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You searched for subject:(Attitude Guidance). Showing records 1 – 30 of 46 total matches.

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Virginia Tech

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

VanDyke, Matthew Clark. “Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite.” 2014. Doctoral Dissertation, Virginia Tech. Accessed June 19, 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. 19 Jun 2019.

Vancouver:

VanDyke MC. Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2019 Jun 19]. 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


Brigham Young University

2. 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 June 19, 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. 19 Jun 2019.

Vancouver:

Argyle ME. Modeling and Control of a Tailsitter with a Ducted Fan. [Internet] [Doctoral dissertation]. Brigham Young University; 2016. [cited 2019 Jun 19]. 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


Durban University of Technology

3. Palmer, David Craig. A study to determine the perceptions, attitudes and knowledge of selected South African pharmacists on the chiropractic profession.

Degree: 2008, Durban University of Technology

Thesis (M.Tech.: Chiropractic)-Dept. of Chiropractic, Durban University of Technology, 2008. ix, 106 leaves

Pharmacists are seen as a trustworthy source of advice and information to… (more)

Subjects/Keywords: Chiropractic; Chiropractic – Evaluation; Perception; Chiropractic – Vocational guidance; Attitude (Psychology); Pharmacists – Attitudes

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APA (6th Edition):

Palmer, D. C. (2008). A study to determine the perceptions, attitudes and knowledge of selected South African pharmacists on the chiropractic profession. (Thesis). Durban University of Technology. Retrieved from http://hdl.handle.net/10321/366

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):

Palmer, David Craig. “A study to determine the perceptions, attitudes and knowledge of selected South African pharmacists on the chiropractic profession.” 2008. Thesis, Durban University of Technology. Accessed June 19, 2019. http://hdl.handle.net/10321/366.

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

MLA Handbook (7th Edition):

Palmer, David Craig. “A study to determine the perceptions, attitudes and knowledge of selected South African pharmacists on the chiropractic profession.” 2008. Web. 19 Jun 2019.

Vancouver:

Palmer DC. A study to determine the perceptions, attitudes and knowledge of selected South African pharmacists on the chiropractic profession. [Internet] [Thesis]. Durban University of Technology; 2008. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/10321/366.

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

Council of Science Editors:

Palmer DC. A study to determine the perceptions, attitudes and knowledge of selected South African pharmacists on the chiropractic profession. [Thesis]. Durban University of Technology; 2008. Available from: http://hdl.handle.net/10321/366

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


Michigan State University

4. Youmans, Elmer Grant. An appraisal of the social factors in the work attitudes and interests of a representative sample of twelfth grade Michigan boys.

Degree: PhD, 1953, Michigan State University

Subjects/Keywords: Vocational guidance; Attitude (Psychology); Work

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APA (6th Edition):

Youmans, E. G. (1953). An appraisal of the social factors in the work attitudes and interests of a representative sample of twelfth grade Michigan boys. (Doctoral Dissertation). Michigan State University. Retrieved from http://etd.lib.msu.edu/islandora/object/etd:44211

Chicago Manual of Style (16th Edition):

Youmans, Elmer Grant. “An appraisal of the social factors in the work attitudes and interests of a representative sample of twelfth grade Michigan boys.” 1953. Doctoral Dissertation, Michigan State University. Accessed June 19, 2019. http://etd.lib.msu.edu/islandora/object/etd:44211.

MLA Handbook (7th Edition):

Youmans, Elmer Grant. “An appraisal of the social factors in the work attitudes and interests of a representative sample of twelfth grade Michigan boys.” 1953. Web. 19 Jun 2019.

Vancouver:

Youmans EG. An appraisal of the social factors in the work attitudes and interests of a representative sample of twelfth grade Michigan boys. [Internet] [Doctoral dissertation]. Michigan State University; 1953. [cited 2019 Jun 19]. Available from: http://etd.lib.msu.edu/islandora/object/etd:44211.

Council of Science Editors:

Youmans EG. An appraisal of the social factors in the work attitudes and interests of a representative sample of twelfth grade Michigan boys. [Doctoral Dissertation]. Michigan State University; 1953. Available from: http://etd.lib.msu.edu/islandora/object/etd:44211


University of Texas – Austin

5. -7636-3233. An attitude determination and control system for small satellites.

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

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

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

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APA (6th Edition):

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

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

Chicago Manual of Style (16th Edition):

-7636-3233. “An attitude determination and control system for small satellites.” 2015. Thesis, University of Texas – Austin. Accessed June 19, 2019. http://hdl.handle.net/2152/31715.

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

MLA Handbook (7th Edition):

-7636-3233. “An attitude determination and control system for small satellites.” 2015. Web. 19 Jun 2019.

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

Vancouver:

-7636-3233. An attitude determination and control system for small satellites. [Internet] [Thesis]. University of Texas – Austin; 2015. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/2152/31715.

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

Council of Science Editors:

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

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


University of Colorado

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

APA (6th Edition):

Gerhardt, D. T. (2014). Small Satellite Passive Magnetic Attitude Control. (Doctoral Dissertation). University of Colorado. Retrieved from http://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 June 19, 2019. http://scholar.colorado.edu/asen_gradetds/78.

MLA Handbook (7th Edition):

Gerhardt, David Thomas. “Small Satellite Passive Magnetic Attitude Control.” 2014. Web. 19 Jun 2019.

Vancouver:

Gerhardt DT. Small Satellite Passive Magnetic Attitude Control. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2019 Jun 19]. Available from: http://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: http://scholar.colorado.edu/asen_gradetds/78

7. -8751-8977. A mixed integer convex programming approach to constrained attitude guidance.

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

 This brief report introduces a new algorithm for attitude motion planning, Constrained Attitude Guidance (CAG) problem, in the presence of angular rate constraints and conic… (more)

Subjects/Keywords: Attitude guidance; Mixed-integer programming

…For given initial and final conditions Constraint Attitude Guidance Problem is solved with… …10 15 23 25 26 Chapter 1 Introduction Attitude motion planning, or guidance is an… …all rely on some form of attitude guidance in order to achieve their mission objectives… …1.1 Motivation This work is specifically motivated by the spacecraft attitude guidance… …Attitude Guidance (CAG) methodology that can be used to obtain quaternion trajectories… 

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APA (6th Edition):

-8751-8977. (2015). A mixed integer convex programming approach to constrained attitude guidance. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/34139

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

Chicago Manual of Style (16th Edition):

-8751-8977. “A mixed integer convex programming approach to constrained attitude guidance.” 2015. Thesis, University of Texas – Austin. Accessed June 19, 2019. http://hdl.handle.net/2152/34139.

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

MLA Handbook (7th Edition):

-8751-8977. “A mixed integer convex programming approach to constrained attitude guidance.” 2015. Web. 19 Jun 2019.

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

Vancouver:

-8751-8977. A mixed integer convex programming approach to constrained attitude guidance. [Internet] [Thesis]. University of Texas – Austin; 2015. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/2152/34139.

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

Council of Science Editors:

-8751-8977. A mixed integer convex programming approach to constrained attitude guidance. [Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/34139

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


University of Kentucky

8. 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 http://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 June 19, 2019. http://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. 19 Jun 2019.

Vancouver:

Bezold M. AN ATTITUDE DETERMINATION SYSTEM WITH MEMS GYROSCOPE DRIFT COMPENSATION FOR SMALL SATELLITES. [Internet] [Masters thesis]. University of Kentucky; 2013. [cited 2019 Jun 19]. Available from: http://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: http://uknowledge.uky.edu/ece_etds/29


University of Western Ontario

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 June 19, 2019. 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. 19 Jun 2019.

Vancouver:

Berkane S. Hybrid Attitude Control and Estimation On SO(3). [Internet] [Thesis]. University of Western Ontario; 2017. [cited 2019 Jun 19]. 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


North-West University

10. Phooko, Frances Willemina. Studiebegeleiding aan leerlinge in die seniorprimêreskoolfase met 'n negatiewe studiehouding / Frances W. Phooko .

Degree: 1997, North-West University

 Under favourable conditions, the child in the senior primary phase (from Grade 5 to Grade 7) should lead a happy and carefree life with few… (more)

Subjects/Keywords: Study; Guidance; Negative; Senior primary phase; Attitude; Study attitude; Study method; Study habits

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APA (6th Edition):

Phooko, F. W. (1997). Studiebegeleiding aan leerlinge in die seniorprimêreskoolfase met 'n negatiewe studiehouding / Frances W. Phooko . (Thesis). North-West University. Retrieved from http://hdl.handle.net/10394/8131

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):

Phooko, Frances Willemina. “Studiebegeleiding aan leerlinge in die seniorprimêreskoolfase met 'n negatiewe studiehouding / Frances W. Phooko .” 1997. Thesis, North-West University. Accessed June 19, 2019. http://hdl.handle.net/10394/8131.

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

MLA Handbook (7th Edition):

Phooko, Frances Willemina. “Studiebegeleiding aan leerlinge in die seniorprimêreskoolfase met 'n negatiewe studiehouding / Frances W. Phooko .” 1997. Web. 19 Jun 2019.

Vancouver:

Phooko FW. Studiebegeleiding aan leerlinge in die seniorprimêreskoolfase met 'n negatiewe studiehouding / Frances W. Phooko . [Internet] [Thesis]. North-West University; 1997. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/10394/8131.

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

Council of Science Editors:

Phooko FW. Studiebegeleiding aan leerlinge in die seniorprimêreskoolfase met 'n negatiewe studiehouding / Frances W. Phooko . [Thesis]. North-West University; 1997. Available from: http://hdl.handle.net/10394/8131

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


University of Colorado

11. 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 http://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 June 19, 2019. http://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. 19 Jun 2019.

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 2019 Jun 19]. Available from: http://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: http://scholar.colorado.edu/asen_gradetds/8


University of Colorado

12. Chabot, Joshua A. A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control.

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

  Spacecraft generally require multiple attitude control devices to achieve full attitude actuation because of the limited control authority a single, traditional device can provide.… (more)

Subjects/Keywords: attitude control; magetic dipole; magnetic bearing; reaction sphere; spherical actuator; Navigation, Guidance, Control and Dynamics; Space Vehicles

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

APA (6th Edition):

Chabot, J. A. (2015). A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/100

Chicago Manual of Style (16th Edition):

Chabot, Joshua A. “A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control.” 2015. Masters Thesis, University of Colorado. Accessed June 19, 2019. http://scholar.colorado.edu/asen_gradetds/100.

MLA Handbook (7th Edition):

Chabot, Joshua A. “A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control.” 2015. Web. 19 Jun 2019.

Vancouver:

Chabot JA. A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control. [Internet] [Masters thesis]. University of Colorado; 2015. [cited 2019 Jun 19]. Available from: http://scholar.colorado.edu/asen_gradetds/100.

Council of Science Editors:

Chabot JA. A Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control. [Masters Thesis]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/100


University of Hawaii – Manoa

13. Nunes, Miguel. Multi-Agent Robotic Systems and Applications for Satellite Missions.

Degree: 2017, University of Hawaii – Manoa

Ph.D. University of Hawaii at Manoa 2016.

A revolution in the space sector is happening. It is expected that in the next decade there will… (more)

Subjects/Keywords: Multi-Agent Robotic Systems; Satellite Attitude Control; Automated Rendezvous and Docking; Guidance Navigation and Control; Satellite Constellation

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APA (6th Edition):

Nunes, M. (2017). Multi-Agent Robotic Systems and Applications for Satellite Missions. (Thesis). University of Hawaii – Manoa. Retrieved from http://hdl.handle.net/10125/51398

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):

Nunes, Miguel. “Multi-Agent Robotic Systems and Applications for Satellite Missions.” 2017. Thesis, University of Hawaii – Manoa. Accessed June 19, 2019. http://hdl.handle.net/10125/51398.

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

MLA Handbook (7th Edition):

Nunes, Miguel. “Multi-Agent Robotic Systems and Applications for Satellite Missions.” 2017. Web. 19 Jun 2019.

Vancouver:

Nunes M. Multi-Agent Robotic Systems and Applications for Satellite Missions. [Internet] [Thesis]. University of Hawaii – Manoa; 2017. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/10125/51398.

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

Council of Science Editors:

Nunes M. Multi-Agent Robotic Systems and Applications for Satellite Missions. [Thesis]. University of Hawaii – Manoa; 2017. Available from: http://hdl.handle.net/10125/51398

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


Marietta College

14. Gingrich, Amy Marie. Effects of Motivational Interviewing on Improving Attitude toward Exercise in College Students.

Degree: MA, Psychology, 2008, Marietta College

 Motivational interviewing (MI) was used with college students in an attempt to improve attitudes towards exercise. Thirty-eight participants between 18 and 24 years of age… (more)

Subjects/Keywords: Academic Guidance Counseling; Behaviorial Sciences; Health; Psychology; motivational interviewing; college students; exercise; attitude toward exercise; sedentary behavior; benefits of exercise

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APA (6th Edition):

Gingrich, A. M. (2008). Effects of Motivational Interviewing on Improving Attitude toward Exercise in College Students. (Masters Thesis). Marietta College. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=marietta1220494280

Chicago Manual of Style (16th Edition):

Gingrich, Amy Marie. “Effects of Motivational Interviewing on Improving Attitude toward Exercise in College Students.” 2008. Masters Thesis, Marietta College. Accessed June 19, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=marietta1220494280.

MLA Handbook (7th Edition):

Gingrich, Amy Marie. “Effects of Motivational Interviewing on Improving Attitude toward Exercise in College Students.” 2008. Web. 19 Jun 2019.

Vancouver:

Gingrich AM. Effects of Motivational Interviewing on Improving Attitude toward Exercise in College Students. [Internet] [Masters thesis]. Marietta College; 2008. [cited 2019 Jun 19]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=marietta1220494280.

Council of Science Editors:

Gingrich AM. Effects of Motivational Interviewing on Improving Attitude toward Exercise in College Students. [Masters Thesis]. Marietta College; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=marietta1220494280


Ryerson University

15. Wong, Frank Y.W. Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point.

Degree: 2009, Ryerson University

 This thesis examines the use of thrusters and solar sails for spacecraft formation keeping control at the Earth-Moon L4 point. Particular emphasis was placed on… (more)

Subjects/Keywords: Space trajectories; Guidance systems (Flight); Navigation (Astronautics); Space vehicles  – Propulsion systems; Space vehicles  – Attitude control systems; Flight control

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

APA (6th Edition):

Wong, F. Y. W. (2009). Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1550

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):

Wong, Frank Y W. “Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point.” 2009. Thesis, Ryerson University. Accessed June 19, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A1550.

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

MLA Handbook (7th Edition):

Wong, Frank Y W. “Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point.” 2009. Web. 19 Jun 2019.

Vancouver:

Wong FYW. Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point. [Internet] [Thesis]. Ryerson University; 2009. [cited 2019 Jun 19]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1550.

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

Council of Science Editors:

Wong FYW. Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point. [Thesis]. Ryerson University; 2009. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1550

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


Virginia Tech

16. Atkins, Brad Matthew. Mars Precision Entry Vehicle Guidance Using Internal Moving Mass Actuators.

Degree: PhD, Aerospace and Ocean Engineering, 2014, Virginia Tech

 Many landing sites of scientific interest on Mars including most of the Southern Hemisphere at elevations above 2km Mars Orbiter Laser Altimeter reference are inaccessible… (more)

Subjects/Keywords: Mars; Precision Entry Guidance; Capsules; Hypersonic Inflatable Aerodynamic Decelerators; Attitude Control; Center of Mass Control; Internal Moving Mass Actuators

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APA (6th Edition):

Atkins, B. M. (2014). Mars Precision Entry Vehicle Guidance Using Internal Moving Mass Actuators. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50648

Chicago Manual of Style (16th Edition):

Atkins, Brad Matthew. “Mars Precision Entry Vehicle Guidance Using Internal Moving Mass Actuators.” 2014. Doctoral Dissertation, Virginia Tech. Accessed June 19, 2019. http://hdl.handle.net/10919/50648.

MLA Handbook (7th Edition):

Atkins, Brad Matthew. “Mars Precision Entry Vehicle Guidance Using Internal Moving Mass Actuators.” 2014. Web. 19 Jun 2019.

Vancouver:

Atkins BM. Mars Precision Entry Vehicle Guidance Using Internal Moving Mass Actuators. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/10919/50648.

Council of Science Editors:

Atkins BM. Mars Precision Entry Vehicle Guidance Using Internal Moving Mass Actuators. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/50648

17. 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 June 19, 2019. 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. 19 Jun 2019.

Vancouver:

Abdallah AM. Flight Dynamics Nonlinearity Assessment Across a New Aerodynamic Attitude Flight Envelope. [Internet] [Doctoral dissertation]. Old Dominion University; 2015. [cited 2019 Jun 19]. 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 Oklahoma

18. Simmons, Milton Delbert. The relationship of personality characteristics to attitudes of ministerial students.

Degree: PhD, 1967, University of Oklahoma

Subjects/Keywords: Education, Guidance and Counseling.; Personality.; Seminarians.; Clergy.; Attitude (Psychology)

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APA (6th Edition):

Simmons, M. D. (1967). The relationship of personality characteristics to attitudes of ministerial students. (Doctoral Dissertation). University of Oklahoma. Retrieved from http://hdl.handle.net/11244/2252

Chicago Manual of Style (16th Edition):

Simmons, Milton Delbert. “The relationship of personality characteristics to attitudes of ministerial students.” 1967. Doctoral Dissertation, University of Oklahoma. Accessed June 19, 2019. http://hdl.handle.net/11244/2252.

MLA Handbook (7th Edition):

Simmons, Milton Delbert. “The relationship of personality characteristics to attitudes of ministerial students.” 1967. Web. 19 Jun 2019.

Vancouver:

Simmons MD. The relationship of personality characteristics to attitudes of ministerial students. [Internet] [Doctoral dissertation]. University of Oklahoma; 1967. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/11244/2252.

Council of Science Editors:

Simmons MD. The relationship of personality characteristics to attitudes of ministerial students. [Doctoral Dissertation]. University of Oklahoma; 1967. Available from: http://hdl.handle.net/11244/2252

19. Kjellberg, Henri Christian. Constrained attitude guidance and control for satellites.

Degree: Aerospace Engineering, 2014, University of Texas – Austin

 To satisfy the requirements of small satellites with attitude control requirements, a guidance, navigation, and control module was designed at the Texas Spacecraft Laboratory. However,… (more)

Subjects/Keywords: Constrained attitude guidance; Control satellites; Unmanned vehicles

…discretized constrained attitude guidance and control scheme… …entire spacecraft mission pointing architecture. The result is an attitude guidance and control… …presents the motivation for performing autonomous con- strained guidance and attitude… …algorithm to produce 2 an end-to-end closed-loop autonomous attitude guidance and control… …architecture for autonomous constrained attitude guidance and control, the spacecraft being developed… 

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APA (6th Edition):

Kjellberg, H. C. (2014). Constrained attitude guidance and control for satellites. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/28313

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):

Kjellberg, Henri Christian. “Constrained attitude guidance and control for satellites.” 2014. Thesis, University of Texas – Austin. Accessed June 19, 2019. http://hdl.handle.net/2152/28313.

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

MLA Handbook (7th Edition):

Kjellberg, Henri Christian. “Constrained attitude guidance and control for satellites.” 2014. Web. 19 Jun 2019.

Vancouver:

Kjellberg HC. Constrained attitude guidance and control for satellites. [Internet] [Thesis]. University of Texas – Austin; 2014. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/2152/28313.

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

Council of Science Editors:

Kjellberg HC. Constrained attitude guidance and control for satellites. [Thesis]. University of Texas – Austin; 2014. Available from: http://hdl.handle.net/2152/28313

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


University of Colorado

20. 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 June 19, 2019. 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. 19 Jun 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 Jun 19]. 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

21. Liston, Curtis Thomas. Level of manifest anxiety as a predictor of attitude change through group vocational counseling.

Degree: 1973, North Texas State University

 This study was conducted to compare changes in self-concept and dogmatism among high school subjects at three levels of manifest anxiety following group vocational counseling.… (more)

Subjects/Keywords: group counseling; anxiety; vocational guidance; attitude change

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APA (6th Edition):

Liston, C. T. (1973). Level of manifest anxiety as a predictor of attitude change through group vocational counseling. (Thesis). North Texas State University. Retrieved from https://digital.library.unt.edu/ark:/67531/metadc798291/

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):

Liston, Curtis Thomas. “Level of manifest anxiety as a predictor of attitude change through group vocational counseling.” 1973. Thesis, North Texas State University. Accessed June 19, 2019. https://digital.library.unt.edu/ark:/67531/metadc798291/.

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

MLA Handbook (7th Edition):

Liston, Curtis Thomas. “Level of manifest anxiety as a predictor of attitude change through group vocational counseling.” 1973. Web. 19 Jun 2019.

Vancouver:

Liston CT. Level of manifest anxiety as a predictor of attitude change through group vocational counseling. [Internet] [Thesis]. North Texas State University; 1973. [cited 2019 Jun 19]. Available from: https://digital.library.unt.edu/ark:/67531/metadc798291/.

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

Council of Science Editors:

Liston CT. Level of manifest anxiety as a predictor of attitude change through group vocational counseling. [Thesis]. North Texas State University; 1973. Available from: https://digital.library.unt.edu/ark:/67531/metadc798291/

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


Vanderbilt University

22. Lyne, Christopher Tucker. Calibration and Testing of Rapid Prototyped Nozzles for Guidance and Control.

Degree: MS, Mechanical Engineering, 2017, Vanderbilt University

 Additive manufacturing of plastics, commonly referred to as Rapid Prototyping, is an emerging field with the potential to improve the performance of guidance and control… (more)

Subjects/Keywords: cold gas propulsion; rapid prototyping; attitude control; thrust measurement; guidance and control; cold gas thruster; additive manufacturing; 3D printing

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APA (6th Edition):

Lyne, C. T. (2017). Calibration and Testing of Rapid Prototyped Nozzles for Guidance and Control. (Masters Thesis). Vanderbilt University. Retrieved from http://etd.library.vanderbilt.edu/available/etd-11252017-181933/ ;

Chicago Manual of Style (16th Edition):

Lyne, Christopher Tucker. “Calibration and Testing of Rapid Prototyped Nozzles for Guidance and Control.” 2017. Masters Thesis, Vanderbilt University. Accessed June 19, 2019. http://etd.library.vanderbilt.edu/available/etd-11252017-181933/ ;.

MLA Handbook (7th Edition):

Lyne, Christopher Tucker. “Calibration and Testing of Rapid Prototyped Nozzles for Guidance and Control.” 2017. Web. 19 Jun 2019.

Vancouver:

Lyne CT. Calibration and Testing of Rapid Prototyped Nozzles for Guidance and Control. [Internet] [Masters thesis]. Vanderbilt University; 2017. [cited 2019 Jun 19]. Available from: http://etd.library.vanderbilt.edu/available/etd-11252017-181933/ ;.

Council of Science Editors:

Lyne CT. Calibration and Testing of Rapid Prototyped Nozzles for Guidance and Control. [Masters Thesis]. Vanderbilt University; 2017. Available from: http://etd.library.vanderbilt.edu/available/etd-11252017-181933/ ;


University of Kentucky

23. Evans, Joshua L. SMALL SATELLITE NONCOMMUTATIVE ROTATION SEQUENCE ATTITUDE CONTROL USING PIEZOELECTRIC ACTUATORS.

Degree: 2016, University of Kentucky

Attitude control remains one of the top engineering challenges faced by small satellite mission planning and design. Conventional methods for attitude control include propulsion, reaction… (more)

Subjects/Keywords: Small Satellites; CubeSats; Piezoelectric Bimorph; Attitude Control; Noncommutative Rotations; Aeronautical Vehicles; Controls and Control Theory; Electrical and Electronics; Navigation, Guidance, Control and Dynamics; Space Vehicles

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APA (6th Edition):

Evans, J. L. (2016). SMALL SATELLITE NONCOMMUTATIVE ROTATION SEQUENCE ATTITUDE CONTROL USING PIEZOELECTRIC ACTUATORS. (Masters Thesis). University of Kentucky. Retrieved from http://uknowledge.uky.edu/ece_etds/91

Chicago Manual of Style (16th Edition):

Evans, Joshua L. “SMALL SATELLITE NONCOMMUTATIVE ROTATION SEQUENCE ATTITUDE CONTROL USING PIEZOELECTRIC ACTUATORS.” 2016. Masters Thesis, University of Kentucky. Accessed June 19, 2019. http://uknowledge.uky.edu/ece_etds/91.

MLA Handbook (7th Edition):

Evans, Joshua L. “SMALL SATELLITE NONCOMMUTATIVE ROTATION SEQUENCE ATTITUDE CONTROL USING PIEZOELECTRIC ACTUATORS.” 2016. Web. 19 Jun 2019.

Vancouver:

Evans JL. SMALL SATELLITE NONCOMMUTATIVE ROTATION SEQUENCE ATTITUDE CONTROL USING PIEZOELECTRIC ACTUATORS. [Internet] [Masters thesis]. University of Kentucky; 2016. [cited 2019 Jun 19]. Available from: http://uknowledge.uky.edu/ece_etds/91.

Council of Science Editors:

Evans JL. SMALL SATELLITE NONCOMMUTATIVE ROTATION SEQUENCE ATTITUDE CONTROL USING PIEZOELECTRIC ACTUATORS. [Masters Thesis]. University of Kentucky; 2016. Available from: http://uknowledge.uky.edu/ece_etds/91


University of Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Stevenson, Daan. “Remote Spacecraft Attitude Control by Coulomb Charging.” 2015. Doctoral Dissertation, University of Colorado. Accessed June 19, 2019. http://scholar.colorado.edu/asen_gradetds/94.

MLA Handbook (7th Edition):

Stevenson, Daan. “Remote Spacecraft Attitude Control by Coulomb Charging.” 2015. Web. 19 Jun 2019.

Vancouver:

Stevenson D. Remote Spacecraft Attitude Control by Coulomb Charging. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Jun 19]. Available from: http://scholar.colorado.edu/asen_gradetds/94.

Council of Science Editors:

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


University of Nairobi

25. Gitonga, Purity K. A study of secondary school head-teachers' attitudes towards guidance and counseling programme in Meru central district .

Degree: 1999, University of Nairobi

 The main purpose of the study was to determine secondary school headteachers' attitude towards guidance and counselling programme; a pupil personnel service. The study also… (more)

Subjects/Keywords: Guidance & counseling; Head-teacher attitude; Secondary school; Meru central district

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APA (6th Edition):

Gitonga, P. K. (1999). A study of secondary school head-teachers' attitudes towards guidance and counseling programme in Meru central district . (Thesis). University of Nairobi. Retrieved from http://erepository.uonbi.ac.ke:8080/xmlui/handle/123456789/17724

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):

Gitonga, Purity K. “A study of secondary school head-teachers' attitudes towards guidance and counseling programme in Meru central district .” 1999. Thesis, University of Nairobi. Accessed June 19, 2019. http://erepository.uonbi.ac.ke:8080/xmlui/handle/123456789/17724.

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

MLA Handbook (7th Edition):

Gitonga, Purity K. “A study of secondary school head-teachers' attitudes towards guidance and counseling programme in Meru central district .” 1999. Web. 19 Jun 2019.

Vancouver:

Gitonga PK. A study of secondary school head-teachers' attitudes towards guidance and counseling programme in Meru central district . [Internet] [Thesis]. University of Nairobi; 1999. [cited 2019 Jun 19]. Available from: http://erepository.uonbi.ac.ke:8080/xmlui/handle/123456789/17724.

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

Council of Science Editors:

Gitonga PK. A study of secondary school head-teachers' attitudes towards guidance and counseling programme in Meru central district . [Thesis]. University of Nairobi; 1999. Available from: http://erepository.uonbi.ac.ke:8080/xmlui/handle/123456789/17724

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


Durban University of Technology

26. Naicker, Daphanie. Tourism graduate employability : stakeholder perceptions of workplace learning for graduate employment.

Degree: 2017, Durban University of Technology

Submitted in fulfillment of the requirements for the Masters in Management Sciences: Tourism and Hospitality Management, Durban University of Technology, Durban, South Africa, 2017.

With… (more)

Subjects/Keywords: WIL; WPL; Perceptions; Attitude; Employability; Supervision; Success; Tourism – Study and teaching (Higher) – South Africa; Tourism – Vocational guidance – South Africa; College graduates – Employment – South Africa; Employability – South Africa

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APA (6th Edition):

Naicker, D. (2017). Tourism graduate employability : stakeholder perceptions of workplace learning for graduate employment. (Thesis). Durban University of Technology. Retrieved from http://hdl.handle.net/10321/2549

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):

Naicker, Daphanie. “Tourism graduate employability : stakeholder perceptions of workplace learning for graduate employment.” 2017. Thesis, Durban University of Technology. Accessed June 19, 2019. http://hdl.handle.net/10321/2549.

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

MLA Handbook (7th Edition):

Naicker, Daphanie. “Tourism graduate employability : stakeholder perceptions of workplace learning for graduate employment.” 2017. Web. 19 Jun 2019.

Vancouver:

Naicker D. Tourism graduate employability : stakeholder perceptions of workplace learning for graduate employment. [Internet] [Thesis]. Durban University of Technology; 2017. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/10321/2549.

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

Council of Science Editors:

Naicker D. Tourism graduate employability : stakeholder perceptions of workplace learning for graduate employment. [Thesis]. Durban University of Technology; 2017. Available from: http://hdl.handle.net/10321/2549

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


Linköping University

27. Abrahamsson, Per. Combined Platform for Boost Guidance and Attitude Control for Sounding Rockets.

Degree: Electrical Engineering, 2004, Linköping University

  This report handles the preliminary design of a control system that includes both attitude control and boost control functionality for sounding rockets. This is… (more)

Subjects/Keywords: Reglerteknik; sounding rocket; attitude control; stabilization; boost guidance; Reglerteknik; Automatic control; Reglerteknik

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APA (6th Edition):

Abrahamsson, P. (2004). Combined Platform for Boost Guidance and Attitude Control for Sounding Rockets. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-2203

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):

Abrahamsson, Per. “Combined Platform for Boost Guidance and Attitude Control for Sounding Rockets.” 2004. Thesis, Linköping University. Accessed June 19, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-2203.

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

MLA Handbook (7th Edition):

Abrahamsson, Per. “Combined Platform for Boost Guidance and Attitude Control for Sounding Rockets.” 2004. Web. 19 Jun 2019.

Vancouver:

Abrahamsson P. Combined Platform for Boost Guidance and Attitude Control for Sounding Rockets. [Internet] [Thesis]. Linköping University; 2004. [cited 2019 Jun 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-2203.

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

Council of Science Editors:

Abrahamsson P. Combined Platform for Boost Guidance and Attitude Control for Sounding Rockets. [Thesis]. Linköping University; 2004. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-2203

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


University of South Africa

28. Dlamini, Nqobile Faith. Factors influencing the choice of agriculture as a study discipline by undergraduates: a case study of a distance university's agriculture department.

Degree: 2017, University of South Africa

 Enrolments in agriculture programmes at universities in South Africa are low when compared to the other programmes. The purpose of this study was therefore to… (more)

Subjects/Keywords: Career choice; FET; Agriculture curricula; National Senior Certificate; Student enrolments; Universities; Subject choice; Agriculture educators; University students; Career guidance and counselling; Learners attitude towards agriculture; Parents

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APA (6th Edition):

Dlamini, N. F. (2017). Factors influencing the choice of agriculture as a study discipline by undergraduates: a case study of a distance university's agriculture department. (Masters Thesis). University of South Africa. Retrieved from http://hdl.handle.net/10500/23377

Chicago Manual of Style (16th Edition):

Dlamini, Nqobile Faith. “Factors influencing the choice of agriculture as a study discipline by undergraduates: a case study of a distance university's agriculture department.” 2017. Masters Thesis, University of South Africa. Accessed June 19, 2019. http://hdl.handle.net/10500/23377.

MLA Handbook (7th Edition):

Dlamini, Nqobile Faith. “Factors influencing the choice of agriculture as a study discipline by undergraduates: a case study of a distance university's agriculture department.” 2017. Web. 19 Jun 2019.

Vancouver:

Dlamini NF. Factors influencing the choice of agriculture as a study discipline by undergraduates: a case study of a distance university's agriculture department. [Internet] [Masters thesis]. University of South Africa; 2017. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/10500/23377.

Council of Science Editors:

Dlamini NF. Factors influencing the choice of agriculture as a study discipline by undergraduates: a case study of a distance university's agriculture department. [Masters Thesis]. University of South Africa; 2017. Available from: http://hdl.handle.net/10500/23377

29. Krantz, Elias. Experiment Design for System Identification on Satellite Hardware Demonstrator.

Degree: Electrical and Space Engineering, 2018, Luleå University of Technology

  The subject of this thesis covers the process of online parameter estimation of agile satellites. Accurate knowledge of parameters such as moment of inertia… (more)

Subjects/Keywords: LTU; Airbus; Attitude; Guidance; Control; AOCS; GNC; Kalman Filter; UKF; System Identification; SysId; Estimation; Determination; CMG; Control Engineering; Reglerteknik; Signal Processing; Signalbehandling; Aerospace Engineering; Rymd- och flygteknik

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

APA (6th Edition):

Krantz, E. (2018). Experiment Design for System Identification on Satellite Hardware Demonstrator. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71351

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):

Krantz, Elias. “Experiment Design for System Identification on Satellite Hardware Demonstrator.” 2018. Thesis, Luleå University of Technology. Accessed June 19, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71351.

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

MLA Handbook (7th Edition):

Krantz, Elias. “Experiment Design for System Identification on Satellite Hardware Demonstrator.” 2018. Web. 19 Jun 2019.

Vancouver:

Krantz E. Experiment Design for System Identification on Satellite Hardware Demonstrator. [Internet] [Thesis]. Luleå University of Technology; 2018. [cited 2019 Jun 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71351.

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

Council of Science Editors:

Krantz E. Experiment Design for System Identification on Satellite Hardware Demonstrator. [Thesis]. Luleå University of Technology; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71351

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


Texas A&M University

30. Tallant, Gregory Stephen. A Kalman filtering technique for spacecraft attitude determination and control using Gibbs vector.

Degree: MS, aerospace engineering, 2012, Texas A&M University

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.; Kalman filtering - Technique.; Space vehicles - Attitude control systems.; Space vehicles - Guidance systems.

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

APA (6th Edition):

Tallant, G. S. (2012). A Kalman filtering technique for spacecraft attitude determination and control using Gibbs vector. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-T147

Chicago Manual of Style (16th Edition):

Tallant, Gregory Stephen. “A Kalman filtering technique for spacecraft attitude determination and control using Gibbs vector.” 2012. Masters Thesis, Texas A&M University. Accessed June 19, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-T147.

MLA Handbook (7th Edition):

Tallant, Gregory Stephen. “A Kalman filtering technique for spacecraft attitude determination and control using Gibbs vector.” 2012. Web. 19 Jun 2019.

Vancouver:

Tallant GS. A Kalman filtering technique for spacecraft attitude determination and control using Gibbs vector. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2019 Jun 19]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-T147.

Council of Science Editors:

Tallant GS. A Kalman filtering technique for spacecraft attitude determination and control using Gibbs vector. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-T147

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