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You searched for +publisher:"Cal Poly" +contributor:("Eric Mehiel"). Showing records 1 – 30 of 33 total matches.

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Cal Poly

1. Chin, Alexander Wong. Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program.

Degree: MS, Aerospace Engineering, 2011, Cal Poly

  Aircraft structures have varying stiffness levels making them flexible. Consequently, this elastic property becomes increasingly important at high speeds affecting the flight dynamics of… (more)

Subjects/Keywords: aeroservoelasticity; aeroelasticity; simulation; aaw; interpolation; discretize; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Chin, A. W. (2011). Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/489 ; 10.15368/theses.2011.43

Chicago Manual of Style (16th Edition):

Chin, Alexander Wong. “Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program.” 2011. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/489 ; 10.15368/theses.2011.43.

MLA Handbook (7th Edition):

Chin, Alexander Wong. “Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program.” 2011. Web. 16 Oct 2019.

Vancouver:

Chin AW. Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program. [Internet] [Masters thesis]. Cal Poly; 2011. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/489 ; 10.15368/theses.2011.43.

Council of Science Editors:

Chin AW. Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program. [Masters Thesis]. Cal Poly; 2011. Available from: https://digitalcommons.calpoly.edu/theses/489 ; 10.15368/theses.2011.43


Cal Poly

2. 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 October 16, 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. 16 Oct 2019.

Vancouver:

Downs MC. Adaptive Control Applied to the Cal Poly Spacecraft Attitude Dynamics Simulator. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2019 Oct 16]. 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


Cal Poly

3. Coakley, Janet M. Dynamic Inversion and Backstepping Controller Robustness Analysis for a Reusable Launch Vehicle.

Degree: MS, Aerospace Engineering, 2011, Cal Poly

  The Air Force has been working towards developing technology for operationally responsive space (ORS), which is the ability to launch military assets into space… (more)

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APA (6th Edition):

Coakley, J. M. (2011). Dynamic Inversion and Backstepping Controller Robustness Analysis for a Reusable Launch Vehicle. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/471 ; 10.15368/theses.2011.26

Chicago Manual of Style (16th Edition):

Coakley, Janet M. “Dynamic Inversion and Backstepping Controller Robustness Analysis for a Reusable Launch Vehicle.” 2011. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/471 ; 10.15368/theses.2011.26.

MLA Handbook (7th Edition):

Coakley, Janet M. “Dynamic Inversion and Backstepping Controller Robustness Analysis for a Reusable Launch Vehicle.” 2011. Web. 16 Oct 2019.

Vancouver:

Coakley JM. Dynamic Inversion and Backstepping Controller Robustness Analysis for a Reusable Launch Vehicle. [Internet] [Masters thesis]. Cal Poly; 2011. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/471 ; 10.15368/theses.2011.26.

Council of Science Editors:

Coakley JM. Dynamic Inversion and Backstepping Controller Robustness Analysis for a Reusable Launch Vehicle. [Masters Thesis]. Cal Poly; 2011. Available from: https://digitalcommons.calpoly.edu/theses/471 ; 10.15368/theses.2011.26


Cal Poly

4. Silva, Seth F. Applied System Identification for a Four Wheel Reaction Wheel Platform.

Degree: MS, Aerospace Engineering, 2010, Cal Poly

 Applied System Identification for a Four Wheel Reaction Wheel Platform By Seth Franklyn Silva At the California Polytechnic State University, San Luis Obispo there is… (more)

Subjects/Keywords: System Identification; Control System; Reaction Wheel Platform; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Silva, S. F. (2010). Applied System Identification for a Four Wheel Reaction Wheel Platform. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/328 ; 10.15368/theses.2010.97

Chicago Manual of Style (16th Edition):

Silva, Seth F. “Applied System Identification for a Four Wheel Reaction Wheel Platform.” 2010. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/328 ; 10.15368/theses.2010.97.

MLA Handbook (7th Edition):

Silva, Seth F. “Applied System Identification for a Four Wheel Reaction Wheel Platform.” 2010. Web. 16 Oct 2019.

Vancouver:

Silva SF. Applied System Identification for a Four Wheel Reaction Wheel Platform. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/328 ; 10.15368/theses.2010.97.

Council of Science Editors:

Silva SF. Applied System Identification for a Four Wheel Reaction Wheel Platform. [Masters Thesis]. Cal Poly; 2010. Available from: https://digitalcommons.calpoly.edu/theses/328 ; 10.15368/theses.2010.97


Cal Poly

5. Sykes, Harrison G. COLD FLOW PERFORMANCE OF A RAMJET ENGINE.

Degree: MS, Aerospace Engineering, 2014, Cal Poly

  The design process and construction of the initial modular ramjet attachment to the Cal Poly supersonic wind tunnel is presented. The design of a… (more)

Subjects/Keywords: Propulsion; Supersonic; Ramjet; Performance; Aerodynamics and Fluid Mechanics; Propulsion and Power

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APA (6th Edition):

Sykes, H. G. (2014). COLD FLOW PERFORMANCE OF A RAMJET ENGINE. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182

Chicago Manual of Style (16th Edition):

Sykes, Harrison G. “COLD FLOW PERFORMANCE OF A RAMJET ENGINE.” 2014. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182.

MLA Handbook (7th Edition):

Sykes, Harrison G. “COLD FLOW PERFORMANCE OF A RAMJET ENGINE.” 2014. Web. 16 Oct 2019.

Vancouver:

Sykes HG. COLD FLOW PERFORMANCE OF A RAMJET ENGINE. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182.

Council of Science Editors:

Sykes HG. COLD FLOW PERFORMANCE OF A RAMJET ENGINE. [Masters Thesis]. Cal Poly; 2014. Available from: https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182


Cal Poly

6. Dam, Long H. Applied Mass Properties Identification Method to the Cal Poly's Spacecraft Simulator.

Degree: MS, Aerospace Engineering, 2014, Cal Poly

  The Cal Poly Spacecraft Simulator is currently being developed for future testing and verifying theoretical control applications. This paper details the effort to balance… (more)

Subjects/Keywords: System and Mass Properties Identification; Spacecraft Simulator; Spacecraft Control; Least Square; Batch Estimation; Navigation, Guidance, Control and Dynamics; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Dam, L. H. (2014). Applied Mass Properties Identification Method to the Cal Poly's Spacecraft Simulator. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1175 ; 10.15368/theses.2014.25

Chicago Manual of Style (16th Edition):

Dam, Long H. “Applied Mass Properties Identification Method to the Cal Poly's Spacecraft Simulator.” 2014. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1175 ; 10.15368/theses.2014.25.

MLA Handbook (7th Edition):

Dam, Long H. “Applied Mass Properties Identification Method to the Cal Poly's Spacecraft Simulator.” 2014. Web. 16 Oct 2019.

Vancouver:

Dam LH. Applied Mass Properties Identification Method to the Cal Poly's Spacecraft Simulator. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1175 ; 10.15368/theses.2014.25.

Council of Science Editors:

Dam LH. Applied Mass Properties Identification Method to the Cal Poly's Spacecraft Simulator. [Masters Thesis]. Cal Poly; 2014. Available from: https://digitalcommons.calpoly.edu/theses/1175 ; 10.15368/theses.2014.25


Cal Poly

7. Howe, William Beaman. DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES.

Degree: MS, Aerospace Engineering, 2015, Cal Poly

  A method for sizing remotely powered unmanned aerial vehicles is presented to augment the conventional design process. This method allows for unconventionally powered aircraft… (more)

Subjects/Keywords: UAV; wireless; power; design; Aeronautical Vehicles; Propulsion and Power

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APA (6th Edition):

Howe, W. B. (2015). DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1386 ; 10.15368/theses.2015.27

Chicago Manual of Style (16th Edition):

Howe, William Beaman. “DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES.” 2015. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1386 ; 10.15368/theses.2015.27.

MLA Handbook (7th Edition):

Howe, William Beaman. “DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES.” 2015. Web. 16 Oct 2019.

Vancouver:

Howe WB. DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1386 ; 10.15368/theses.2015.27.

Council of Science Editors:

Howe WB. DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES. [Masters Thesis]. Cal Poly; 2015. Available from: https://digitalcommons.calpoly.edu/theses/1386 ; 10.15368/theses.2015.27


Cal Poly

8. MacLean, Steven M. Modeling and Simulation of a Sounding Rocket Active Stabilization System.

Degree: MS, Aerospace Engineering, 2017, Cal Poly

  The Horizon Simulation Framework is a modeling and simulation framework developed to verify system level requirements. In this thesis, the framework is extended to… (more)

Subjects/Keywords: Navigation, Guidance, Control and Dynamics; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

MacLean, S. M. (2017). Modeling and Simulation of a Sounding Rocket Active Stabilization System. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1735

Chicago Manual of Style (16th Edition):

MacLean, Steven M. “Modeling and Simulation of a Sounding Rocket Active Stabilization System.” 2017. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1735.

MLA Handbook (7th Edition):

MacLean, Steven M. “Modeling and Simulation of a Sounding Rocket Active Stabilization System.” 2017. Web. 16 Oct 2019.

Vancouver:

MacLean SM. Modeling and Simulation of a Sounding Rocket Active Stabilization System. [Internet] [Masters thesis]. Cal Poly; 2017. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1735.

Council of Science Editors:

MacLean SM. Modeling and Simulation of a Sounding Rocket Active Stabilization System. [Masters Thesis]. Cal Poly; 2017. Available from: https://digitalcommons.calpoly.edu/theses/1735


Cal Poly

9. Patel, Viren Kishor. SysML Output Interface and System-Level Requirement Analyzer for the Horizon Simulation Framework.

Degree: MS, Aerospace Engineering, 2018, Cal Poly

  Model-Based Systems Engineering in industry has been constantly increasing its presence within the aerospace industry. SysML is one such MBSE tool that shows complex… (more)

Subjects/Keywords: HSF; Horizon; SysML; Translator; Requirement; Other Aerospace Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Patel, V. K. (2018). SysML Output Interface and System-Level Requirement Analyzer for the Horizon Simulation Framework. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1834

Chicago Manual of Style (16th Edition):

Patel, Viren Kishor. “SysML Output Interface and System-Level Requirement Analyzer for the Horizon Simulation Framework.” 2018. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1834.

MLA Handbook (7th Edition):

Patel, Viren Kishor. “SysML Output Interface and System-Level Requirement Analyzer for the Horizon Simulation Framework.” 2018. Web. 16 Oct 2019.

Vancouver:

Patel VK. SysML Output Interface and System-Level Requirement Analyzer for the Horizon Simulation Framework. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1834.

Council of Science Editors:

Patel VK. SysML Output Interface and System-Level Requirement Analyzer for the Horizon Simulation Framework. [Masters Thesis]. Cal Poly; 2018. Available from: https://digitalcommons.calpoly.edu/theses/1834


Cal Poly

10. Guzman, Esteban. Generating Exploration Mission-3 Trajectories to a 9:2 NRHO using Machine Learning.

Degree: MS, Aerospace Engineering, 2018, Cal Poly

  The purpose of this thesis is to design a machine learning algorithm platform that provides expanded knowledge of mission availability through a launch season… (more)

Subjects/Keywords: machine learning; nrho; space exploration; regression; k-Nearest Neighbor; Bayesian Linear; Astrodynamics; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Guzman, E. (2018). Generating Exploration Mission-3 Trajectories to a 9:2 NRHO using Machine Learning. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1953

Chicago Manual of Style (16th Edition):

Guzman, Esteban. “Generating Exploration Mission-3 Trajectories to a 9:2 NRHO using Machine Learning.” 2018. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1953.

MLA Handbook (7th Edition):

Guzman, Esteban. “Generating Exploration Mission-3 Trajectories to a 9:2 NRHO using Machine Learning.” 2018. Web. 16 Oct 2019.

Vancouver:

Guzman E. Generating Exploration Mission-3 Trajectories to a 9:2 NRHO using Machine Learning. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1953.

Council of Science Editors:

Guzman E. Generating Exploration Mission-3 Trajectories to a 9:2 NRHO using Machine Learning. [Masters Thesis]. Cal Poly; 2018. Available from: https://digitalcommons.calpoly.edu/theses/1953


Cal Poly

11. Kirkpatrick, Brian E. "Picasso" Interface for Horizon Simulation Framework.

Degree: MS, Aerospace Engineering, 2010, Cal Poly

 The Horizon Simulation Framework, or HSF, is a modeling and simulation framework compiled from C/C++ source code into a command line program. Picasso is an… (more)

Subjects/Keywords: picasso; horizon; simulation; spacecraft; satellite; modeling; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Kirkpatrick, B. E. (2010). "Picasso" Interface for Horizon Simulation Framework. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/372 ; 10.15368/theses.2010.137

Chicago Manual of Style (16th Edition):

Kirkpatrick, Brian E. “"Picasso" Interface for Horizon Simulation Framework.” 2010. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/372 ; 10.15368/theses.2010.137.

MLA Handbook (7th Edition):

Kirkpatrick, Brian E. “"Picasso" Interface for Horizon Simulation Framework.” 2010. Web. 16 Oct 2019.

Vancouver:

Kirkpatrick BE. "Picasso" Interface for Horizon Simulation Framework. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/372 ; 10.15368/theses.2010.137.

Council of Science Editors:

Kirkpatrick BE. "Picasso" Interface for Horizon Simulation Framework. [Masters Thesis]. Cal Poly; 2010. Available from: https://digitalcommons.calpoly.edu/theses/372 ; 10.15368/theses.2010.137


Cal Poly

12. Currie, Blake J. Control of a Spacecraft Using Mixed Momentum Exchange Devices.

Degree: MS, Aerospace Engineering, 2014, Cal Poly

  Hardware configurations, a control law, and a steering law are developed for a mixed hardware spacecraft that uses both control moment gyros and reaction… (more)

Subjects/Keywords: spacecraft; control; CMG; Gyro; Reaction Wheel; Pointing; Acoustics, Dynamics, and Controls; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Currie, B. J. (2014). Control of a Spacecraft Using Mixed Momentum Exchange Devices. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1313 ; 10.15368/theses.2014.162

Chicago Manual of Style (16th Edition):

Currie, Blake J. “Control of a Spacecraft Using Mixed Momentum Exchange Devices.” 2014. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1313 ; 10.15368/theses.2014.162.

MLA Handbook (7th Edition):

Currie, Blake J. “Control of a Spacecraft Using Mixed Momentum Exchange Devices.” 2014. Web. 16 Oct 2019.

Vancouver:

Currie BJ. Control of a Spacecraft Using Mixed Momentum Exchange Devices. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1313 ; 10.15368/theses.2014.162.

Council of Science Editors:

Currie BJ. Control of a Spacecraft Using Mixed Momentum Exchange Devices. [Masters Thesis]. Cal Poly; 2014. Available from: https://digitalcommons.calpoly.edu/theses/1313 ; 10.15368/theses.2014.162


Cal Poly

13. KATO, TOMOYUKI. Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification.

Degree: MS, Aerospace Engineering, 2014, Cal Poly

  The Cal Poly Spacecraft Dynamics Simulator, also known as the Pyramidal Reaction Wheel Platform (PRWP), is an air-bearing four reaction wheel spacecraft simulator designed… (more)

Subjects/Keywords: Spacecraft; Simulator; Adaptive; Control; Robust; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

KATO, T. (2014). Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1201 ; 10.15368/theses.2014.48

Chicago Manual of Style (16th Edition):

KATO, TOMOYUKI. “Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification.” 2014. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1201 ; 10.15368/theses.2014.48.

MLA Handbook (7th Edition):

KATO, TOMOYUKI. “Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification.” 2014. Web. 16 Oct 2019.

Vancouver:

KATO T. Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1201 ; 10.15368/theses.2014.48.

Council of Science Editors:

KATO T. Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification. [Masters Thesis]. Cal Poly; 2014. Available from: https://digitalcommons.calpoly.edu/theses/1201 ; 10.15368/theses.2014.48


Cal Poly

14. 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 October 16, 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. 16 Oct 2019.

Vancouver:

Brake NJ. Control System Development for small UAV Gimbal. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Oct 16]. 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


Cal Poly

15. Luther, Shaun. SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  This thesis examines the feasibility of substituting the system input script of Cal Poly’s Horizon Simulation Framework (HSF) with a Model Based Systems Engineering… (more)

Subjects/Keywords: SysML; HSF; CubeSat; Simulation; Model; Space Vehicles; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Luther, S. (2016). SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1591 ; 10.15368/theses.2016.63

Chicago Manual of Style (16th Edition):

Luther, Shaun. “SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK.” 2016. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1591 ; 10.15368/theses.2016.63.

MLA Handbook (7th Edition):

Luther, Shaun. “SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK.” 2016. Web. 16 Oct 2019.

Vancouver:

Luther S. SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1591 ; 10.15368/theses.2016.63.

Council of Science Editors:

Luther S. SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1591 ; 10.15368/theses.2016.63


Cal Poly

16. Lunsford, Ian M. SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  System design is an inherently expensive and time consuming process. Engineers are constantly tasked to investigate new solutions for various programs. Model-based systems engineering… (more)

Subjects/Keywords: Horizon Simulation Framework; Model-based Systems Engineering; Simulations; Modeling; Systems Engineering; MBSE; Model-based Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Lunsford, I. M. (2016). SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1560 ; 10.15368/theses.2016.40

Chicago Manual of Style (16th Edition):

Lunsford, Ian M. “SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK.” 2016. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1560 ; 10.15368/theses.2016.40.

MLA Handbook (7th Edition):

Lunsford, Ian M. “SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK.” 2016. Web. 16 Oct 2019.

Vancouver:

Lunsford IM. SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1560 ; 10.15368/theses.2016.40.

Council of Science Editors:

Lunsford IM. SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1560 ; 10.15368/theses.2016.40

17. Mirijanian, James Julian. Techniques to Characterize Vapor Cell Performance for a Nuclear-Magnetic-Resonance Gyroscope.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  Research was performed to improve the procedures for testing performance parameters of vapor cells for a nuclear-magnetic-resonance gyroscope. In addition to summarizing the theoretical… (more)

Subjects/Keywords: gyroscope; nmr; atom; lifetime; larmor precession; quantum mechanics; Atomic, Molecular and Optical Physics

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APA (6th Edition):

Mirijanian, J. J. (2012). Techniques to Characterize Vapor Cell Performance for a Nuclear-Magnetic-Resonance Gyroscope. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/724 ; 10.15368/theses.2012.39

Chicago Manual of Style (16th Edition):

Mirijanian, James Julian. “Techniques to Characterize Vapor Cell Performance for a Nuclear-Magnetic-Resonance Gyroscope.” 2012. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/724 ; 10.15368/theses.2012.39.

MLA Handbook (7th Edition):

Mirijanian, James Julian. “Techniques to Characterize Vapor Cell Performance for a Nuclear-Magnetic-Resonance Gyroscope.” 2012. Web. 16 Oct 2019.

Vancouver:

Mirijanian JJ. Techniques to Characterize Vapor Cell Performance for a Nuclear-Magnetic-Resonance Gyroscope. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/724 ; 10.15368/theses.2012.39.

Council of Science Editors:

Mirijanian JJ. Techniques to Characterize Vapor Cell Performance for a Nuclear-Magnetic-Resonance Gyroscope. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/724 ; 10.15368/theses.2012.39

18. Haddock, Michelle. Inductive Monitoring Systems: A CubeSat Ground-Based Prototype.

Degree: MS, Aerospace Engineering, 2015, Cal Poly

  Inductive Monitoring Systems (IMS) are the newest form of health monitoring available to the aerospace industry. IMS is a program that builds a knowledge… (more)

Subjects/Keywords: IMS; Aerospace Engineering

…based prototype of IMS developed for a CubeSat testbed at Cal Poly. This thesis describes how… 

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APA (6th Edition):

Haddock, M. (2015). Inductive Monitoring Systems: A CubeSat Ground-Based Prototype. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1515 ; 10.15368/theses.2015.164

Chicago Manual of Style (16th Edition):

Haddock, Michelle. “Inductive Monitoring Systems: A CubeSat Ground-Based Prototype.” 2015. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1515 ; 10.15368/theses.2015.164.

MLA Handbook (7th Edition):

Haddock, Michelle. “Inductive Monitoring Systems: A CubeSat Ground-Based Prototype.” 2015. Web. 16 Oct 2019.

Vancouver:

Haddock M. Inductive Monitoring Systems: A CubeSat Ground-Based Prototype. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1515 ; 10.15368/theses.2015.164.

Council of Science Editors:

Haddock M. Inductive Monitoring Systems: A CubeSat Ground-Based Prototype. [Masters Thesis]. Cal Poly; 2015. Available from: https://digitalcommons.calpoly.edu/theses/1515 ; 10.15368/theses.2015.164

19. Yost, Morgan. An Iteration on the Horizon Simulation Framework to Include .NET and Python Scripting.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  Modeling and Simulation is a crucial element of the aerospace engineering design pro- cess because it allows designers to thoroughly test their solution before… (more)

Subjects/Keywords: Modeling and Simulation; Aerospace; Design; Verification; Space Vehicles; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Yost, M. (2016). An Iteration on the Horizon Simulation Framework to Include .NET and Python Scripting. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1607 ; 10.15368/theses.2016.77

Chicago Manual of Style (16th Edition):

Yost, Morgan. “An Iteration on the Horizon Simulation Framework to Include .NET and Python Scripting.” 2016. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1607 ; 10.15368/theses.2016.77.

MLA Handbook (7th Edition):

Yost, Morgan. “An Iteration on the Horizon Simulation Framework to Include .NET and Python Scripting.” 2016. Web. 16 Oct 2019.

Vancouver:

Yost M. An Iteration on the Horizon Simulation Framework to Include .NET and Python Scripting. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1607 ; 10.15368/theses.2016.77.

Council of Science Editors:

Yost M. An Iteration on the Horizon Simulation Framework to Include .NET and Python Scripting. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1607 ; 10.15368/theses.2016.77

20. Chiu, Alton Pak-Hin. Flying Qualities Built-In-Test For Unmanned Aerial Systems.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  This paper presents a flying qualities built-in-test for UAS application with the scope limited to the longitudinal axis. A doublet input waveform excites the… (more)

Subjects/Keywords: SID; UAV; Flying Qualities; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Chiu, A. P. (2012). Flying Qualities Built-In-Test For Unmanned Aerial Systems. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/712 ; 10.15368/theses.2012.54

Chicago Manual of Style (16th Edition):

Chiu, Alton Pak-Hin. “Flying Qualities Built-In-Test For Unmanned Aerial Systems.” 2012. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/712 ; 10.15368/theses.2012.54.

MLA Handbook (7th Edition):

Chiu, Alton Pak-Hin. “Flying Qualities Built-In-Test For Unmanned Aerial Systems.” 2012. Web. 16 Oct 2019.

Vancouver:

Chiu AP. Flying Qualities Built-In-Test For Unmanned Aerial Systems. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/712 ; 10.15368/theses.2012.54.

Council of Science Editors:

Chiu AP. Flying Qualities Built-In-Test For Unmanned Aerial Systems. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/712 ; 10.15368/theses.2012.54

21. Lopez, Christian W. UAV Formation Flight Utilizing a Low Cost, Open Source Configuration.

Degree: MS, Aerospace Engineering, 2013, Cal Poly

  The control of multiple unmanned aerial vehicles (UAVs) in a swarm or cooperative team scenario has been a topic of great interest for well… (more)

Subjects/Keywords: UAV; Formation Flight; Simulation; Flight Testing; Multi-Vehicle Systems and Air Traffic Control; Navigation, Guidance, Control and Dynamics

…evaluation test set-up at the Cal Poly EFR… …projects at Cal Poly, but also among academics and hobbyists around the world. 1.3 Project… …Goals Previous work at Cal Poly has focused on the development and high-level simulation of a… …control studies at Cal Poly • Adaptation of the developed control strategies for an embedded… …studies at Cal Poly in a way that will be both meaningful and sustainable, low cost hardware and… 

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APA (6th Edition):

Lopez, C. W. (2013). UAV Formation Flight Utilizing a Low Cost, Open Source Configuration. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1089 ; 10.15368/theses.2013.103

Chicago Manual of Style (16th Edition):

Lopez, Christian W. “UAV Formation Flight Utilizing a Low Cost, Open Source Configuration.” 2013. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1089 ; 10.15368/theses.2013.103.

MLA Handbook (7th Edition):

Lopez, Christian W. “UAV Formation Flight Utilizing a Low Cost, Open Source Configuration.” 2013. Web. 16 Oct 2019.

Vancouver:

Lopez CW. UAV Formation Flight Utilizing a Low Cost, Open Source Configuration. [Internet] [Masters thesis]. Cal Poly; 2013. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1089 ; 10.15368/theses.2013.103.

Council of Science Editors:

Lopez CW. UAV Formation Flight Utilizing a Low Cost, Open Source Configuration. [Masters Thesis]. Cal Poly; 2013. Available from: https://digitalcommons.calpoly.edu/theses/1089 ; 10.15368/theses.2013.103

22. Burt, Colin. Design, Fabrication and Test of an Operationally Responsive Aircraft with NIIRS Evaluated Imager.

Degree: MS, 2013, Cal Poly

  Unmanned Aerial Systems (UAS) are a growing asset. Currently UAS are on the cutting edge with resources being spent developing the capabilities mostly for… (more)

Subjects/Keywords: Aircraft; NIIRS; UAV; Imager; Airplane; Remote Sensing; Aerospace Engineering; Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Burt, C. (2013). Design, Fabrication and Test of an Operationally Responsive Aircraft with NIIRS Evaluated Imager. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1087 ; 10.15368/theses.2013.167

Chicago Manual of Style (16th Edition):

Burt, Colin. “Design, Fabrication and Test of an Operationally Responsive Aircraft with NIIRS Evaluated Imager.” 2013. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1087 ; 10.15368/theses.2013.167.

MLA Handbook (7th Edition):

Burt, Colin. “Design, Fabrication and Test of an Operationally Responsive Aircraft with NIIRS Evaluated Imager.” 2013. Web. 16 Oct 2019.

Vancouver:

Burt C. Design, Fabrication and Test of an Operationally Responsive Aircraft with NIIRS Evaluated Imager. [Internet] [Masters thesis]. Cal Poly; 2013. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1087 ; 10.15368/theses.2013.167.

Council of Science Editors:

Burt C. Design, Fabrication and Test of an Operationally Responsive Aircraft with NIIRS Evaluated Imager. [Masters Thesis]. Cal Poly; 2013. Available from: https://digitalcommons.calpoly.edu/theses/1087 ; 10.15368/theses.2013.167

23. Ruddy, Marcus A. Pico-Satellite Integrated System Level Test Program.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  Testing is an integral part of a satellite’s development, requirements verification and risk mitigation efforts. A robust test program serves to verify construction, integration… (more)

Subjects/Keywords: Pico-satellite; Requirements; Verification; Test; CubeSat; Space Vehicles; Systems Engineering; Systems Engineering and Multidisciplinary Design Optimization

…between California Polytechnic State University, San Luis Obispo (Cal Poly), and… …technology or provides tools for scientific research. Figure 1 shows multiple CubeSats. Cal Poly is… …In the case of the CubeSat Program, stakeholder examples include the Cal Poly students and… …to ensure compliance. For the Cal Poly CubeSat, most requirements have already been… …for the Cal Poly CP2 Cubesat Project. B.S. Senior Project. California Polytechnic State… 

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APA (6th Edition):

Ruddy, M. A. (2012). Pico-Satellite Integrated System Level Test Program. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/688 ; 10.15368/theses.2012.5

Chicago Manual of Style (16th Edition):

Ruddy, Marcus A. “Pico-Satellite Integrated System Level Test Program.” 2012. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/688 ; 10.15368/theses.2012.5.

MLA Handbook (7th Edition):

Ruddy, Marcus A. “Pico-Satellite Integrated System Level Test Program.” 2012. Web. 16 Oct 2019.

Vancouver:

Ruddy MA. Pico-Satellite Integrated System Level Test Program. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/688 ; 10.15368/theses.2012.5.

Council of Science Editors:

Ruddy MA. Pico-Satellite Integrated System Level Test Program. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/688 ; 10.15368/theses.2012.5

24. Lewis, Eugene Daniel. Activity Node Based Flight Software as a Benefit to Systems Engineering.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  This report discusses one application of a flight software design for a spacecraft in which the software executes from a database that can be… (more)

Subjects/Keywords: Flight Software; Systems Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Lewis, E. D. (2012). Activity Node Based Flight Software as a Benefit to Systems Engineering. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/734 ; 10.15368/theses.2012.59

Chicago Manual of Style (16th Edition):

Lewis, Eugene Daniel. “Activity Node Based Flight Software as a Benefit to Systems Engineering.” 2012. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/734 ; 10.15368/theses.2012.59.

MLA Handbook (7th Edition):

Lewis, Eugene Daniel. “Activity Node Based Flight Software as a Benefit to Systems Engineering.” 2012. Web. 16 Oct 2019.

Vancouver:

Lewis ED. Activity Node Based Flight Software as a Benefit to Systems Engineering. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/734 ; 10.15368/theses.2012.59.

Council of Science Editors:

Lewis ED. Activity Node Based Flight Software as a Benefit to Systems Engineering. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/734 ; 10.15368/theses.2012.59

25. Marchini, Brian Decimo. Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs.

Degree: MS, Aerospace Engineering, 2013, Cal Poly

  Fixed-wing unmanned aerial vehicles (UAVs) with the ability to hover combine the speed and endurance of traditional fixed-wing fight with the stable hovering and… (more)

Subjects/Keywords: Unmanned Aerial Vehicles; Adaptive Control; Autopilots; Arduino; ArduPilot; Fixed-Wing Hovering; Aerodynamics and Fluid Mechanics; Aeronautical Vehicles; Navigation, Guidance, Control and Dynamics

…airplane. By using the APM and ArduPlane firmware, the research at Cal Poly has been able focus… 

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APA (6th Edition):

Marchini, B. D. (2013). Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1108 ; 10.15368/theses.2013.191

Chicago Manual of Style (16th Edition):

Marchini, Brian Decimo. “Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs.” 2013. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1108 ; 10.15368/theses.2013.191.

MLA Handbook (7th Edition):

Marchini, Brian Decimo. “Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs.” 2013. Web. 16 Oct 2019.

Vancouver:

Marchini BD. Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs. [Internet] [Masters thesis]. Cal Poly; 2013. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1108 ; 10.15368/theses.2013.191.

Council of Science Editors:

Marchini BD. Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs. [Masters Thesis]. Cal Poly; 2013. Available from: https://digitalcommons.calpoly.edu/theses/1108 ; 10.15368/theses.2013.191

26. Scherling, Alexander I. Reduced-Order Reference Models for Adaptive Control of Space Structures.

Degree: MS, Aerospace Engineering, 2014, Cal Poly

  In addition to serving as a brief overview of aspects relevant to reduced-order modeling (in particular balanced-state and modal techniques) as applied to structural… (more)

Subjects/Keywords: Balanced Truncation; Modal Form; Gramian; Adaptive Control; Finite Element; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Scherling, A. I. (2014). Reduced-Order Reference Models for Adaptive Control of Space Structures. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1199 ; 10.15368/theses.2014.46

Chicago Manual of Style (16th Edition):

Scherling, Alexander I. “Reduced-Order Reference Models for Adaptive Control of Space Structures.” 2014. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1199 ; 10.15368/theses.2014.46.

MLA Handbook (7th Edition):

Scherling, Alexander I. “Reduced-Order Reference Models for Adaptive Control of Space Structures.” 2014. Web. 16 Oct 2019.

Vancouver:

Scherling AI. Reduced-Order Reference Models for Adaptive Control of Space Structures. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1199 ; 10.15368/theses.2014.46.

Council of Science Editors:

Scherling AI. Reduced-Order Reference Models for Adaptive Control of Space Structures. [Masters Thesis]. Cal Poly; 2014. Available from: https://digitalcommons.calpoly.edu/theses/1199 ; 10.15368/theses.2014.46

27. Butler, Brian Jeffrey. Dynamic Model Creation and Scripting Support in the Horizon Simulation Framework.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  Dynamic model creation and support for the Lua scripting language was added to the Horizon Simulation Framework used for the verification and validation of… (more)

Subjects/Keywords: Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Butler, B. J. (2012). Dynamic Model Creation and Scripting Support in the Horizon Simulation Framework. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/697 ; 10.15368/theses.2012.8

Chicago Manual of Style (16th Edition):

Butler, Brian Jeffrey. “Dynamic Model Creation and Scripting Support in the Horizon Simulation Framework.” 2012. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/697 ; 10.15368/theses.2012.8.

MLA Handbook (7th Edition):

Butler, Brian Jeffrey. “Dynamic Model Creation and Scripting Support in the Horizon Simulation Framework.” 2012. Web. 16 Oct 2019.

Vancouver:

Butler BJ. Dynamic Model Creation and Scripting Support in the Horizon Simulation Framework. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/697 ; 10.15368/theses.2012.8.

Council of Science Editors:

Butler BJ. Dynamic Model Creation and Scripting Support in the Horizon Simulation Framework. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/697 ; 10.15368/theses.2012.8

28. Borra, Brian M. Nonlinear UAV Flight Control Using Command Filtered Backstepping.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  The aim of this effort is to implement a nonlinear flight control architecture, specifically flight path control via command filtered backstepping, for use in… (more)

Subjects/Keywords: Backstepping; Control Allocation; Command Filtering; Nonlinear; UAV; Lyapunov; Aeronautical Vehicles; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Borra, B. M. (2012). Nonlinear UAV Flight Control Using Command Filtered Backstepping. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/713 ; 10.15368/theses.2012.29

Chicago Manual of Style (16th Edition):

Borra, Brian M. “Nonlinear UAV Flight Control Using Command Filtered Backstepping.” 2012. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/713 ; 10.15368/theses.2012.29.

MLA Handbook (7th Edition):

Borra, Brian M. “Nonlinear UAV Flight Control Using Command Filtered Backstepping.” 2012. Web. 16 Oct 2019.

Vancouver:

Borra BM. Nonlinear UAV Flight Control Using Command Filtered Backstepping. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/713 ; 10.15368/theses.2012.29.

Council of Science Editors:

Borra BM. Nonlinear UAV Flight Control Using Command Filtered Backstepping. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/713 ; 10.15368/theses.2012.29

29. Darling, Michael B. Autonomous Close Formation Flight of Small UAVs Using Vision-Based Localization.

Degree: MS, Aerospace Engineering, 2014, Cal Poly

  As Unmanned Aerial Vehicles (UAVs) are integrated into the national airspace to comply with the 2012 Federal Aviation Administration Reauthorization Act, new civilian uses… (more)

Subjects/Keywords: Vision Formation Flight UAV LEDs PnP; Navigation, Guidance, Control and Dynamics

…Formation Flight Work at Cal Poly Over the course of the past few years, a number of projects… …dealing with small UAVs have come through the Cal Poly Aerospace Engineering Department. Of… …completed his thesis, which built upon the simulation work of Cal Poly alumnus, Masamitsu Tsuruta… …upon previous small UAV work carried out at Cal Poly by designing, implementing, and… …projects at Cal Poly by developing a baseline vision system. Future students interested in camera… 

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APA (6th Edition):

Darling, M. B. (2014). Autonomous Close Formation Flight of Small UAVs Using Vision-Based Localization. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1185 ; 10.15368/theses.2014.27

Chicago Manual of Style (16th Edition):

Darling, Michael B. “Autonomous Close Formation Flight of Small UAVs Using Vision-Based Localization.” 2014. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/1185 ; 10.15368/theses.2014.27.

MLA Handbook (7th Edition):

Darling, Michael B. “Autonomous Close Formation Flight of Small UAVs Using Vision-Based Localization.” 2014. Web. 16 Oct 2019.

Vancouver:

Darling MB. Autonomous Close Formation Flight of Small UAVs Using Vision-Based Localization. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/1185 ; 10.15368/theses.2014.27.

Council of Science Editors:

Darling MB. Autonomous Close Formation Flight of Small UAVs Using Vision-Based Localization. [Masters Thesis]. Cal Poly; 2014. Available from: https://digitalcommons.calpoly.edu/theses/1185 ; 10.15368/theses.2014.27

30. Brown, Sean M. Determination of Human Powered Helicopter Stability Characteristics using Multi-Body System Simulation Techniques.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  Multi-Body System Simulation combined with System Identification was developed as a method for determining the stability characteristics of a human powered helicopter(HPH) configurations. HPH… (more)

Subjects/Keywords: HPH; Simulation; Stability; Dynamics; Human-Powered; Helicopter; Aeronautical Vehicles; Navigation, Guidance, Control and Dynamics

…Figure 1.3: Gamera II’s Highest flight,[3] The Da Vinci Series from Cal Poly and the… …x5B;32] focused on the stability and possible control of the Da Vinci series from Cal… …Poly. Totah and Patterson used a five degree of freedom kinematic model to study the affect… 

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APA (6th Edition):

Brown, S. M. (2012). Determination of Human Powered Helicopter Stability Characteristics using Multi-Body System Simulation Techniques. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/874 ; 10.15368/theses.2012.192

Chicago Manual of Style (16th Edition):

Brown, Sean M. “Determination of Human Powered Helicopter Stability Characteristics using Multi-Body System Simulation Techniques.” 2012. Masters Thesis, Cal Poly. Accessed October 16, 2019. https://digitalcommons.calpoly.edu/theses/874 ; 10.15368/theses.2012.192.

MLA Handbook (7th Edition):

Brown, Sean M. “Determination of Human Powered Helicopter Stability Characteristics using Multi-Body System Simulation Techniques.” 2012. Web. 16 Oct 2019.

Vancouver:

Brown SM. Determination of Human Powered Helicopter Stability Characteristics using Multi-Body System Simulation Techniques. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Oct 16]. Available from: https://digitalcommons.calpoly.edu/theses/874 ; 10.15368/theses.2012.192.

Council of Science Editors:

Brown SM. Determination of Human Powered Helicopter Stability Characteristics using Multi-Body System Simulation Techniques. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/874 ; 10.15368/theses.2012.192

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