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6928&context=etd.

MLA Handbook (7th Edition):

Argyle, Matthew Elliott. “Modeling and Control of a Tailsitter with a Ducted Fan.” 2016. Web. 21 Mar 2019.

Vancouver:

Argyle ME. Modeling and Control of a Tailsitter with a Ducted Fan. [Internet] [Doctoral dissertation]. Brigham Young University; 2016. [cited 2019 Mar 21]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6928&context=etd.

Council of Science Editors:

Argyle ME. Modeling and Control of a Tailsitter with a Ducted Fan. [Doctoral Dissertation]. Brigham Young University; 2016. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6928&context=etd


Brno University of Technology

25. Chaloupka, Roman. Návrh řízení osy s lineárním motorem .

Degree: 2015, Brno University of Technology

 Tato práce se zabývá konstrukcí, zapojením a řízením osy s lineárním motorem. Začátek práce je zaměřen na princip fungování a vlastnosti lineárních motorů. V následující… (more)

Subjects/Keywords: Lineární motor; lineární osa; PLC; řízení osy; TwinCAT; Linear motor; linear axis; PLC; axis control; TwinCAT

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APA (6th Edition):

Chaloupka, R. (2015). Návrh řízení osy s lineárním motorem . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/40112

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):

Chaloupka, Roman. “Návrh řízení osy s lineárním motorem .” 2015. Thesis, Brno University of Technology. Accessed March 21, 2019. http://hdl.handle.net/11012/40112.

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

MLA Handbook (7th Edition):

Chaloupka, Roman. “Návrh řízení osy s lineárním motorem .” 2015. Web. 21 Mar 2019.

Vancouver:

Chaloupka R. Návrh řízení osy s lineárním motorem . [Internet] [Thesis]. Brno University of Technology; 2015. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/11012/40112.

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

Council of Science Editors:

Chaloupka R. Návrh řízení osy s lineárním motorem . [Thesis]. Brno University of Technology; 2015. Available from: http://hdl.handle.net/11012/40112

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


Wright State University

26. Gugale, Gaurav Subhash. Development of Analytical Equations for Optimum Tilt of Two-Axis and Single-Axis Rotating Solar Panels for Clear-Atmosphere Condition.

Degree: MSin Renewable and Clean Energy Engineering MSRCE, Renewable and Clean Energy, 2016, Wright State University

 Solar Energy is a renewable energy source which is used widely in recent times. Photovoltaic panels collect the sun’s energy and convert it to electricity.… (more)

Subjects/Keywords: Alternative Energy; Energy; Engineering; Mechanical Engineering; Solar Energy; Optimum tilt angle; Optimum tilt angle equations; Clear atmosphere model; single axis tracking solar panel; two-axis tracking solar panel

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

APA (6th Edition):

Gugale, G. S. (2016). Development of Analytical Equations for Optimum Tilt of Two-Axis and Single-Axis Rotating Solar Panels for Clear-Atmosphere Condition. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright148459939571045

Chicago Manual of Style (16th Edition):

Gugale, Gaurav Subhash. “Development of Analytical Equations for Optimum Tilt of Two-Axis and Single-Axis Rotating Solar Panels for Clear-Atmosphere Condition.” 2016. Masters Thesis, Wright State University. Accessed March 21, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=wright148459939571045.

MLA Handbook (7th Edition):

Gugale, Gaurav Subhash. “Development of Analytical Equations for Optimum Tilt of Two-Axis and Single-Axis Rotating Solar Panels for Clear-Atmosphere Condition.” 2016. Web. 21 Mar 2019.

Vancouver:

Gugale GS. Development of Analytical Equations for Optimum Tilt of Two-Axis and Single-Axis Rotating Solar Panels for Clear-Atmosphere Condition. [Internet] [Masters thesis]. Wright State University; 2016. [cited 2019 Mar 21]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright148459939571045.

Council of Science Editors:

Gugale GS. Development of Analytical Equations for Optimum Tilt of Two-Axis and Single-Axis Rotating Solar Panels for Clear-Atmosphere Condition. [Masters Thesis]. Wright State University; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright148459939571045


University of California – Berkeley

27. Wang, Yizhou. Attitude Control and Estimation.

Degree: Mechanical Engineering, 2015, University of California – Berkeley

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

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

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

APA (6th Edition):

Wang, Y. (2015). Attitude Control and Estimation. (Thesis). University of California – Berkeley. Retrieved from http://www.escholarship.org/uc/item/59b5d7hh

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

Chicago Manual of Style (16th Edition):

Wang, Yizhou. “Attitude Control and Estimation.” 2015. Thesis, University of California – Berkeley. Accessed March 21, 2019. http://www.escholarship.org/uc/item/59b5d7hh.

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

MLA Handbook (7th Edition):

Wang, Yizhou. “Attitude Control and Estimation.” 2015. Web. 21 Mar 2019.

Vancouver:

Wang Y. Attitude Control and Estimation. [Internet] [Thesis]. University of California – Berkeley; 2015. [cited 2019 Mar 21]. Available from: http://www.escholarship.org/uc/item/59b5d7hh.

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

Council of Science Editors:

Wang Y. Attitude Control and Estimation. [Thesis]. University of California – Berkeley; 2015. Available from: http://www.escholarship.org/uc/item/59b5d7hh

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


University of Colorado

28. 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; Aerospace Engineering

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

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 http://scholar.colorado.edu/asen_gradetds/165

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 21, 2019. http://scholar.colorado.edu/asen_gradetds/165.

MLA Handbook (7th Edition):

Diaz Ramos, Manuel Francisco. “Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control.” 2017. Web. 21 Mar 2019.

Vancouver:

Diaz Ramos MF. Kinematic Steering Law for Conically-Constrained Torque-Limited Spacecraft Attitude Control. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2019 Mar 21]. Available from: http://scholar.colorado.edu/asen_gradetds/165.

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: http://scholar.colorado.edu/asen_gradetds/165


University of Toronto

29. Tarantini, Vincent. Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite.

Degree: 2012, University of Toronto

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

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

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Tarantini, Vincent. “Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite.” 2012. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/33557.

MLA Handbook (7th Edition):

Tarantini, Vincent. “Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite.” 2012. Web. 21 Mar 2019.

Vancouver:

Tarantini V. Attitude Dependent De-orbit Lifetime Analysis of an Aerodynamic Drag Sail Demonstration Spacecraft and Detailed Thermal Subsystem Design for a Polar Orbiting Communications Nanosatellite. [Internet] [Masters thesis]. University of Toronto; 2012. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/33557.

Council of Science Editors:

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


Delft University of Technology

30. Habets, J.M.G. Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft:.

Degree: 2015, Delft University of Technology

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

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

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

APA (6th Edition):

Habets, J. M. G. (2015). Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f1bc854a-36f9-4401-a892-2313e4022ea8

Chicago Manual of Style (16th Edition):

Habets, J M G. “Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft:.” 2015. Masters Thesis, Delft University of Technology. Accessed March 21, 2019. http://resolver.tudelft.nl/uuid:f1bc854a-36f9-4401-a892-2313e4022ea8.

MLA Handbook (7th Edition):

Habets, J M G. “Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft:.” 2015. Web. 21 Mar 2019.

Vancouver:

Habets JMG. Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Mar 21]. Available from: http://resolver.tudelft.nl/uuid:f1bc854a-36f9-4401-a892-2313e4022ea8.

Council of Science Editors:

Habets JMG. Evolving Systems Approach to the Attitude Control of a Large-Space-Debris Removal Spacecraft:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:f1bc854a-36f9-4401-a892-2313e4022ea8

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