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You searched for subject:(Navigation Guidance Control AND Dynamics). Showing records 1 – 30 of 1026 total matches.

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Cal Poly

1. Iuliano, Jay R. A Solution to the Circular Restricted N Body Problem in Planetary Systems.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  This thesis is a brief look at a new solution to a problem that has been approached in many different ways in the past… (more)

Subjects/Keywords: Astrodynamics; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Iuliano, J. R. (2016). A Solution to the Circular Restricted N Body Problem in Planetary Systems. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80

Chicago Manual of Style (16th Edition):

Iuliano, Jay R. “A Solution to the Circular Restricted N Body Problem in Planetary Systems.” 2016. Masters Thesis, Cal Poly. Accessed April 07, 2020. https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80.

MLA Handbook (7th Edition):

Iuliano, Jay R. “A Solution to the Circular Restricted N Body Problem in Planetary Systems.” 2016. Web. 07 Apr 2020.

Vancouver:

Iuliano JR. A Solution to the Circular Restricted N Body Problem in Planetary Systems. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2020 Apr 07]. Available from: https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80.

Council of Science Editors:

Iuliano JR. A Solution to the Circular Restricted N Body Problem in Planetary Systems. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80


University of Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Leonard, Jason Michael. “Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.” 2015. Doctoral Dissertation, University of Colorado. Accessed April 07, 2020. https://scholar.colorado.edu/asen_gradetds/97.

MLA Handbook (7th Edition):

Leonard, Jason Michael. “Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System.” 2015. Web. 07 Apr 2020.

Vancouver:

Leonard JM. Supporting Crewed Missions using LiAISON Navigation in the Earth-Moon System. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2020 Apr 07]. Available from: https://scholar.colorado.edu/asen_gradetds/97.

Council of Science Editors:

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


Cal Poly

3. 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 April 07, 2020. 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. 07 Apr 2020.

Vancouver:

KATO T. Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2020 Apr 07]. 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

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

Degree: MS, Aerospace Engineering, 2016, Cal Poly

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Villa, Andres Eduardo. “Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere.” 2016. Masters Thesis, Cal Poly. Accessed April 07, 2020. https://digitalcommons.calpoly.edu/theses/1571 ; 10.15368/theses.2016.48.

MLA Handbook (7th Edition):

Villa, Andres Eduardo. “Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere.” 2016. Web. 07 Apr 2020.

Vancouver:

Villa AE. Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2020 Apr 07]. Available from: https://digitalcommons.calpoly.edu/theses/1571 ; 10.15368/theses.2016.48.

Council of Science Editors:

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


Cal Poly

5. 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 April 07, 2020. 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. 07 Apr 2020.

Vancouver:

Brake NJ. Control System Development for small UAV Gimbal. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2020 Apr 07]. 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

6. DiMiceli, Jacob Daniel. ATTITUDE DETERMINATION OF A STUDENT SATELLITE USING ON-ORBIT MAGNETOMETER AND TEMPERATURE DATA.

Degree: MS, Aerospace Engineering, 2009, Cal Poly

 An extended Kalman filter is modified to support only magnetometer data as a measurement for spacecraft attitude information. Actual on-orbit data from a student satellite… (more)

Subjects/Keywords: Navigation; Guidance; Control and Dynamics

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APA (6th Edition):

DiMiceli, J. D. (2009). ATTITUDE DETERMINATION OF A STUDENT SATELLITE USING ON-ORBIT MAGNETOMETER AND TEMPERATURE DATA. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/106 ; 10.15368/theses.2009.62

Chicago Manual of Style (16th Edition):

DiMiceli, Jacob Daniel. “ATTITUDE DETERMINATION OF A STUDENT SATELLITE USING ON-ORBIT MAGNETOMETER AND TEMPERATURE DATA.” 2009. Masters Thesis, Cal Poly. Accessed April 07, 2020. https://digitalcommons.calpoly.edu/theses/106 ; 10.15368/theses.2009.62.

MLA Handbook (7th Edition):

DiMiceli, Jacob Daniel. “ATTITUDE DETERMINATION OF A STUDENT SATELLITE USING ON-ORBIT MAGNETOMETER AND TEMPERATURE DATA.” 2009. Web. 07 Apr 2020.

Vancouver:

DiMiceli JD. ATTITUDE DETERMINATION OF A STUDENT SATELLITE USING ON-ORBIT MAGNETOMETER AND TEMPERATURE DATA. [Internet] [Masters thesis]. Cal Poly; 2009. [cited 2020 Apr 07]. Available from: https://digitalcommons.calpoly.edu/theses/106 ; 10.15368/theses.2009.62.

Council of Science Editors:

DiMiceli JD. ATTITUDE DETERMINATION OF A STUDENT SATELLITE USING ON-ORBIT MAGNETOMETER AND TEMPERATURE DATA. [Masters Thesis]. Cal Poly; 2009. Available from: https://digitalcommons.calpoly.edu/theses/106 ; 10.15368/theses.2009.62


Cal Poly

7. 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 April 07, 2020. 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. 07 Apr 2020.

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 2020 Apr 07]. 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


University of Tennessee – Knoxville

8. Kamp, Michael Anthony. Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet.

Degree: MS, Aviation Systems, 2009, University of Tennessee – Knoxville

 A self-contained, portable, inertial and positional measurement system was developed and tested for an HGU-55 model fighter pilot helmet. The system, designated the Portable Helmet… (more)

Subjects/Keywords: Navigation; Guidance; Control and Dynamics

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APA (6th Edition):

Kamp, M. A. (2009). Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/535

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

Chicago Manual of Style (16th Edition):

Kamp, Michael Anthony. “Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet.” 2009. Thesis, University of Tennessee – Knoxville. Accessed April 07, 2020. https://trace.tennessee.edu/utk_gradthes/535.

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

MLA Handbook (7th Edition):

Kamp, Michael Anthony. “Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet.” 2009. Web. 07 Apr 2020.

Vancouver:

Kamp MA. Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet. [Internet] [Thesis]. University of Tennessee – Knoxville; 2009. [cited 2020 Apr 07]. Available from: https://trace.tennessee.edu/utk_gradthes/535.

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

Council of Science Editors:

Kamp MA. Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet. [Thesis]. University of Tennessee – Knoxville; 2009. Available from: https://trace.tennessee.edu/utk_gradthes/535

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


University of Tennessee – Knoxville

9. Schrum, Brian T. F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings.

Degree: MS, Aviation Systems, 2007, University of Tennessee – Knoxville

  The purpose for writing this thesis is to prove the automatic carrier landing system (ACLS) a valuable Operational Risk Management (ORM) tool for recovering… (more)

Subjects/Keywords: Navigation; Guidance; Control and Dynamics

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APA (6th Edition):

Schrum, B. T. (2007). F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/323

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

Chicago Manual of Style (16th Edition):

Schrum, Brian T. “F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings.” 2007. Thesis, University of Tennessee – Knoxville. Accessed April 07, 2020. https://trace.tennessee.edu/utk_gradthes/323.

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

MLA Handbook (7th Edition):

Schrum, Brian T. “F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings.” 2007. Web. 07 Apr 2020.

Vancouver:

Schrum BT. F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings. [Internet] [Thesis]. University of Tennessee – Knoxville; 2007. [cited 2020 Apr 07]. Available from: https://trace.tennessee.edu/utk_gradthes/323.

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

Council of Science Editors:

Schrum BT. F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings. [Thesis]. University of Tennessee – Knoxville; 2007. Available from: https://trace.tennessee.edu/utk_gradthes/323

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


University of Tennessee – Knoxville

10. Reimuller, Jason David. The Design and Integration of an Airborne Imager and Flight Campaign to Study the Time Evolution and Vertical Structures of Polar Mesospheric Clouds.

Degree: MS, Aviation Systems, 2007, University of Tennessee – Knoxville

  The scientific objective of this study is to design an aircraft flight experiment that will provide airborne imaging data, augmenting satellite data, to advance… (more)

Subjects/Keywords: Navigation; Guidance; Control and Dynamics

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APA (6th Edition):

Reimuller, J. D. (2007). The Design and Integration of an Airborne Imager and Flight Campaign to Study the Time Evolution and Vertical Structures of Polar Mesospheric Clouds. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/318

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

Chicago Manual of Style (16th Edition):

Reimuller, Jason David. “The Design and Integration of an Airborne Imager and Flight Campaign to Study the Time Evolution and Vertical Structures of Polar Mesospheric Clouds.” 2007. Thesis, University of Tennessee – Knoxville. Accessed April 07, 2020. https://trace.tennessee.edu/utk_gradthes/318.

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

MLA Handbook (7th Edition):

Reimuller, Jason David. “The Design and Integration of an Airborne Imager and Flight Campaign to Study the Time Evolution and Vertical Structures of Polar Mesospheric Clouds.” 2007. Web. 07 Apr 2020.

Vancouver:

Reimuller JD. The Design and Integration of an Airborne Imager and Flight Campaign to Study the Time Evolution and Vertical Structures of Polar Mesospheric Clouds. [Internet] [Thesis]. University of Tennessee – Knoxville; 2007. [cited 2020 Apr 07]. Available from: https://trace.tennessee.edu/utk_gradthes/318.

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

Council of Science Editors:

Reimuller JD. The Design and Integration of an Airborne Imager and Flight Campaign to Study the Time Evolution and Vertical Structures of Polar Mesospheric Clouds. [Thesis]. University of Tennessee – Knoxville; 2007. Available from: https://trace.tennessee.edu/utk_gradthes/318

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


University of Tennessee – Knoxville

11. Mires, James Robert. A Compliance Strategy for Use of GPS for IFR Navigation in the E-2C Hawkeye.

Degree: MS, Aviation Systems, 2007, University of Tennessee – Knoxville

  Naval aviation is on the brink of taking advantage of a 12 year old capability. Naval commercial derivative aircraft have had the ability to… (more)

Subjects/Keywords: Navigation; Guidance; Control and Dynamics

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APA (6th Edition):

Mires, J. R. (2007). A Compliance Strategy for Use of GPS for IFR Navigation in the E-2C Hawkeye. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/312

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

Chicago Manual of Style (16th Edition):

Mires, James Robert. “A Compliance Strategy for Use of GPS for IFR Navigation in the E-2C Hawkeye.” 2007. Thesis, University of Tennessee – Knoxville. Accessed April 07, 2020. https://trace.tennessee.edu/utk_gradthes/312.

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

MLA Handbook (7th Edition):

Mires, James Robert. “A Compliance Strategy for Use of GPS for IFR Navigation in the E-2C Hawkeye.” 2007. Web. 07 Apr 2020.

Vancouver:

Mires JR. A Compliance Strategy for Use of GPS for IFR Navigation in the E-2C Hawkeye. [Internet] [Thesis]. University of Tennessee – Knoxville; 2007. [cited 2020 Apr 07]. Available from: https://trace.tennessee.edu/utk_gradthes/312.

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

Council of Science Editors:

Mires JR. A Compliance Strategy for Use of GPS for IFR Navigation in the E-2C Hawkeye. [Thesis]. University of Tennessee – Knoxville; 2007. Available from: https://trace.tennessee.edu/utk_gradthes/312

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


Embry-Riddle Aeronautical University

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Hervás, Jaime Rubio. “Dynamics and Control of Higher-order Nonholonomic Systems.” 2013. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed April 07, 2020. https://commons.erau.edu/edt/154.

MLA Handbook (7th Edition):

Hervás, Jaime Rubio. “Dynamics and Control of Higher-order Nonholonomic Systems.” 2013. Web. 07 Apr 2020.

Vancouver:

Hervás JR. Dynamics and Control of Higher-order Nonholonomic Systems. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2013. [cited 2020 Apr 07]. Available from: https://commons.erau.edu/edt/154.

Council of Science Editors:

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


Grand Valley State University

13. Gross, Richard Allen. Algorithm for Geodetic Positioning Based On Angle-Of-Arrival of Automatic Dependent Surveillance-Broadcasts.

Degree: 2019, Grand Valley State University

 This paper develops a non-precision, three-dimensional, geodetic positioning algorithm for airborne vehicles. The algorithm leverages the proliferation of Automatic Dependent Surveillance – Broadcast (ADS-B) equipped… (more)

Subjects/Keywords: Navigation; Positioning; Angle-of-Arrival; SLAM; ADS-B; Mechanical Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Gross, R. A. (2019). Algorithm for Geodetic Positioning Based On Angle-Of-Arrival of Automatic Dependent Surveillance-Broadcasts. (Thesis). Grand Valley State University. Retrieved from https://scholarworks.gvsu.edu/theses/925

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

Chicago Manual of Style (16th Edition):

Gross, Richard Allen. “Algorithm for Geodetic Positioning Based On Angle-Of-Arrival of Automatic Dependent Surveillance-Broadcasts.” 2019. Thesis, Grand Valley State University. Accessed April 07, 2020. https://scholarworks.gvsu.edu/theses/925.

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

MLA Handbook (7th Edition):

Gross, Richard Allen. “Algorithm for Geodetic Positioning Based On Angle-Of-Arrival of Automatic Dependent Surveillance-Broadcasts.” 2019. Web. 07 Apr 2020.

Vancouver:

Gross RA. Algorithm for Geodetic Positioning Based On Angle-Of-Arrival of Automatic Dependent Surveillance-Broadcasts. [Internet] [Thesis]. Grand Valley State University; 2019. [cited 2020 Apr 07]. Available from: https://scholarworks.gvsu.edu/theses/925.

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

Council of Science Editors:

Gross RA. Algorithm for Geodetic Positioning Based On Angle-Of-Arrival of Automatic Dependent Surveillance-Broadcasts. [Thesis]. Grand Valley State University; 2019. Available from: https://scholarworks.gvsu.edu/theses/925

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

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

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

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

Subjects/Keywords: Backstepping control; Lyapunov-Based Design; Nonlinear flight control; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Tran, Thanh Trung. “Nonlinear Flight Control Design Using Backstepping Methodology.” 2016. Doctoral Dissertation, Old Dominion University. Accessed April 07, 2020. 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16.

MLA Handbook (7th Edition):

Tran, Thanh Trung. “Nonlinear Flight Control Design Using Backstepping Methodology.” 2016. Web. 07 Apr 2020.

Vancouver:

Tran TT. Nonlinear Flight Control Design Using Backstepping Methodology. [Internet] [Doctoral dissertation]. Old Dominion University; 2016. [cited 2020 Apr 07]. Available from: 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16.

Council of Science Editors:

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


University of Nevada – Las Vegas

15. Fjare, Paul D. Feedback Speed Control of a Small Two-Stroke Internal Combustion Engine that Propels an Unmanned Aerial Vehicle.

Degree: MSE, Mechanical Engineering, 2014, University of Nevada – Las Vegas

  Unmanned aerial vehicles (UAV) require intelligent control of their power source. Small UAV are typically powered by electric motors or small two-stroke internal combustion… (more)

Subjects/Keywords: Acoustics, Dynamics, and Controls; Aerospace Engineering; Mechanical Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Fjare, P. D. (2014). Feedback Speed Control of a Small Two-Stroke Internal Combustion Engine that Propels an Unmanned Aerial Vehicle. (Masters Thesis). University of Nevada – Las Vegas. Retrieved from https://digitalscholarship.unlv.edu/thesesdissertations/2179

Chicago Manual of Style (16th Edition):

Fjare, Paul D. “Feedback Speed Control of a Small Two-Stroke Internal Combustion Engine that Propels an Unmanned Aerial Vehicle.” 2014. Masters Thesis, University of Nevada – Las Vegas. Accessed April 07, 2020. https://digitalscholarship.unlv.edu/thesesdissertations/2179.

MLA Handbook (7th Edition):

Fjare, Paul D. “Feedback Speed Control of a Small Two-Stroke Internal Combustion Engine that Propels an Unmanned Aerial Vehicle.” 2014. Web. 07 Apr 2020.

Vancouver:

Fjare PD. Feedback Speed Control of a Small Two-Stroke Internal Combustion Engine that Propels an Unmanned Aerial Vehicle. [Internet] [Masters thesis]. University of Nevada – Las Vegas; 2014. [cited 2020 Apr 07]. Available from: https://digitalscholarship.unlv.edu/thesesdissertations/2179.

Council of Science Editors:

Fjare PD. Feedback Speed Control of a Small Two-Stroke Internal Combustion Engine that Propels an Unmanned Aerial Vehicle. [Masters Thesis]. University of Nevada – Las Vegas; 2014. Available from: https://digitalscholarship.unlv.edu/thesesdissertations/2179


Cal Poly

16. 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 April 07, 2020. 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. 07 Apr 2020.

Vancouver:

Silva SF. Applied System Identification for a Four Wheel Reaction Wheel Platform. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2020 Apr 07]. 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


University of Colorado

17. Rizvi, Farheen. Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects.

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

  In this thesis, a control method is developed for the solar sail normal vector to trace a desired circular coning trajectory at orbit rate.… (more)

Subjects/Keywords: attitude dynamics and control; coning control; control methods; Solar sail; Aerospace Engineering; Navigation, Guidance, Control and Dynamics; Space Vehicles

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APA (6th Edition):

Rizvi, F. (2010). Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/8

Chicago Manual of Style (16th Edition):

Rizvi, Farheen. “Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects.” 2010. Masters Thesis, University of Colorado. Accessed April 07, 2020. https://scholar.colorado.edu/asen_gradetds/8.

MLA Handbook (7th Edition):

Rizvi, Farheen. “Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects.” 2010. Web. 07 Apr 2020.

Vancouver:

Rizvi F. Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects. [Internet] [Masters thesis]. University of Colorado; 2010. [cited 2020 Apr 07]. Available from: https://scholar.colorado.edu/asen_gradetds/8.

Council of Science Editors:

Rizvi F. Solar Sail Attitude Dynamics and Coning Control: On Developing Control Methods for Solar Sail Coning at Orbit Rate to Attain Desired Orbital Effects. [Masters Thesis]. University of Colorado; 2010. Available from: https://scholar.colorado.edu/asen_gradetds/8


Portland State University

18. Kirkpatrick, Daniel Eugene. Design of a Hardware Platform for GPS-Based Orientation Sensing.

Degree: MS(M.S.) in Electrical and Computer Engineering, Electrical and Computer Engineering, 2015, Portland State University

  Unmanned aerial vehicles (UAV's) have recently gained popularity in military, civil service, agriculture, commercial, and hobby use. This is due in part to their… (more)

Subjects/Keywords: Global Positioning System; Drone aircraft  – Control systems  – Design and construction; Inertial navigation; Electrical and Computer Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Kirkpatrick, D. E. (2015). Design of a Hardware Platform for GPS-Based Orientation Sensing. (Masters Thesis). Portland State University. Retrieved from https://pdxscholar.library.pdx.edu/open_access_etds/2197

Chicago Manual of Style (16th Edition):

Kirkpatrick, Daniel Eugene. “Design of a Hardware Platform for GPS-Based Orientation Sensing.” 2015. Masters Thesis, Portland State University. Accessed April 07, 2020. https://pdxscholar.library.pdx.edu/open_access_etds/2197.

MLA Handbook (7th Edition):

Kirkpatrick, Daniel Eugene. “Design of a Hardware Platform for GPS-Based Orientation Sensing.” 2015. Web. 07 Apr 2020.

Vancouver:

Kirkpatrick DE. Design of a Hardware Platform for GPS-Based Orientation Sensing. [Internet] [Masters thesis]. Portland State University; 2015. [cited 2020 Apr 07]. Available from: https://pdxscholar.library.pdx.edu/open_access_etds/2197.

Council of Science Editors:

Kirkpatrick DE. Design of a Hardware Platform for GPS-Based Orientation Sensing. [Masters Thesis]. Portland State University; 2015. Available from: https://pdxscholar.library.pdx.edu/open_access_etds/2197


Cal Poly

19. 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 April 07, 2020. 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. 07 Apr 2020.

Vancouver:

Downs MC. Adaptive Control Applied to the Cal Poly Spacecraft Attitude Dynamics Simulator. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2020 Apr 07]. 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

20. Li, Zhenhua. Modeling and Simulation of Autonomous Thermal Soaring with Horizon Simulation Framework.

Degree: MS, Aerospace Engineering, 2010, Cal Poly

 A thermal is a column of warm rising air triggered by differential heating on the ground. In recent studies UAVs were programmed to exploit this… (more)

Subjects/Keywords: Modeling; Autonomous; Thermal; Soaring; Horizon; Simulation; Astrodynamics; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Li, Z. (2010). Modeling and Simulation of Autonomous Thermal Soaring with Horizon Simulation Framework. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/442 ; 10.15368/theses.2010.205

Chicago Manual of Style (16th Edition):

Li, Zhenhua. “Modeling and Simulation of Autonomous Thermal Soaring with Horizon Simulation Framework.” 2010. Masters Thesis, Cal Poly. Accessed April 07, 2020. https://digitalcommons.calpoly.edu/theses/442 ; 10.15368/theses.2010.205.

MLA Handbook (7th Edition):

Li, Zhenhua. “Modeling and Simulation of Autonomous Thermal Soaring with Horizon Simulation Framework.” 2010. Web. 07 Apr 2020.

Vancouver:

Li Z. Modeling and Simulation of Autonomous Thermal Soaring with Horizon Simulation Framework. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2020 Apr 07]. Available from: https://digitalcommons.calpoly.edu/theses/442 ; 10.15368/theses.2010.205.

Council of Science Editors:

Li Z. Modeling and Simulation of Autonomous Thermal Soaring with Horizon Simulation Framework. [Masters Thesis]. Cal Poly; 2010. Available from: https://digitalcommons.calpoly.edu/theses/442 ; 10.15368/theses.2010.205


Cal Poly

21. Bryan, Jason M. GLOBAL OPTIMIZATION OF MGA-DSM PROBLEMS USING THE INTERPLANETARY GRAVITY ASSIST TRAJECTORY OPTIMIZER (IGATO).

Degree: MS, Aerospace Engineering, 2011, Cal Poly

  Interplanetary multiple gravity assist (MGA) trajectory optimization has long been a field of interest to space scientists and engineers. Gravity assist maneuvers alter a… (more)

Subjects/Keywords: Gravity assist; interplanetary trajectory; global optimization; PaGMO; MGA; Astrodynamics; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Bryan, J. M. (2011). GLOBAL OPTIMIZATION OF MGA-DSM PROBLEMS USING THE INTERPLANETARY GRAVITY ASSIST TRAJECTORY OPTIMIZER (IGATO). (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/663 ; 10.15368/theses.2011.218

Chicago Manual of Style (16th Edition):

Bryan, Jason M. “GLOBAL OPTIMIZATION OF MGA-DSM PROBLEMS USING THE INTERPLANETARY GRAVITY ASSIST TRAJECTORY OPTIMIZER (IGATO).” 2011. Masters Thesis, Cal Poly. Accessed April 07, 2020. https://digitalcommons.calpoly.edu/theses/663 ; 10.15368/theses.2011.218.

MLA Handbook (7th Edition):

Bryan, Jason M. “GLOBAL OPTIMIZATION OF MGA-DSM PROBLEMS USING THE INTERPLANETARY GRAVITY ASSIST TRAJECTORY OPTIMIZER (IGATO).” 2011. Web. 07 Apr 2020.

Vancouver:

Bryan JM. GLOBAL OPTIMIZATION OF MGA-DSM PROBLEMS USING THE INTERPLANETARY GRAVITY ASSIST TRAJECTORY OPTIMIZER (IGATO). [Internet] [Masters thesis]. Cal Poly; 2011. [cited 2020 Apr 07]. Available from: https://digitalcommons.calpoly.edu/theses/663 ; 10.15368/theses.2011.218.

Council of Science Editors:

Bryan JM. GLOBAL OPTIMIZATION OF MGA-DSM PROBLEMS USING THE INTERPLANETARY GRAVITY ASSIST TRAJECTORY OPTIMIZER (IGATO). [Masters Thesis]. Cal Poly; 2011. Available from: https://digitalcommons.calpoly.edu/theses/663 ; 10.15368/theses.2011.218


Cal Poly

22. Fujizawa, Brian T. Control Law Design and Validation for a Helicopter In-Flight Simulator.

Degree: MS, Aerospace Engineering, 2010, Cal Poly

 In-flight simulation allows one aircraft to simulate the dynamic response of another aircraft. A control system designed to give RASCAL, a JUH-60A Black Hawk helicopter… (more)

Subjects/Keywords: Helicopter; In-flight simulation; flight controls; simulation; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Fujizawa, B. T. (2010). Control Law Design and Validation for a Helicopter In-Flight Simulator. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/240 ; 10.15368/theses.2010.10

Chicago Manual of Style (16th Edition):

Fujizawa, Brian T. “Control Law Design and Validation for a Helicopter In-Flight Simulator.” 2010. Masters Thesis, Cal Poly. Accessed April 07, 2020. https://digitalcommons.calpoly.edu/theses/240 ; 10.15368/theses.2010.10.

MLA Handbook (7th Edition):

Fujizawa, Brian T. “Control Law Design and Validation for a Helicopter In-Flight Simulator.” 2010. Web. 07 Apr 2020.

Vancouver:

Fujizawa BT. Control Law Design and Validation for a Helicopter In-Flight Simulator. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2020 Apr 07]. Available from: https://digitalcommons.calpoly.edu/theses/240 ; 10.15368/theses.2010.10.

Council of Science Editors:

Fujizawa BT. Control Law Design and Validation for a Helicopter In-Flight Simulator. [Masters Thesis]. Cal Poly; 2010. Available from: https://digitalcommons.calpoly.edu/theses/240 ; 10.15368/theses.2010.10


University of Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Shupe, Nathan C. “Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object.” 2010. Masters Thesis, University of Colorado. Accessed April 07, 2020. https://scholar.colorado.edu/asen_gradetds/7.

MLA Handbook (7th Edition):

Shupe, Nathan C. “Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object.” 2010. Web. 07 Apr 2020.

Vancouver:

Shupe NC. Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object. [Internet] [Masters thesis]. University of Colorado; 2010. [cited 2020 Apr 07]. Available from: https://scholar.colorado.edu/asen_gradetds/7.

Council of Science Editors:

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


University of Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Takahashi, Yu. “Gravity Field Characterization around Small Bodies.” 2013. Doctoral Dissertation, University of Colorado. Accessed April 07, 2020. https://scholar.colorado.edu/asen_gradetds/70.

MLA Handbook (7th Edition):

Takahashi, Yu. “Gravity Field Characterization around Small Bodies.” 2013. Web. 07 Apr 2020.

Vancouver:

Takahashi Y. Gravity Field Characterization around Small Bodies. [Internet] [Doctoral dissertation]. University of Colorado; 2013. [cited 2020 Apr 07]. Available from: https://scholar.colorado.edu/asen_gradetds/70.

Council of Science Editors:

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


University of Colorado

25. Gerhardt, David Thomas. Small Satellite Passive Magnetic Attitude Control.

Degree: PhD, Aerospace Engineering Sciences, 2014, University of Colorado

  Passive Magnetic Attitude Control (PMAC) is capable of aligning a satellite within 5 degrees of the local magnetic field at low resource cost, making… (more)

Subjects/Keywords: Attitude; Determination; Magnetic; Measurement; Passive; Simulation; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Gerhardt, David Thomas. “Small Satellite Passive Magnetic Attitude Control.” 2014. Doctoral Dissertation, University of Colorado. Accessed April 07, 2020. https://scholar.colorado.edu/asen_gradetds/78.

MLA Handbook (7th Edition):

Gerhardt, David Thomas. “Small Satellite Passive Magnetic Attitude Control.” 2014. Web. 07 Apr 2020.

Vancouver:

Gerhardt DT. Small Satellite Passive Magnetic Attitude Control. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2020 Apr 07]. Available from: https://scholar.colorado.edu/asen_gradetds/78.

Council of Science Editors:

Gerhardt DT. Small Satellite Passive Magnetic Attitude Control. [Doctoral Dissertation]. University of Colorado; 2014. Available from: https://scholar.colorado.edu/asen_gradetds/78


University of Colorado

26. Dietrich, Ann Brown. Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies.

Degree: PhD, Aerospace Engineering Sciences, 2017, University of Colorado

 Spacecraft navigation in proximity to small celestial bodies, such as asteroids and comets, is challenging due to their complex dynamical environment and the lag in… (more)

Subjects/Keywords: Lidar; orbit determination; Small bodies; Aerospace Engineering; Astrodynamics; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Dietrich, A. B. (2017). Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/178

Chicago Manual of Style (16th Edition):

Dietrich, Ann Brown. “Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies.” 2017. Doctoral Dissertation, University of Colorado. Accessed April 07, 2020. https://scholar.colorado.edu/asen_gradetds/178.

MLA Handbook (7th Edition):

Dietrich, Ann Brown. “Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies.” 2017. Web. 07 Apr 2020.

Vancouver:

Dietrich AB. Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2020 Apr 07]. Available from: https://scholar.colorado.edu/asen_gradetds/178.

Council of Science Editors:

Dietrich AB. Supporting Autonomous Navigation with Flash Lidar Images in Proximity to Small Celestial Bodies. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/178


University of Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Smith, Sarah Mitchell. “Proximal Blade Twist Feedback Control for Heliogyro Solar Sails.” 2015. Masters Thesis, University of Colorado. Accessed April 07, 2020. https://scholar.colorado.edu/asen_gradetds/108.

MLA Handbook (7th Edition):

Smith, Sarah Mitchell. “Proximal Blade Twist Feedback Control for Heliogyro Solar Sails.” 2015. Web. 07 Apr 2020.

Vancouver:

Smith SM. Proximal Blade Twist Feedback Control for Heliogyro Solar Sails. [Internet] [Masters thesis]. University of Colorado; 2015. [cited 2020 Apr 07]. Available from: https://scholar.colorado.edu/asen_gradetds/108.

Council of Science Editors:

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


Grand Valley State University

28. Aryal, Milan. Object Detection, Classification, and Tracking for Autonomous Vehicle.

Degree: 2018, Grand Valley State University

 The detection and tracking of objects around an autonomous vehicle is essential to operate safely. This paper presents an algorithm to detect, classify, and track… (more)

Subjects/Keywords: Object Detection; Tracking; EKF; SLAM; YOLO; Automotive Engineering; Navigation, Guidance, Control, and Dynamics

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APA (6th Edition):

Aryal, M. (2018). Object Detection, Classification, and Tracking for Autonomous Vehicle. (Thesis). Grand Valley State University. Retrieved from https://scholarworks.gvsu.edu/theses/912

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

Chicago Manual of Style (16th Edition):

Aryal, Milan. “Object Detection, Classification, and Tracking for Autonomous Vehicle.” 2018. Thesis, Grand Valley State University. Accessed April 07, 2020. https://scholarworks.gvsu.edu/theses/912.

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

MLA Handbook (7th Edition):

Aryal, Milan. “Object Detection, Classification, and Tracking for Autonomous Vehicle.” 2018. Web. 07 Apr 2020.

Vancouver:

Aryal M. Object Detection, Classification, and Tracking for Autonomous Vehicle. [Internet] [Thesis]. Grand Valley State University; 2018. [cited 2020 Apr 07]. Available from: https://scholarworks.gvsu.edu/theses/912.

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

Council of Science Editors:

Aryal M. Object Detection, Classification, and Tracking for Autonomous Vehicle. [Thesis]. Grand Valley State University; 2018. Available from: https://scholarworks.gvsu.edu/theses/912

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


West Virginia University

29. Watson, Ryan Magnum. Enabling Robust State Estimation through Covariance Adaptation.

Degree: PhD, Mechanical and Aerospace Engineering, 2019, West Virginia University

  Several robust state estimation frameworks have been proposed over the previous decades. Underpinning all of these robust frameworks is one dubious assumption. Specifically, the… (more)

Subjects/Keywords: Robust State Estimation; Covariance Adaptation; GNSS; Factor Graph; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Watson, R. M. (2019). Enabling Robust State Estimation through Covariance Adaptation. (Doctoral Dissertation). West Virginia University. Retrieved from https://researchrepository.wvu.edu/etd/7455

Chicago Manual of Style (16th Edition):

Watson, Ryan Magnum. “Enabling Robust State Estimation through Covariance Adaptation.” 2019. Doctoral Dissertation, West Virginia University. Accessed April 07, 2020. https://researchrepository.wvu.edu/etd/7455.

MLA Handbook (7th Edition):

Watson, Ryan Magnum. “Enabling Robust State Estimation through Covariance Adaptation.” 2019. Web. 07 Apr 2020.

Vancouver:

Watson RM. Enabling Robust State Estimation through Covariance Adaptation. [Internet] [Doctoral dissertation]. West Virginia University; 2019. [cited 2020 Apr 07]. Available from: https://researchrepository.wvu.edu/etd/7455.

Council of Science Editors:

Watson RM. Enabling Robust State Estimation through Covariance Adaptation. [Doctoral Dissertation]. West Virginia University; 2019. Available from: https://researchrepository.wvu.edu/etd/7455


West Virginia University

30. Rhodes, Andrew P. Utilization of Scale in Keypoint Detection and Feature Description.

Degree: PhD, Mechanical and Aerospace Engineering, 2019, West Virginia University

  Ubiquitous availability of inexpensive three dimensional (3D) sensors has led to an abundance of keypoint detection and feature description techniques for point-clouds. While some… (more)

Subjects/Keywords: scale-space; diffusion; keypoints; feature histogram descriptor; Laplace-Beltrami; Navigation, Guidance, Control and Dynamics

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

APA (6th Edition):

Rhodes, A. P. (2019). Utilization of Scale in Keypoint Detection and Feature Description. (Doctoral Dissertation). West Virginia University. Retrieved from https://researchrepository.wvu.edu/etd/7437

Chicago Manual of Style (16th Edition):

Rhodes, Andrew P. “Utilization of Scale in Keypoint Detection and Feature Description.” 2019. Doctoral Dissertation, West Virginia University. Accessed April 07, 2020. https://researchrepository.wvu.edu/etd/7437.

MLA Handbook (7th Edition):

Rhodes, Andrew P. “Utilization of Scale in Keypoint Detection and Feature Description.” 2019. Web. 07 Apr 2020.

Vancouver:

Rhodes AP. Utilization of Scale in Keypoint Detection and Feature Description. [Internet] [Doctoral dissertation]. West Virginia University; 2019. [cited 2020 Apr 07]. Available from: https://researchrepository.wvu.edu/etd/7437.

Council of Science Editors:

Rhodes AP. Utilization of Scale in Keypoint Detection and Feature Description. [Doctoral Dissertation]. West Virginia University; 2019. Available from: https://researchrepository.wvu.edu/etd/7437

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