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You searched for subject:(Aerospace Vehicles Guidance AND Control). Showing records 1 – 30 of 275 total matches.

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Indian Institute of Science

1. Das, Priya G. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.

Degree: 2009, Indian Institute of Science

 To address the concern of classical guidance and control designs (where guidance and control loops are designed separately in an “outer loop – inner loop”… (more)

Subjects/Keywords: Aerospace Vehicles - Guidance and Control; Interceptors (Aerospace Engineering); Guidance Systems (Flight); Flight Control; Endo-Atmospheric Interceptors; Partial Integrated Guidance and Control; Integrated Guidance and Control (IGC); Impact Angle Constraint; Astronautics

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

APA (6th Edition):

Das, P. G. (2009). Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1099

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):

Das, Priya G. “Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.” 2009. Thesis, Indian Institute of Science. Accessed December 13, 2019. http://hdl.handle.net/2005/1099.

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

MLA Handbook (7th Edition):

Das, Priya G. “Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.” 2009. Web. 13 Dec 2019.

Vancouver:

Das PG. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2019 Dec 13]. Available from: http://hdl.handle.net/2005/1099.

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

Council of Science Editors:

Das PG. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/1099

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


University of Colorado

2. 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 December 13, 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. 13 Dec 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 Dec 13]. 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


Indian Institute of Science

3. Abdul Saleem, P K. Guidance Laws for Engagement Time Control.

Degree: 2016, Indian Institute of Science

 Autonomous aerial vehicles like missiles and unmanned aerial vehicles (UAVs) have attracted various military and civilian applications. The primary guidance objective of any autonomous vehicle… (more)

Subjects/Keywords: Unmanned Aerial Vehicles; Missile Impact Time Control; Guidance Laws; Missile Guidance; Impact Time Control Guidance Law; Unmanned Aerial Vehcile Arrival Time Control; Lyapunov Guidance Law; Unmanned Aerial Vehicle Guidance; Nonlinear Guidance Laws; Autonomous Aerial Vehicles; Missiles; Salvo Attack; Impact Time Control; UAVs; Aerospace Engineering

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APA (6th Edition):

Abdul Saleem, P. K. (2016). Guidance Laws for Engagement Time Control. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2926

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):

Abdul Saleem, P K. “Guidance Laws for Engagement Time Control.” 2016. Thesis, Indian Institute of Science. Accessed December 13, 2019. http://hdl.handle.net/2005/2926.

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

MLA Handbook (7th Edition):

Abdul Saleem, P K. “Guidance Laws for Engagement Time Control.” 2016. Web. 13 Dec 2019.

Vancouver:

Abdul Saleem PK. Guidance Laws for Engagement Time Control. [Internet] [Thesis]. Indian Institute of Science; 2016. [cited 2019 Dec 13]. Available from: http://hdl.handle.net/2005/2926.

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

Council of Science Editors:

Abdul Saleem PK. Guidance Laws for Engagement Time Control. [Thesis]. Indian Institute of Science; 2016. Available from: http://hdl.handle.net/2005/2926

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


Indian Institute of Science

4. Maity, Arnab. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.

Degree: 2012, Indian Institute of Science

 A new suboptimal guidance law design approach for aerospace vehicles is proposed in this thesis, followed by an advanced control design for supersonic air-breathing engines.… (more)

Subjects/Keywords: Aerospace Vehicles; Aerospace Vehicles - Guidance and Control; Air-Breathing Engines - Control; Generalized Model Predictive Static Programming (G-MPSP); Supersonic Air-Breathing Engines; Launch Vehicles (Astronautics); Solid Motor Propelled Carrier Launch Vehicle; Air-Breathing Vehicles - Guidance; Kalman Filtering; Flight Trajectory; Supersonic Air-Breathing Vehicles - Guidance; Supersonic Air-Breathing Vehicle; Hypersonic Mission; Extended Kalman Filter (EKF); Optimal Control Theory; Astronautics

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

APA (6th Edition):

Maity, A. (2012). Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2550

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):

Maity, Arnab. “Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.” 2012. Thesis, Indian Institute of Science. Accessed December 13, 2019. http://hdl.handle.net/2005/2550.

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

MLA Handbook (7th Edition):

Maity, Arnab. “Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.” 2012. Web. 13 Dec 2019.

Vancouver:

Maity A. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Dec 13]. Available from: http://hdl.handle.net/2005/2550.

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

Council of Science Editors:

Maity A. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. [Thesis]. Indian Institute of Science; 2012. Available from: http://hdl.handle.net/2005/2550

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


Indian Institute of Science

5. Maity, Arnab. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.

Degree: 2012, Indian Institute of Science

 A new suboptimal guidance law design approach for aerospace vehicles is proposed in this thesis, followed by an advanced control design for supersonic air-breathing engines.… (more)

Subjects/Keywords: Aerospace Vehicles; Aerospace Vehicles - Guidance and Control; Air-Breathing Engines - Control; Generalized Model Predictive Static Programming (G-MPSP); Supersonic Air-Breathing Engines; Launch Vehicles (Astronautics); Solid Motor Propelled Carrier Launch Vehicle; Air-Breathing Vehicles - Guidance; Kalman Filtering; Flight Trajectory; Supersonic Air-Breathing Vehicles - Guidance; Supersonic Air-Breathing Vehicle; Hypersonic Mission; Extended Kalman Filter (EKF); Optimal Control Theory; Astronautics

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

APA (6th Edition):

Maity, A. (2012). Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2550 ; http://etd.ncsi.iisc.ernet.in/abstracts/3308/G25667-Abs.pdf

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):

Maity, Arnab. “Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.” 2012. Thesis, Indian Institute of Science. Accessed December 13, 2019. http://etd.iisc.ernet.in/handle/2005/2550 ; http://etd.ncsi.iisc.ernet.in/abstracts/3308/G25667-Abs.pdf.

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

MLA Handbook (7th Edition):

Maity, Arnab. “Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.” 2012. Web. 13 Dec 2019.

Vancouver:

Maity A. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Dec 13]. Available from: http://etd.iisc.ernet.in/handle/2005/2550 ; http://etd.ncsi.iisc.ernet.in/abstracts/3308/G25667-Abs.pdf.

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

Council of Science Editors:

Maity A. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. [Thesis]. Indian Institute of Science; 2012. Available from: http://etd.iisc.ernet.in/handle/2005/2550 ; http://etd.ncsi.iisc.ernet.in/abstracts/3308/G25667-Abs.pdf

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


Cal Poly

6. Belfield, Eric. Assessment of Asymmetric Flight on Solar UAS.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  An investigation was conducted into the feasibility of using an unconventional flight technique, asymmetric flight, to improve overall efficiency of solar aircraft. In this… (more)

Subjects/Keywords: asymmetric flight; aircraft performance; solar aircraft; UAS; Aerodynamics and Fluid Mechanics; Aeronautical Vehicles; Navigation, Guidance, Control and Dynamics; Other Aerospace Engineering

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APA (6th Edition):

Belfield, E. (2016). Assessment of Asymmetric Flight on Solar UAS. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1676

Chicago Manual of Style (16th Edition):

Belfield, Eric. “Assessment of Asymmetric Flight on Solar UAS.” 2016. Masters Thesis, Cal Poly. Accessed December 13, 2019. https://digitalcommons.calpoly.edu/theses/1676.

MLA Handbook (7th Edition):

Belfield, Eric. “Assessment of Asymmetric Flight on Solar UAS.” 2016. Web. 13 Dec 2019.

Vancouver:

Belfield E. Assessment of Asymmetric Flight on Solar UAS. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2019 Dec 13]. Available from: https://digitalcommons.calpoly.edu/theses/1676.

Council of Science Editors:

Belfield E. Assessment of Asymmetric Flight on Solar UAS. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1676


University of Tennessee – Knoxville

7. Vallabhaneni, Naveen Kumar. Continuously Variable Rotorcraft Propulsion System: Modelling and Simulation.

Degree: MS, Aerospace Engineering, 2011, University of Tennessee – Knoxville

  This study explores the variable speed operation and shift response of a prototype of a two speed single path CVT rotorcraft driveline system. Here… (more)

Subjects/Keywords: CVT; gasturbine; control system; rotorcraft model; propulsion system; Acoustics, Dynamics, and Controls; Aerodynamics and Fluid Mechanics; Aeronautical Vehicles; Aerospace Engineering; Navigation, Guidance, Control and Dynamics; Propulsion and Power

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APA (6th Edition):

Vallabhaneni, N. K. (2011). Continuously Variable Rotorcraft Propulsion System: Modelling and Simulation. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/1033

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):

Vallabhaneni, Naveen Kumar. “Continuously Variable Rotorcraft Propulsion System: Modelling and Simulation.” 2011. Thesis, University of Tennessee – Knoxville. Accessed December 13, 2019. https://trace.tennessee.edu/utk_gradthes/1033.

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

MLA Handbook (7th Edition):

Vallabhaneni, Naveen Kumar. “Continuously Variable Rotorcraft Propulsion System: Modelling and Simulation.” 2011. Web. 13 Dec 2019.

Vancouver:

Vallabhaneni NK. Continuously Variable Rotorcraft Propulsion System: Modelling and Simulation. [Internet] [Thesis]. University of Tennessee – Knoxville; 2011. [cited 2019 Dec 13]. Available from: https://trace.tennessee.edu/utk_gradthes/1033.

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

Council of Science Editors:

Vallabhaneni NK. Continuously Variable Rotorcraft Propulsion System: Modelling and Simulation. [Thesis]. University of Tennessee – Knoxville; 2011. Available from: https://trace.tennessee.edu/utk_gradthes/1033

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


Texas A&M University

8. 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 (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 December 13, 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. 13 Dec 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 Dec 13]. 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


Cal Poly

9. Brake, Nicholas J. Control System Development for small UAV Gimbal.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  The design process of unmanned ISR systems has typically driven in the direction of increasing system mass to increase stabilization performance and imagery quality.… (more)

Subjects/Keywords: Aerospace Engineering; Navigation, Guidance, Control and Dynamics; Other Aerospace Engineering

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APA (6th Edition):

Brake, N. J. (2012). Control System Development for small UAV Gimbal. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/838 ; 10.15368/theses.2012.155

Chicago Manual of Style (16th Edition):

Brake, Nicholas J. “Control System Development for small UAV Gimbal.” 2012. Masters Thesis, Cal Poly. Accessed December 13, 2019. https://digitalcommons.calpoly.edu/theses/838 ; 10.15368/theses.2012.155.

MLA Handbook (7th Edition):

Brake, Nicholas J. “Control System Development for small UAV Gimbal.” 2012. Web. 13 Dec 2019.

Vancouver:

Brake NJ. Control System Development for small UAV Gimbal. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Dec 13]. Available from: https://digitalcommons.calpoly.edu/theses/838 ; 10.15368/theses.2012.155.

Council of Science Editors:

Brake NJ. Control System Development for small UAV Gimbal. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/838 ; 10.15368/theses.2012.155


Iowa State University

10. Mathur, Sanjay R. Three dimensional analysis of a rotor in forward flight.

Degree: 1989, Iowa State University

Subjects/Keywords: Aerospace engineering; Aeronautical Vehicles; Navigation, Guidance, Control and Dynamics; Space Vehicles; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Mathur, S. R. (1989). Three dimensional analysis of a rotor in forward flight. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/rtd/16925

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):

Mathur, Sanjay R. “Three dimensional analysis of a rotor in forward flight.” 1989. Thesis, Iowa State University. Accessed December 13, 2019. https://lib.dr.iastate.edu/rtd/16925.

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

MLA Handbook (7th Edition):

Mathur, Sanjay R. “Three dimensional analysis of a rotor in forward flight.” 1989. Web. 13 Dec 2019.

Vancouver:

Mathur SR. Three dimensional analysis of a rotor in forward flight. [Internet] [Thesis]. Iowa State University; 1989. [cited 2019 Dec 13]. Available from: https://lib.dr.iastate.edu/rtd/16925.

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

Council of Science Editors:

Mathur SR. Three dimensional analysis of a rotor in forward flight. [Thesis]. Iowa State University; 1989. Available from: https://lib.dr.iastate.edu/rtd/16925

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


Virginia Tech

11. Balasubramanian, Balasundar. A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints.

Degree: MS, Electrical and Computer Engineering, 2010, Virginia Tech

 We present a new trajectory generation algorithm for autonomous guidance and control of unmanned vehicles from a given starting point to a given target location.… (more)

Subjects/Keywords: path planning; guidance; trajectory generation; unmanned vehicles; receding horizon control

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APA (6th Edition):

Balasubramanian, B. (2010). A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36430

Chicago Manual of Style (16th Edition):

Balasubramanian, Balasundar. “A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints.” 2010. Masters Thesis, Virginia Tech. Accessed December 13, 2019. http://hdl.handle.net/10919/36430.

MLA Handbook (7th Edition):

Balasubramanian, Balasundar. “A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints.” 2010. Web. 13 Dec 2019.

Vancouver:

Balasubramanian B. A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2019 Dec 13]. Available from: http://hdl.handle.net/10919/36430.

Council of Science Editors:

Balasubramanian B. A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/36430


Indian Institute of Science

12. Kumar, Shashi Ranjan. Sliding Mode Control Based Guidance Strategies with Terminal Constraints.

Degree: 2015, Indian Institute of Science

 In the guidance literature, minimizing miss distance along with optimizing the energy usage had been an objective for several decades. In current day applications, additional… (more)

Subjects/Keywords: Sliding Mode Control; Guidance and Control Theory; Sliding Mode Guidance Laws; Impact Angle Guidance; Impact Time Guidance; Guidance Laws; Sliding Mode Guidance; Salvo Attack Guidance; Nonlinear Engagement Dynamics; Missile Guidance; Flight Control; Finite Time Convergence; Sliding-Mode Guidance; Impact Time Guidance; Aerospace Engineering

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APA (6th Edition):

Kumar, S. R. (2015). Sliding Mode Control Based Guidance Strategies with Terminal Constraints. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-Abs.pdf

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):

Kumar, Shashi Ranjan. “Sliding Mode Control Based Guidance Strategies with Terminal Constraints.” 2015. Thesis, Indian Institute of Science. Accessed December 13, 2019. http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-Abs.pdf.

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

MLA Handbook (7th Edition):

Kumar, Shashi Ranjan. “Sliding Mode Control Based Guidance Strategies with Terminal Constraints.” 2015. Web. 13 Dec 2019.

Vancouver:

Kumar SR. Sliding Mode Control Based Guidance Strategies with Terminal Constraints. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Dec 13]. Available from: http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-Abs.pdf.

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

Council of Science Editors:

Kumar SR. Sliding Mode Control Based Guidance Strategies with Terminal Constraints. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-Abs.pdf

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

13. Tran, Thanh Trung. Nonlinear Flight Control Design Using Backstepping Methodology.

Degree: PhD, Aerospace Engineering, 2016, Old Dominion University

  The subject of nonlinear flight control design using backstepping control methodology is investigated in the dissertation research presented here. Control design methods based on… (more)

Subjects/Keywords: Backstepping control; Lyapunov-Based Design; Nonlinear flight control; 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):

Tran, T. T. (2016). Nonlinear Flight Control Design Using Backstepping Methodology. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16

Chicago Manual of Style (16th Edition):

Tran, Thanh Trung. “Nonlinear Flight Control Design Using Backstepping Methodology.” 2016. Doctoral Dissertation, Old Dominion University. Accessed December 13, 2019. 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16.

MLA Handbook (7th Edition):

Tran, Thanh Trung. “Nonlinear Flight Control Design Using Backstepping Methodology.” 2016. Web. 13 Dec 2019.

Vancouver:

Tran TT. Nonlinear Flight Control Design Using Backstepping Methodology. [Internet] [Doctoral dissertation]. Old Dominion University; 2016. [cited 2019 Dec 13]. Available from: 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16.

Council of Science Editors:

Tran TT. Nonlinear Flight Control Design Using Backstepping Methodology. [Doctoral Dissertation]. Old Dominion University; 2016. Available from: 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16


Embry-Riddle Aeronautical University

14. Hervás, Jaime Rubio. Dynamics and Control of Higher-order Nonholonomic Systems.

Degree: PhD, Doctoral Studies, 2013, Embry-Riddle Aeronautical University

  A theoretical framework is established for the control of higher-order nonholonomic systems, defined as systems that satisfy higher-order nonintegrable constraints. A model for such… (more)

Subjects/Keywords: Aerospace Engineering; Navigation, Guidance, Control and Dynamics; Robotics

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APA (6th Edition):

Hervás, J. R. (2013). Dynamics and Control of Higher-order Nonholonomic Systems. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from http://commons.erau.edu/edt/154

Chicago Manual of Style (16th Edition):

Hervás, Jaime Rubio. “Dynamics and Control of Higher-order Nonholonomic Systems.” 2013. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed December 13, 2019. http://commons.erau.edu/edt/154.

MLA Handbook (7th Edition):

Hervás, Jaime Rubio. “Dynamics and Control of Higher-order Nonholonomic Systems.” 2013. Web. 13 Dec 2019.

Vancouver:

Hervás JR. Dynamics and Control of Higher-order Nonholonomic Systems. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2013. [cited 2019 Dec 13]. Available from: http://commons.erau.edu/edt/154.

Council of Science Editors:

Hervás JR. Dynamics and Control of Higher-order Nonholonomic Systems. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2013. Available from: http://commons.erau.edu/edt/154


Iowa State University

15. Rademacher, Branden James. In-flight trajectory planning and guidance for autonomous parafoils.

Degree: 2009, Iowa State University

 We present a framework for on-board trajectory planning and guidance for a large class of autonomously guided parafoils. The problem is for the parafoil to… (more)

Subjects/Keywords: control; guidance; navigation; parafoil; planning; trajectory; Aerospace Engineering

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APA (6th Edition):

Rademacher, B. J. (2009). In-flight trajectory planning and guidance for autonomous parafoils. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/10597

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):

Rademacher, Branden James. “In-flight trajectory planning and guidance for autonomous parafoils.” 2009. Thesis, Iowa State University. Accessed December 13, 2019. https://lib.dr.iastate.edu/etd/10597.

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

MLA Handbook (7th Edition):

Rademacher, Branden James. “In-flight trajectory planning and guidance for autonomous parafoils.” 2009. Web. 13 Dec 2019.

Vancouver:

Rademacher BJ. In-flight trajectory planning and guidance for autonomous parafoils. [Internet] [Thesis]. Iowa State University; 2009. [cited 2019 Dec 13]. Available from: https://lib.dr.iastate.edu/etd/10597.

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

Council of Science Editors:

Rademacher BJ. In-flight trajectory planning and guidance for autonomous parafoils. [Thesis]. Iowa State University; 2009. Available from: https://lib.dr.iastate.edu/etd/10597

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


University of Michigan

16. Walsh, Alex. Extremum-Seeking Guidance and Conic-Sector-Based Control of Aerospace Systems.

Degree: PhD, Aerospace Engineering, 2017, University of Michigan

 This dissertation studies guidance and control of aerospace systems. Guidance algorithms are used to determine desired trajectories of systems, and in particular, this dissertation examines… (more)

Subjects/Keywords: extremum-seeking guidance; control; conic sector; Aerospace Engineering; Engineering

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APA (6th Edition):

Walsh, A. (2017). Extremum-Seeking Guidance and Conic-Sector-Based Control of Aerospace Systems. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/143993

Chicago Manual of Style (16th Edition):

Walsh, Alex. “Extremum-Seeking Guidance and Conic-Sector-Based Control of Aerospace Systems.” 2017. Doctoral Dissertation, University of Michigan. Accessed December 13, 2019. http://hdl.handle.net/2027.42/143993.

MLA Handbook (7th Edition):

Walsh, Alex. “Extremum-Seeking Guidance and Conic-Sector-Based Control of Aerospace Systems.” 2017. Web. 13 Dec 2019.

Vancouver:

Walsh A. Extremum-Seeking Guidance and Conic-Sector-Based Control of Aerospace Systems. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2019 Dec 13]. Available from: http://hdl.handle.net/2027.42/143993.

Council of Science Editors:

Walsh A. Extremum-Seeking Guidance and Conic-Sector-Based Control of Aerospace Systems. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/143993


Ryerson University

17. 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 (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 December 13, 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. 13 Dec 2019.

Vancouver:

Wong FYW. Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point. [Internet] [Thesis]. Ryerson University; 2009. [cited 2019 Dec 13]. 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


University of Washington

18. Szmuk, Michael. Successive Convexification & High Performance Feedback Control for Agile Flight.

Degree: PhD, 2019, University of Washington

 The topic of this dissertation is successive convexification and high performance feedback control for agile flight. This document is divided into three primary branches. The… (more)

Subjects/Keywords: Autonomy; Control; Feedback control; Guidance; Multi-Rotors; Trajectory optimization; Aerospace engineering; Aeronautics and astronautics

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APA (6th Edition):

Szmuk, M. (2019). Successive Convexification & High Performance Feedback Control for Agile Flight. (Doctoral Dissertation). University of Washington. Retrieved from http://hdl.handle.net/1773/44017

Chicago Manual of Style (16th Edition):

Szmuk, Michael. “Successive Convexification & High Performance Feedback Control for Agile Flight.” 2019. Doctoral Dissertation, University of Washington. Accessed December 13, 2019. http://hdl.handle.net/1773/44017.

MLA Handbook (7th Edition):

Szmuk, Michael. “Successive Convexification & High Performance Feedback Control for Agile Flight.” 2019. Web. 13 Dec 2019.

Vancouver:

Szmuk M. Successive Convexification & High Performance Feedback Control for Agile Flight. [Internet] [Doctoral dissertation]. University of Washington; 2019. [cited 2019 Dec 13]. Available from: http://hdl.handle.net/1773/44017.

Council of Science Editors:

Szmuk M. Successive Convexification & High Performance Feedback Control for Agile Flight. [Doctoral Dissertation]. University of Washington; 2019. Available from: http://hdl.handle.net/1773/44017


Cal Poly

19. Villa, Andres Eduardo. Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  Due to mass and volume constraints on planetary missions, the development of control techniques that do not require fuel are of big interest. For… (more)

Subjects/Keywords: Mars; Formation Flying; Proximity Operations; Differential Drag; Lyapunov; Control Theory; Guidance; Navigation; Perturbations; Aerospace Engineering; Astrodynamics; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Villa, A. E. (2016). Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1571 ; 10.15368/theses.2016.48

Chicago Manual of Style (16th Edition):

Villa, Andres Eduardo. “Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere.” 2016. Masters Thesis, Cal Poly. Accessed December 13, 2019. https://digitalcommons.calpoly.edu/theses/1571 ; 10.15368/theses.2016.48.

MLA Handbook (7th Edition):

Villa, Andres Eduardo. “Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere.” 2016. Web. 13 Dec 2019.

Vancouver:

Villa AE. Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2019 Dec 13]. Available from: https://digitalcommons.calpoly.edu/theses/1571 ; 10.15368/theses.2016.48.

Council of Science Editors:

Villa AE. Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1571 ; 10.15368/theses.2016.48


Cranfield University

20. Bilale, Abudureheman. State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles.

Degree: 2018, Cranfield University

 Path-following is a primary task for most marine, air or space crafts, especially during autonomous operations. Research on autonomous underwater vehicles (AUV) has received large… (more)

Subjects/Keywords: line-of-sight guidance; path-following control; Guidance systems; underwater vehicles; kinematics; dynamics and modelling; marine systems; ocean currents

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APA (6th Edition):

Bilale, A. (2018). State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles. (Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/13963

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):

Bilale, Abudureheman. “State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles.” 2018. Thesis, Cranfield University. Accessed December 13, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/13963.

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

MLA Handbook (7th Edition):

Bilale, Abudureheman. “State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles.” 2018. Web. 13 Dec 2019.

Vancouver:

Bilale A. State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles. [Internet] [Thesis]. Cranfield University; 2018. [cited 2019 Dec 13]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/13963.

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

Council of Science Editors:

Bilale A. State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles. [Thesis]. Cranfield University; 2018. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/13963

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


Cranfield University

21. Bilale, Abudureheman. State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles.

Degree: PhD, 2018, Cranfield University

 Path-following is a primary task for most marine, air or space crafts, especially during autonomous operations. Research on autonomous underwater vehicles (AUV) has received large… (more)

Subjects/Keywords: line-of-sight guidance; path-following control; Guidance systems; underwater vehicles; kinematics; dynamics and modelling; marine systems; ocean currents

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APA (6th Edition):

Bilale, A. (2018). State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/13963 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.768185

Chicago Manual of Style (16th Edition):

Bilale, Abudureheman. “State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles.” 2018. Doctoral Dissertation, Cranfield University. Accessed December 13, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/13963 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.768185.

MLA Handbook (7th Edition):

Bilale, Abudureheman. “State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles.” 2018. Web. 13 Dec 2019.

Vancouver:

Bilale A. State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles. [Internet] [Doctoral dissertation]. Cranfield University; 2018. [cited 2019 Dec 13]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/13963 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.768185.

Council of Science Editors:

Bilale A. State relativity and speed-allocated line-of-sight course control for path-following of underwater vehicles. [Doctoral Dissertation]. Cranfield University; 2018. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/13963 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.768185


University of Colorado

22. Leonard, Jason Michael. Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.

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

  Crewed navigation in certain regions of the Earth-Moon system provides a unique challenge due to the unstable dynamics and observation geometry relative to standard… (more)

Subjects/Keywords: Autonomous Navigation; Navigation; Orbit Determination; Stochastic Processes; Navigation, Guidance, Control and Dynamics; Space Vehicles

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APA (6th Edition):

Leonard, J. M. (2015). Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/97

Chicago Manual of Style (16th Edition):

Leonard, Jason Michael. “Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.” 2015. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/97.

MLA Handbook (7th Edition):

Leonard, Jason Michael. “Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.” 2015. Web. 13 Dec 2019.

Vancouver:

Leonard JM. Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/97.

Council of Science Editors:

Leonard JM. Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System. [Doctoral Dissertation]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/97


University of Toronto

23. Lau, George Tin Lam. Path Planning Algorithms for Autonomous Border Patrol Vehicles.

Degree: 2012, University of Toronto

This thesis presents an online path planning algorithm developed for unmanned vehicles in charge of autonomous border patrol. In this Pursuit-Evasion game, the unmanned vehicle… (more)

Subjects/Keywords: autonomous vehicles; guidance; path planning; border patrol; Pursuit-Evasion; optimal control; 0538

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APA (6th Edition):

Lau, G. T. L. (2012). Path Planning Algorithms for Autonomous Border Patrol Vehicles. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/33303

Chicago Manual of Style (16th Edition):

Lau, George Tin Lam. “Path Planning Algorithms for Autonomous Border Patrol Vehicles.” 2012. Masters Thesis, University of Toronto. Accessed December 13, 2019. http://hdl.handle.net/1807/33303.

MLA Handbook (7th Edition):

Lau, George Tin Lam. “Path Planning Algorithms for Autonomous Border Patrol Vehicles.” 2012. Web. 13 Dec 2019.

Vancouver:

Lau GTL. Path Planning Algorithms for Autonomous Border Patrol Vehicles. [Internet] [Masters thesis]. University of Toronto; 2012. [cited 2019 Dec 13]. Available from: http://hdl.handle.net/1807/33303.

Council of Science Editors:

Lau GTL. Path Planning Algorithms for Autonomous Border Patrol Vehicles. [Masters Thesis]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/33303


University of Colorado

24. 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 December 13, 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. 13 Dec 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 Dec 13]. 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


Cal Poly

25. Downs, Matthew C. Adaptive Control Applied to the Cal Poly Spacecraft Attitude Dynamics Simulator.

Degree: MS, Aerospace Engineering, 2010, Cal Poly

 The goal of this thesis is to use the Cal Poly Spacecraft Attitude Dynamics Simulator to provide proof of concept of two adaptive control theories… (more)

Subjects/Keywords: Reaction Wheel Pyramid; Adaptive Control; PRWP; Spacecraft; Spacecraft Control; Acoustics, Dynamics, and Controls; Astrodynamics; Navigation, Guidance, Control and Dynamics; Space Vehicles

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APA (6th Edition):

Downs, M. C. (2010). Adaptive Control Applied to the Cal Poly Spacecraft Attitude Dynamics Simulator. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/231 ; 10.15368/theses.2010.6

Chicago Manual of Style (16th Edition):

Downs, Matthew C. “Adaptive Control Applied to the Cal Poly Spacecraft Attitude Dynamics Simulator.” 2010. Masters Thesis, Cal Poly. Accessed December 13, 2019. https://digitalcommons.calpoly.edu/theses/231 ; 10.15368/theses.2010.6.

MLA Handbook (7th Edition):

Downs, Matthew C. “Adaptive Control Applied to the Cal Poly Spacecraft Attitude Dynamics Simulator.” 2010. Web. 13 Dec 2019.

Vancouver:

Downs MC. Adaptive Control Applied to the Cal Poly Spacecraft Attitude Dynamics Simulator. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2019 Dec 13]. Available from: https://digitalcommons.calpoly.edu/theses/231 ; 10.15368/theses.2010.6.

Council of Science Editors:

Downs MC. Adaptive Control Applied to the Cal Poly Spacecraft Attitude Dynamics Simulator. [Masters Thesis]. Cal Poly; 2010. Available from: https://digitalcommons.calpoly.edu/theses/231 ; 10.15368/theses.2010.6


Portland State University

26. Podhradský, Michal. A Multi-Agent System for Adaptive Control of a Flapping-Wing Micro Air Vehicle.

Degree: PhD, Electrical and Computer Engineering, 2016, Portland State University

  Biomimetic flapping-wing vehicles have attracted recent interest because of their numerous potential military and civilian applications. In this dissertation is described the design of… (more)

Subjects/Keywords: Micro air vehicles  – Control systems  – Design; Multiagent systems; Micro air vehicles  – Automatic control; Adaptive control systems; Electrical and Computer Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Podhradský, M. (2016). A Multi-Agent System for Adaptive Control of a Flapping-Wing Micro Air Vehicle. (Doctoral Dissertation). Portland State University. Retrieved from https://pdxscholar.library.pdx.edu/open_access_etds/3291

Chicago Manual of Style (16th Edition):

Podhradský, Michal. “A Multi-Agent System for Adaptive Control of a Flapping-Wing Micro Air Vehicle.” 2016. Doctoral Dissertation, Portland State University. Accessed December 13, 2019. https://pdxscholar.library.pdx.edu/open_access_etds/3291.

MLA Handbook (7th Edition):

Podhradský, Michal. “A Multi-Agent System for Adaptive Control of a Flapping-Wing Micro Air Vehicle.” 2016. Web. 13 Dec 2019.

Vancouver:

Podhradský M. A Multi-Agent System for Adaptive Control of a Flapping-Wing Micro Air Vehicle. [Internet] [Doctoral dissertation]. Portland State University; 2016. [cited 2019 Dec 13]. Available from: https://pdxscholar.library.pdx.edu/open_access_etds/3291.

Council of Science Editors:

Podhradský M. A Multi-Agent System for Adaptive Control of a Flapping-Wing Micro Air Vehicle. [Doctoral Dissertation]. Portland State University; 2016. Available from: https://pdxscholar.library.pdx.edu/open_access_etds/3291


University of Colorado

27. Shupe, Nathan C. Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object.

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

  Based on the recommendations of the Augustine Commission, President Obama has proposed a vision for U.S. human spaceflight in the post-Shuttle era which includes… (more)

Subjects/Keywords: Human Exploration; Near Earth Object; Orbits; Orion; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Shupe, N. C. (2010). Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/7

Chicago Manual of Style (16th Edition):

Shupe, Nathan C. “Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object.” 2010. Masters Thesis, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/7.

MLA Handbook (7th Edition):

Shupe, Nathan C. “Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object.” 2010. Web. 13 Dec 2019.

Vancouver:

Shupe NC. Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object. [Internet] [Masters thesis]. University of Colorado; 2010. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/7.

Council of Science Editors:

Shupe NC. Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object. [Masters Thesis]. University of Colorado; 2010. Available from: http://scholar.colorado.edu/asen_gradetds/7


University of Colorado

28. Takahashi, Yu. Gravity Field Characterization around Small Bodies.

Degree: PhD, Aerospace Engineering Sciences, 2013, University of Colorado

  A small body rendezvous mission requires accurate gravity field characterization for safe, accurate navigation purposes. However, the current techniques of gravity field modeling around… (more)

Subjects/Keywords: Asteroids; Comets; Gravity Field; Small Body; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Takahashi, Y. (2013). Gravity Field Characterization around Small Bodies. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/70

Chicago Manual of Style (16th Edition):

Takahashi, Yu. “Gravity Field Characterization around Small Bodies.” 2013. Doctoral Dissertation, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/70.

MLA Handbook (7th Edition):

Takahashi, Yu. “Gravity Field Characterization around Small Bodies.” 2013. Web. 13 Dec 2019.

Vancouver:

Takahashi Y. Gravity Field Characterization around Small Bodies. [Internet] [Doctoral dissertation]. University of Colorado; 2013. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/70.

Council of Science Editors:

Takahashi Y. Gravity Field Characterization around Small Bodies. [Doctoral Dissertation]. University of Colorado; 2013. Available from: http://scholar.colorado.edu/asen_gradetds/70


University of Colorado

29. 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 December 13, 2019. http://scholar.colorado.edu/asen_gradetds/78.

MLA Handbook (7th Edition):

Gerhardt, David Thomas. “Small Satellite Passive Magnetic Attitude Control.” 2014. Web. 13 Dec 2019.

Vancouver:

Gerhardt DT. Small Satellite Passive Magnetic Attitude Control. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2019 Dec 13]. 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


University of Colorado

30. Smith, Sarah Mitchell. Proximal Blade Twist Feedback Control for Heliogyro Solar Sails.

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

  A heliogyro spacecraft is a specific type of solar sail that generates thrust from the reflection of solar photons. It consists of multiple long… (more)

Subjects/Keywords: solar sailing; space; Aerospace Engineering; Navigation, Guidance, Control and Dynamics; Structures and Materials

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

APA (6th Edition):

Smith, S. M. (2015). Proximal Blade Twist Feedback Control for Heliogyro Solar Sails. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/108

Chicago Manual of Style (16th Edition):

Smith, Sarah Mitchell. “Proximal Blade Twist Feedback Control for Heliogyro Solar Sails.” 2015. Masters Thesis, University of Colorado. Accessed December 13, 2019. http://scholar.colorado.edu/asen_gradetds/108.

MLA Handbook (7th Edition):

Smith, Sarah Mitchell. “Proximal Blade Twist Feedback Control for Heliogyro Solar Sails.” 2015. Web. 13 Dec 2019.

Vancouver:

Smith SM. Proximal Blade Twist Feedback Control for Heliogyro Solar Sails. [Internet] [Masters thesis]. University of Colorado; 2015. [cited 2019 Dec 13]. Available from: http://scholar.colorado.edu/asen_gradetds/108.

Council of Science Editors:

Smith SM. Proximal Blade Twist Feedback Control for Heliogyro Solar Sails. [Masters Thesis]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/108

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