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You searched for +publisher:"Virginia Tech" +contributor:("Sultan, Cornel"). Showing records 1 – 30 of 36 total matches.

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Virginia Tech

1. Stiltner, Brandon Chase. Macro Fiber Composite Actuated Control Surfaces with Applications Toward Ducted Fan Vehicles.

Degree: MS, Aerospace and Ocean Engineering, 2011, Virginia Tech

 In most man-made flight, vehicle control is achieved by deflecting flaps. However, in nature, morphing surfaces are found on both flying and swimming creatures. Morphing… (more)

Subjects/Keywords: PZT; morphing control surfaces; UAVs; ducted fan; MAVs; macro fiber composite; piezoelectric

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APA (6th Edition):

Stiltner, B. C. (2011). Macro Fiber Composite Actuated Control Surfaces with Applications Toward Ducted Fan Vehicles. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34441

Chicago Manual of Style (16th Edition):

Stiltner, Brandon Chase. “Macro Fiber Composite Actuated Control Surfaces with Applications Toward Ducted Fan Vehicles.” 2011. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/34441.

MLA Handbook (7th Edition):

Stiltner, Brandon Chase. “Macro Fiber Composite Actuated Control Surfaces with Applications Toward Ducted Fan Vehicles.” 2011. Web. 30 Sep 2020.

Vancouver:

Stiltner BC. Macro Fiber Composite Actuated Control Surfaces with Applications Toward Ducted Fan Vehicles. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/34441.

Council of Science Editors:

Stiltner BC. Macro Fiber Composite Actuated Control Surfaces with Applications Toward Ducted Fan Vehicles. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/34441


Virginia Tech

2. Keil, Elizabeth Marie. Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit.

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

 This thesis details the development and implementation of an attitude and orbit determining Kalman filter algorithm for a satellite in a Molniya orbit. To apply… (more)

Subjects/Keywords: Attitude; Orbit; Determination; Kalman Filter

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APA (6th Edition):

Keil, E. M. (2014). Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49102

Chicago Manual of Style (16th Edition):

Keil, Elizabeth Marie. “Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit.” 2014. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/49102.

MLA Handbook (7th Edition):

Keil, Elizabeth Marie. “Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit.” 2014. Web. 30 Sep 2020.

Vancouver:

Keil EM. Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/49102.

Council of Science Editors:

Keil EM. Kalman Filter Implementation to Determine Orbit and Attitude of a Satellite in a Molniya Orbit. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/49102


Virginia Tech

3. Ojeda Romero, Juan Andre. Dual Satellite Coverage using Particle Swarm Optimization.

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

 A dual satellite system in a Low Earth Orbit, LEO, would be beneficial to study the electromagnetic occurrences in the magnetosphere and their contributions to… (more)

Subjects/Keywords: particle swarm optimization; space weather; aurora borealis; orbital mechanics; satellite coverage

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APA (6th Edition):

Ojeda Romero, J. A. (2014). Dual Satellite Coverage using Particle Swarm Optimization. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50627

Chicago Manual of Style (16th Edition):

Ojeda Romero, Juan Andre. “Dual Satellite Coverage using Particle Swarm Optimization.” 2014. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/50627.

MLA Handbook (7th Edition):

Ojeda Romero, Juan Andre. “Dual Satellite Coverage using Particle Swarm Optimization.” 2014. Web. 30 Sep 2020.

Vancouver:

Ojeda Romero JA. Dual Satellite Coverage using Particle Swarm Optimization. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/50627.

Council of Science Editors:

Ojeda Romero JA. Dual Satellite Coverage using Particle Swarm Optimization. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/50627


Virginia Tech

4. Guthrie, Kyle Thomas. Linear Parameter Varying Path Following Control of a Small Fixed Wing Unmanned Aerial Vehicle.

Degree: MS, Aerospace and Ocean Engineering, 2013, Virginia Tech

 A mathematical model of a small fixed-wing aircraft was developed through application of parameter estimation techniques to simulated flight test data. Multiple controllers were devised… (more)

Subjects/Keywords: path following; LPV control; robust control; unmanned aerial vehicles

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APA (6th Edition):

Guthrie, K. T. (2013). Linear Parameter Varying Path Following Control of a Small Fixed Wing Unmanned Aerial Vehicle. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23740

Chicago Manual of Style (16th Edition):

Guthrie, Kyle Thomas. “Linear Parameter Varying Path Following Control of a Small Fixed Wing Unmanned Aerial Vehicle.” 2013. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/23740.

MLA Handbook (7th Edition):

Guthrie, Kyle Thomas. “Linear Parameter Varying Path Following Control of a Small Fixed Wing Unmanned Aerial Vehicle.” 2013. Web. 30 Sep 2020.

Vancouver:

Guthrie KT. Linear Parameter Varying Path Following Control of a Small Fixed Wing Unmanned Aerial Vehicle. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/23740.

Council of Science Editors:

Guthrie KT. Linear Parameter Varying Path Following Control of a Small Fixed Wing Unmanned Aerial Vehicle. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23740


Virginia Tech

5. Singh, Raymond Charan. Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling.

Degree: MS, Aerospace Engineering, 2012, Virginia Tech

 Given the ever-growing need for device autonomy and renewable sources of energy, energy harvesting has become an increasingly popular field of research. This research focuses… (more)

Subjects/Keywords: Piezoelectric; Energy Harvesting; Computational Methods; Membranes

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APA (6th Edition):

Singh, R. C. (2012). Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76793

Chicago Manual of Style (16th Edition):

Singh, Raymond Charan. “Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling.” 2012. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/76793.

MLA Handbook (7th Edition):

Singh, Raymond Charan. “Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling.” 2012. Web. 30 Sep 2020.

Vancouver:

Singh RC. Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/76793.

Council of Science Editors:

Singh RC. Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/76793


Virginia Tech

6. Sudalagunta, Praneeth Reddy. Control-oriented Modeling of an Air-breathing Hypersonic Vehicle.

Degree: PhD, Aerospace and Ocean Engineering, 2016, Virginia Tech

 Design and development of future high speed aircraft require the use of advanced modeling tools early on in the design phase to study and analyze… (more)

Subjects/Keywords: Control-oriented Modeling; Aeroelasticity; Air-breathing Hypersonic Vehicles

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APA (6th Edition):

Sudalagunta, P. R. (2016). Control-oriented Modeling of an Air-breathing Hypersonic Vehicle. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/72872

Chicago Manual of Style (16th Edition):

Sudalagunta, Praneeth Reddy. “Control-oriented Modeling of an Air-breathing Hypersonic Vehicle.” 2016. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/72872.

MLA Handbook (7th Edition):

Sudalagunta, Praneeth Reddy. “Control-oriented Modeling of an Air-breathing Hypersonic Vehicle.” 2016. Web. 30 Sep 2020.

Vancouver:

Sudalagunta PR. Control-oriented Modeling of an Air-breathing Hypersonic Vehicle. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/72872.

Council of Science Editors:

Sudalagunta PR. Control-oriented Modeling of an Air-breathing Hypersonic Vehicle. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/72872


Virginia Tech

7. Morris, Craig C. Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization.

Degree: PhD, Aerospace Engineering, 2014, Virginia Tech

 This work details the development of a stability and control module for implementation into a Multidisciplinary Design Optimization (MDO) framework for the conceptual design of… (more)

Subjects/Keywords: MDO; Dynamic Performance; Stability and Control; Linear Matrix Inequalities

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APA (6th Edition):

Morris, C. C. (2014). Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/25787

Chicago Manual of Style (16th Edition):

Morris, Craig C. “Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization.” 2014. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/25787.

MLA Handbook (7th Edition):

Morris, Craig C. “Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization.” 2014. Web. 30 Sep 2020.

Vancouver:

Morris CC. Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/25787.

Council of Science Editors:

Morris CC. Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/25787


Virginia Tech

8. Towler, Jerry Alwynne. Autonomous Aerial Localization of Radioactive Point Sources via Recursive Bayesian Estimation and Contour Analysis.

Degree: MS, Electrical and Computer Engineering, 2011, Virginia Tech

 The rapid, accurate determination of the positions and strengths of sources of dangerous radioactivity takes high priority after a catastrophic event to ensure the safety… (more)

Subjects/Keywords: unmanned aerial vehicle; UAV; unmanned systems; contour following; source localization

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APA (6th Edition):

Towler, J. A. (2011). Autonomous Aerial Localization of Radioactive Point Sources via Recursive Bayesian Estimation and Contour Analysis. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/43465

Chicago Manual of Style (16th Edition):

Towler, Jerry Alwynne. “Autonomous Aerial Localization of Radioactive Point Sources via Recursive Bayesian Estimation and Contour Analysis.” 2011. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/43465.

MLA Handbook (7th Edition):

Towler, Jerry Alwynne. “Autonomous Aerial Localization of Radioactive Point Sources via Recursive Bayesian Estimation and Contour Analysis.” 2011. Web. 30 Sep 2020.

Vancouver:

Towler JA. Autonomous Aerial Localization of Radioactive Point Sources via Recursive Bayesian Estimation and Contour Analysis. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/43465.

Council of Science Editors:

Towler JA. Autonomous Aerial Localization of Radioactive Point Sources via Recursive Bayesian Estimation and Contour Analysis. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/43465


Virginia Tech

9. Wolosik, Anthony Thomas. Advancements in the Design and Development of CubeSat Attitude Determination and Control Testing at the Virginia Tech Space Systems Simulation Laboratory.

Degree: MS, Aerospace and Ocean Engineering, 2018, Virginia Tech

 Among the various challenges involved in the development of CubeSats lies the attitude determination and control of the satellite. The importance of a properly functioning… (more)

Subjects/Keywords: CubeSat; Attitude Control; Air Bearing; Reaction Wheel Array; Helmholtz Cage

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APA (6th Edition):

Wolosik, A. T. (2018). Advancements in the Design and Development of CubeSat Attitude Determination and Control Testing at the Virginia Tech Space Systems Simulation Laboratory. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/84980

Chicago Manual of Style (16th Edition):

Wolosik, Anthony Thomas. “Advancements in the Design and Development of CubeSat Attitude Determination and Control Testing at the Virginia Tech Space Systems Simulation Laboratory.” 2018. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/84980.

MLA Handbook (7th Edition):

Wolosik, Anthony Thomas. “Advancements in the Design and Development of CubeSat Attitude Determination and Control Testing at the Virginia Tech Space Systems Simulation Laboratory.” 2018. Web. 30 Sep 2020.

Vancouver:

Wolosik AT. Advancements in the Design and Development of CubeSat Attitude Determination and Control Testing at the Virginia Tech Space Systems Simulation Laboratory. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/84980.

Council of Science Editors:

Wolosik AT. Advancements in the Design and Development of CubeSat Attitude Determination and Control Testing at the Virginia Tech Space Systems Simulation Laboratory. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/84980


Virginia Tech

10. Brown, Gavin Miles. Designing Transfers Between Earth-Moon Halo Orbits Using Manifolds and Optimization.

Degree: MS, Aerospace Engineering, 2020, Virginia Tech

 Being able to identify fuel efficient transfers between orbits is critical to planning and executing missions involving spacecraft. With a renewed focus on lunar missions,… (more)

Subjects/Keywords: Transfers; Manifolds; Optimization; Halo Orbits; CR3BP

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APA (6th Edition):

Brown, G. M. (2020). Designing Transfers Between Earth-Moon Halo Orbits Using Manifolds and Optimization. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/99901

Chicago Manual of Style (16th Edition):

Brown, Gavin Miles. “Designing Transfers Between Earth-Moon Halo Orbits Using Manifolds and Optimization.” 2020. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/99901.

MLA Handbook (7th Edition):

Brown, Gavin Miles. “Designing Transfers Between Earth-Moon Halo Orbits Using Manifolds and Optimization.” 2020. Web. 30 Sep 2020.

Vancouver:

Brown GM. Designing Transfers Between Earth-Moon Halo Orbits Using Manifolds and Optimization. [Internet] [Masters thesis]. Virginia Tech; 2020. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/99901.

Council of Science Editors:

Brown GM. Designing Transfers Between Earth-Moon Halo Orbits Using Manifolds and Optimization. [Masters Thesis]. Virginia Tech; 2020. Available from: http://hdl.handle.net/10919/99901

11. Agarwal, Divyanshu. A Study on the Feasibility of Using Fractional Differential Equations for Roll Damping Models.

Degree: MS, Aerospace and Ocean Engineering, 2015, Virginia Tech

 An optimization algorithm has been developed to study the effectiveness of substituting time tested ODEs with FDEs as applied to ship motions, specifically with an… (more)

Subjects/Keywords: Fractional Differential Equation; Damping; Roll; Pitch

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APA (6th Edition):

Agarwal, D. (2015). A Study on the Feasibility of Using Fractional Differential Equations for Roll Damping Models. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/52959

Chicago Manual of Style (16th Edition):

Agarwal, Divyanshu. “A Study on the Feasibility of Using Fractional Differential Equations for Roll Damping Models.” 2015. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/52959.

MLA Handbook (7th Edition):

Agarwal, Divyanshu. “A Study on the Feasibility of Using Fractional Differential Equations for Roll Damping Models.” 2015. Web. 30 Sep 2020.

Vancouver:

Agarwal D. A Study on the Feasibility of Using Fractional Differential Equations for Roll Damping Models. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/52959.

Council of Science Editors:

Agarwal D. A Study on the Feasibility of Using Fractional Differential Equations for Roll Damping Models. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/52959


Virginia Tech

12. Gonzalez-Rocha, Javier. Sensing Atmospheric Winds from Quadrotor Motion.

Degree: PhD, Aerospace Engineering, 2020, Virginia Tech

 Wind observations that are critical for understanding meteorological processes occurring inside of the Earth's atmospheric boundary layer (ABL) are sparse due to limitations of conventional… (more)

Subjects/Keywords: Unmanned Aircraft Systems; State Estimation; System Identification

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APA (6th Edition):

Gonzalez-Rocha, J. (2020). Sensing Atmospheric Winds from Quadrotor Motion. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/98657

Chicago Manual of Style (16th Edition):

Gonzalez-Rocha, Javier. “Sensing Atmospheric Winds from Quadrotor Motion.” 2020. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/98657.

MLA Handbook (7th Edition):

Gonzalez-Rocha, Javier. “Sensing Atmospheric Winds from Quadrotor Motion.” 2020. Web. 30 Sep 2020.

Vancouver:

Gonzalez-Rocha J. Sensing Atmospheric Winds from Quadrotor Motion. [Internet] [Doctoral dissertation]. Virginia Tech; 2020. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/98657.

Council of Science Editors:

Gonzalez-Rocha J. Sensing Atmospheric Winds from Quadrotor Motion. [Doctoral Dissertation]. Virginia Tech; 2020. Available from: http://hdl.handle.net/10919/98657


Virginia Tech

13. 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 September 30, 2020. 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. 30 Sep 2020.

Vancouver:

Atkins BM. Mars Precision Entry Vehicle Guidance Using Internal Moving Mass Actuators. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2020 Sep 30]. 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


Virginia Tech

14. Lei, Yu. Functional Regression and Adaptive Control.

Degree: PhD, Aerospace and Ocean Engineering, 2012, Virginia Tech

 The author proposes a novel functional regression method for parameter estimation and adaptive control in this dissertation. In the functional regression method, the regressors and… (more)

Subjects/Keywords: Functional Regression; Persistent Excitation; Adaptive Control; Nonlinear Systems; Parameter Estimation; System Identification

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APA (6th Edition):

Lei, Y. (2012). Functional Regression and Adaptive Control. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/29113

Chicago Manual of Style (16th Edition):

Lei, Yu. “Functional Regression and Adaptive Control.” 2012. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/29113.

MLA Handbook (7th Edition):

Lei, Yu. “Functional Regression and Adaptive Control.” 2012. Web. 30 Sep 2020.

Vancouver:

Lei Y. Functional Regression and Adaptive Control. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/29113.

Council of Science Editors:

Lei Y. Functional Regression and Adaptive Control. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/29113


Virginia Tech

15. Kraus, Robert J. Analytical and Numerical Optimal Motion Planning for an Underwater Glider.

Degree: PhD, Aerospace and Ocean Engineering, 2010, Virginia Tech

 The use of autonomous underwater vehicles (AUVs) for oceanic observation and research is becoming more common. Underwater gliders are a specific class of AUV that… (more)

Subjects/Keywords: Underwater Glider; Singular Control; Optimal Path Generation; Optimal Control

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APA (6th Edition):

Kraus, R. J. (2010). Analytical and Numerical Optimal Motion Planning for an Underwater Glider. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77352

Chicago Manual of Style (16th Edition):

Kraus, Robert J. “Analytical and Numerical Optimal Motion Planning for an Underwater Glider.” 2010. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/77352.

MLA Handbook (7th Edition):

Kraus, Robert J. “Analytical and Numerical Optimal Motion Planning for an Underwater Glider.” 2010. Web. 30 Sep 2020.

Vancouver:

Kraus RJ. Analytical and Numerical Optimal Motion Planning for an Underwater Glider. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/77352.

Council of Science Editors:

Kraus RJ. Analytical and Numerical Optimal Motion Planning for an Underwater Glider. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/77352


Virginia Tech

16. Wagner, Katherine Mott. Optimization of Disaggregated Space Systems Using the Disaggregated Integral Systems Concept Optimization Technology Methodology.

Degree: PhD, Aerospace Engineering, 2020, Virginia Tech

 Civilians, businesses, and the government all rely on space-based resources for their daily operations. For example, the signal provided by GPS satellites is used by… (more)

Subjects/Keywords: disaggregation; constellation design; DSS; optimization

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APA (6th Edition):

Wagner, K. M. (2020). Optimization of Disaggregated Space Systems Using the Disaggregated Integral Systems Concept Optimization Technology Methodology. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/99338

Chicago Manual of Style (16th Edition):

Wagner, Katherine Mott. “Optimization of Disaggregated Space Systems Using the Disaggregated Integral Systems Concept Optimization Technology Methodology.” 2020. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/99338.

MLA Handbook (7th Edition):

Wagner, Katherine Mott. “Optimization of Disaggregated Space Systems Using the Disaggregated Integral Systems Concept Optimization Technology Methodology.” 2020. Web. 30 Sep 2020.

Vancouver:

Wagner KM. Optimization of Disaggregated Space Systems Using the Disaggregated Integral Systems Concept Optimization Technology Methodology. [Internet] [Doctoral dissertation]. Virginia Tech; 2020. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/99338.

Council of Science Editors:

Wagner KM. Optimization of Disaggregated Space Systems Using the Disaggregated Integral Systems Concept Optimization Technology Methodology. [Doctoral Dissertation]. Virginia Tech; 2020. Available from: http://hdl.handle.net/10919/99338


Virginia Tech

17. Karlgaard, Christopher David. Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit.

Degree: PhD, Aerospace and Ocean Engineering, 2010, Virginia Tech

 The development of navigation filters that make use of robust estimation techniques is important due to the sensitivity of the typical minimum L2 norm techniques,… (more)

Subjects/Keywords: Robust Estimation; Rendezvous; Adaptive Estimation

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APA (6th Edition):

Karlgaard, C. D. (2010). Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28274

Chicago Manual of Style (16th Edition):

Karlgaard, Christopher David. “Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit.” 2010. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/28274.

MLA Handbook (7th Edition):

Karlgaard, Christopher David. “Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit.” 2010. Web. 30 Sep 2020.

Vancouver:

Karlgaard CD. Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/28274.

Council of Science Editors:

Karlgaard CD. Robust Adaptive Estimation for Autonomous Rendezvous in Elliptical Orbit. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/28274


Virginia Tech

18. Shukla, Himanshu. Nonlinear Analysis and Control of Aeroelastic Systems.

Degree: PhD, Aerospace and Ocean Engineering, 2016, Virginia Tech

 Presence of nonlinearities may lead to limit cycle oscillations (LCOs) in aeroelastic systems. LCOs can result in fatigue in wings leading to catastrophic failures. Existence… (more)

Subjects/Keywords: Aeroelasticity; Control; Limit cycle oscillations; Optimization; Subcritical; Supercritical

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APA (6th Edition):

Shukla, H. (2016). Nonlinear Analysis and Control of Aeroelastic Systems. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71468

Chicago Manual of Style (16th Edition):

Shukla, Himanshu. “Nonlinear Analysis and Control of Aeroelastic Systems.” 2016. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/71468.

MLA Handbook (7th Edition):

Shukla, Himanshu. “Nonlinear Analysis and Control of Aeroelastic Systems.” 2016. Web. 30 Sep 2020.

Vancouver:

Shukla H. Nonlinear Analysis and Control of Aeroelastic Systems. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/71468.

Council of Science Editors:

Shukla H. Nonlinear Analysis and Control of Aeroelastic Systems. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71468


Virginia Tech

19. Ngo, Tri Dinh. Constrained Control for Helicopter Shipboard Operations and Moored Ocean Current Turbine Flight Control.

Degree: PhD, Aerospace and Ocean Engineering, 2016, Virginia Tech

 This dissertation focuses on constrained control of two applications: helicopter and ocean current turbines (OCT). A major contribution in the helicopter application is a novel… (more)

Subjects/Keywords: helicopter shipboard operations; ocean current turbine; model predictive control; mixed integer quadratic programming; motion planning; ouput variance constrained control

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APA (6th Edition):

Ngo, T. D. (2016). Constrained Control for Helicopter Shipboard Operations and Moored Ocean Current Turbine Flight Control. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71685

Chicago Manual of Style (16th Edition):

Ngo, Tri Dinh. “Constrained Control for Helicopter Shipboard Operations and Moored Ocean Current Turbine Flight Control.” 2016. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/71685.

MLA Handbook (7th Edition):

Ngo, Tri Dinh. “Constrained Control for Helicopter Shipboard Operations and Moored Ocean Current Turbine Flight Control.” 2016. Web. 30 Sep 2020.

Vancouver:

Ngo TD. Constrained Control for Helicopter Shipboard Operations and Moored Ocean Current Turbine Flight Control. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/71685.

Council of Science Editors:

Ngo TD. Constrained Control for Helicopter Shipboard Operations and Moored Ocean Current Turbine Flight Control. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71685


Virginia Tech

20. Oktay, Tugrul. Constrained Control of Complex Helicopter Models.

Degree: PhD, Aerospace and Ocean Engineering, 2012, Virginia Tech

 Complex helicopter models that include effects typically ignored in control models, such as an analytical formulation for fuselage aerodynamics, blade lead-lagging and flexibility, and tail… (more)

Subjects/Keywords: simultaneous design; constrained control; control oriented helicopter modeling; physics-based control

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APA (6th Edition):

Oktay, T. (2012). Constrained Control of Complex Helicopter Models. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/26619

Chicago Manual of Style (16th Edition):

Oktay, Tugrul. “Constrained Control of Complex Helicopter Models.” 2012. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/26619.

MLA Handbook (7th Edition):

Oktay, Tugrul. “Constrained Control of Complex Helicopter Models.” 2012. Web. 30 Sep 2020.

Vancouver:

Oktay T. Constrained Control of Complex Helicopter Models. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/26619.

Council of Science Editors:

Oktay T. Constrained Control of Complex Helicopter Models. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/26619


Virginia Tech

21. Ferhat, Ipar. Development and Application of Modern Optimal Controllers for a Membrane Structure Using Vector Second Order Form.

Degree: PhD, Aerospace and Ocean Engineering, 2015, Virginia Tech

 With increasing advancement in material science and computational power of current computers that allows us to analyze high dimensional systems, very light and large structures… (more)

Subjects/Keywords: Thin / membrane structures; piezoelectric actuators; smart materials; control of structures; distributed control; vector second order form.

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APA (6th Edition):

Ferhat, I. (2015). Development and Application of Modern Optimal Controllers for a Membrane Structure Using Vector Second Order Form. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/53513

Chicago Manual of Style (16th Edition):

Ferhat, Ipar. “Development and Application of Modern Optimal Controllers for a Membrane Structure Using Vector Second Order Form.” 2015. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/53513.

MLA Handbook (7th Edition):

Ferhat, Ipar. “Development and Application of Modern Optimal Controllers for a Membrane Structure Using Vector Second Order Form.” 2015. Web. 30 Sep 2020.

Vancouver:

Ferhat I. Development and Application of Modern Optimal Controllers for a Membrane Structure Using Vector Second Order Form. [Internet] [Doctoral dissertation]. Virginia Tech; 2015. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/53513.

Council of Science Editors:

Ferhat I. Development and Application of Modern Optimal Controllers for a Membrane Structure Using Vector Second Order Form. [Doctoral Dissertation]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/53513


Virginia Tech

22. Grymin, David J. Two-Step System Identification and Primitive-Based Motion Planning for Control of Small Unmanned Aerial Vehicles  .

Degree: PhD, Aerospace and Ocean Engineering, 2013, Virginia Tech

 This dissertation addresses motion planning, modeling, and feedback control for autonomous vehicle systems. A hierarchical approach for motion planning and control of nonlinear systems operating… (more)

Subjects/Keywords: Aircraft; Motion Primitives; Parameter Estimation; Path Planning; System Identification; Trajectory Generation

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APA (6th Edition):

Grymin, D. J. (2013). Two-Step System Identification and Primitive-Based Motion Planning for Control of Small Unmanned Aerial Vehicles  . (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/24520

Chicago Manual of Style (16th Edition):

Grymin, David J. “Two-Step System Identification and Primitive-Based Motion Planning for Control of Small Unmanned Aerial Vehicles  .” 2013. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/24520.

MLA Handbook (7th Edition):

Grymin, David J. “Two-Step System Identification and Primitive-Based Motion Planning for Control of Small Unmanned Aerial Vehicles  .” 2013. Web. 30 Sep 2020.

Vancouver:

Grymin DJ. Two-Step System Identification and Primitive-Based Motion Planning for Control of Small Unmanned Aerial Vehicles  . [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/24520.

Council of Science Editors:

Grymin DJ. Two-Step System Identification and Primitive-Based Motion Planning for Control of Small Unmanned Aerial Vehicles  . [Doctoral Dissertation]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/24520


Virginia Tech

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

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

 This dissertation investigates attitude transition maneuvers of a gyrosat-satellite between relative equilibria. The primary challenge in transitioning between relative equilibria is the proper adjustment of… (more)

Subjects/Keywords: Gyrostat-Satellite; Relative Equilibrium; Spacecraft Dynamics; Attitude Control; Attitude Guidance; Gravitational Torque; Attitude Maneuvers

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

VanDyke, Matthew Clark. “Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite.” 2014. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/24911.

MLA Handbook (7th Edition):

VanDyke, Matthew Clark. “Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite.” 2014. Web. 30 Sep 2020.

Vancouver:

VanDyke MC. Constant Orbital Momentum Equilibrium Trajectories of a Gyrostat-Satellite. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2020 Sep 30]. 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


Virginia Tech

24. Bean, Jacob Jon. Design and Analysis of an Active Noise Canceling Headrest.

Degree: PhD, Aerospace Engineering, 2018, Virginia Tech

 This dissertation is concerned with the active control of local sound fields, as applied to an active headrest system. Using loudspeakers and microphones, an active… (more)

Subjects/Keywords: Active headrest; active noise control; adaptive control; hybrid control; finite element modeling

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APA (6th Edition):

Bean, J. J. (2018). Design and Analysis of an Active Noise Canceling Headrest. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/94626

Chicago Manual of Style (16th Edition):

Bean, Jacob Jon. “Design and Analysis of an Active Noise Canceling Headrest.” 2018. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/94626.

MLA Handbook (7th Edition):

Bean, Jacob Jon. “Design and Analysis of an Active Noise Canceling Headrest.” 2018. Web. 30 Sep 2020.

Vancouver:

Bean JJ. Design and Analysis of an Active Noise Canceling Headrest. [Internet] [Doctoral dissertation]. Virginia Tech; 2018. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/94626.

Council of Science Editors:

Bean JJ. Design and Analysis of an Active Noise Canceling Headrest. [Doctoral Dissertation]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/94626


Virginia Tech

25. Greer, William Bryce. Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers.

Degree: PhD, Aerospace Engineering, 2019, Virginia Tech

 This dissertation proposes and, using simulation, analyzes control algorithms and their use on helicopter shipboard operations. Various benefits and advances for controls in this area… (more)

Subjects/Keywords: Helicopter; Landing; MPC; Control

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APA (6th Edition):

Greer, W. B. (2019). Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/95031

Chicago Manual of Style (16th Edition):

Greer, William Bryce. “Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers.” 2019. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/95031.

MLA Handbook (7th Edition):

Greer, William Bryce. “Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers.” 2019. Web. 30 Sep 2020.

Vancouver:

Greer WB. Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers. [Internet] [Doctoral dissertation]. Virginia Tech; 2019. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/95031.

Council of Science Editors:

Greer WB. Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers. [Doctoral Dissertation]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/95031


Virginia Tech

26. Sharma, Harsh Apurva. Structure-preserving Numerical Methods for Engineering Applications.

Degree: PhD, Aerospace Engineering, 2020, Virginia Tech

 Accurate numerical simulation of dynamical systems over long time horizons is essential in applications ranging from particle physics to geophysical fluid flow to space hazard… (more)

Subjects/Keywords: Structure-preserving methods; Geometric numerical integration; Variational integrators; Lie group methods

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APA (6th Edition):

Sharma, H. A. (2020). Structure-preserving Numerical Methods for Engineering Applications. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/99912

Chicago Manual of Style (16th Edition):

Sharma, Harsh Apurva. “Structure-preserving Numerical Methods for Engineering Applications.” 2020. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/99912.

MLA Handbook (7th Edition):

Sharma, Harsh Apurva. “Structure-preserving Numerical Methods for Engineering Applications.” 2020. Web. 30 Sep 2020.

Vancouver:

Sharma HA. Structure-preserving Numerical Methods for Engineering Applications. [Internet] [Doctoral dissertation]. Virginia Tech; 2020. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/99912.

Council of Science Editors:

Sharma HA. Structure-preserving Numerical Methods for Engineering Applications. [Doctoral Dissertation]. Virginia Tech; 2020. Available from: http://hdl.handle.net/10919/99912

27. Mcclelland, Hunter Grant. Towards Detecting Atmospheric Coherent Structures using Small Fixed-Wing Unmanned Aircraft.

Degree: PhD, Aerospace Engineering, 2019, Virginia Tech

 In a natural or man-made disaster, first responders depend on accurate predictions of where the wind might carry hazardous material. A mathematical theory of Lagrangian… (more)

Subjects/Keywords: Airborne Wind Measurement; Flight Dynamic Modeling; Unmanned Aircraft Systems; Lagrangian Coherent Structures

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APA (6th Edition):

Mcclelland, H. G. (2019). Towards Detecting Atmospheric Coherent Structures using Small Fixed-Wing Unmanned Aircraft. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/90667

Chicago Manual of Style (16th Edition):

Mcclelland, Hunter Grant. “Towards Detecting Atmospheric Coherent Structures using Small Fixed-Wing Unmanned Aircraft.” 2019. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/90667.

MLA Handbook (7th Edition):

Mcclelland, Hunter Grant. “Towards Detecting Atmospheric Coherent Structures using Small Fixed-Wing Unmanned Aircraft.” 2019. Web. 30 Sep 2020.

Vancouver:

Mcclelland HG. Towards Detecting Atmospheric Coherent Structures using Small Fixed-Wing Unmanned Aircraft. [Internet] [Doctoral dissertation]. Virginia Tech; 2019. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/90667.

Council of Science Editors:

Mcclelland HG. Towards Detecting Atmospheric Coherent Structures using Small Fixed-Wing Unmanned Aircraft. [Doctoral Dissertation]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/90667

28. Arifianto, Ony. A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation.

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

 This dissertation describes the development and modeling of a low-cost, open source, and reliable small fixed-wing unmanned aerial vehicle (UAV) for advanced control implementation. The… (more)

Subjects/Keywords: Unmanned Aerial Research Vehicles; Linear Time-Varying Control; Embedded Systems; System Identification

…performed in the Subsonic Open Jet Wind Tunnel at Virginia Tech following the procedure given in… 

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APA (6th Edition):

Arifianto, O. (2014). A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49301

Chicago Manual of Style (16th Edition):

Arifianto, Ony. “A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation.” 2014. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/49301.

MLA Handbook (7th Edition):

Arifianto, Ony. “A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation.” 2014. Web. 30 Sep 2020.

Vancouver:

Arifianto O. A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/49301.

Council of Science Editors:

Arifianto O. A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/49301

29. Yang, Shu. Modeling and Control of Tensegrity-Membrane Systems.

Degree: PhD, Aerospace and Ocean Engineering, 2016, Virginia Tech

 Tensegrity-membrane systems are a class of new bar-tendon-membrane systems. Such novel systems can be treated as extensions of tensegrity structures and are generally lightweight and… (more)

Subjects/Keywords: tensegrity-membrane systems; nonlinear finite element model; control-oriented model; nonlinear adaptive control; linear parameter-varying control

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APA (6th Edition):

Yang, S. (2016). Modeling and Control of Tensegrity-Membrane Systems. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71686

Chicago Manual of Style (16th Edition):

Yang, Shu. “Modeling and Control of Tensegrity-Membrane Systems.” 2016. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/71686.

MLA Handbook (7th Edition):

Yang, Shu. “Modeling and Control of Tensegrity-Membrane Systems.” 2016. Web. 30 Sep 2020.

Vancouver:

Yang S. Modeling and Control of Tensegrity-Membrane Systems. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/71686.

Council of Science Editors:

Yang S. Modeling and Control of Tensegrity-Membrane Systems. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71686

30. Rye, Maria del Carmen. Dynamics and Control of a Tensegrity System in Low-Earth Orbit.

Degree: PhD, Aerospace and Ocean Engineering, 2017, Virginia Tech

 Tensegrity is the name given to a system of interconnected bars and tendons that can form a flexible self-standing structure. Its flexibility is due to… (more)

Subjects/Keywords: tensegrity; spacecraft dynamics; gravity gradient

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APA (6th Edition):

Rye, M. d. C. (2017). Dynamics and Control of a Tensegrity System in Low-Earth Orbit. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77584

Chicago Manual of Style (16th Edition):

Rye, Maria del Carmen. “Dynamics and Control of a Tensegrity System in Low-Earth Orbit.” 2017. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/77584.

MLA Handbook (7th Edition):

Rye, Maria del Carmen. “Dynamics and Control of a Tensegrity System in Low-Earth Orbit.” 2017. Web. 30 Sep 2020.

Vancouver:

Rye MdC. Dynamics and Control of a Tensegrity System in Low-Earth Orbit. [Internet] [Doctoral dissertation]. Virginia Tech; 2017. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/77584.

Council of Science Editors:

Rye MdC. Dynamics and Control of a Tensegrity System in Low-Earth Orbit. [Doctoral Dissertation]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/77584

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