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You searched for +publisher:"Texas A&M University" +contributor:("Junkins, John"). Showing records 1 – 30 of 88 total matches.

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Texas A&M University

1. Roshan Suresh Kumar, FNU. Calibration of Linear Imager Camera for Relative Pose Estimation.

Degree: MS, Aerospace Engineering, 2019, Texas A&M University

 The process of camera calibration is of paramount importance in order to employ any vision based sensor for relative navigation purposes. Understanding and quantifying the… (more)

Subjects/Keywords: Camera Calibration; Linear Imager; Relative Pose Estimation; GNC; Brown's Distortion; Homography; Geometric Distortion; Relative Navigation

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APA (6th Edition):

Roshan Suresh Kumar, F. (2019). Calibration of Linear Imager Camera for Relative Pose Estimation. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/187541

Chicago Manual of Style (16th Edition):

Roshan Suresh Kumar, FNU. “Calibration of Linear Imager Camera for Relative Pose Estimation.” 2019. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/187541.

MLA Handbook (7th Edition):

Roshan Suresh Kumar, FNU. “Calibration of Linear Imager Camera for Relative Pose Estimation.” 2019. Web. 25 Feb 2021.

Vancouver:

Roshan Suresh Kumar F. Calibration of Linear Imager Camera for Relative Pose Estimation. [Internet] [Masters thesis]. Texas A&M University; 2019. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/187541.

Council of Science Editors:

Roshan Suresh Kumar F. Calibration of Linear Imager Camera for Relative Pose Estimation. [Masters Thesis]. Texas A&M University; 2019. Available from: http://hdl.handle.net/1969.1/187541


Texas A&M University

2. Schaeperkoetter, Andrew Vernon. A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques.

Degree: MS, Aerospace Engineering, 2012, Texas A&M University

 During the last two centuries many methods have been proposed to solve the angles-only initial orbit determination problem. As this problem continues to be relevant… (more)

Subjects/Keywords: Initial Orbit Determination; Gooding; Double R; Gauss; Laplace

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APA (6th Edition):

Schaeperkoetter, A. V. (2012). A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242

Chicago Manual of Style (16th Edition):

Schaeperkoetter, Andrew Vernon. “A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques.” 2012. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242.

MLA Handbook (7th Edition):

Schaeperkoetter, Andrew Vernon. “A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques.” 2012. Web. 25 Feb 2021.

Vancouver:

Schaeperkoetter AV. A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242.

Council of Science Editors:

Schaeperkoetter AV. A Comprehensive Comparison Between Angles-Only Initial Orbit Determination Techniques. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10242


Texas A&M University

3. Enkh, Mandakh. Bouquet: a Satellite Constellation Visualization Program for Walkers and Lattice Flower Constellations.

Degree: MS, Aerospace Engineering, 2011, Texas A&M University

 The development of the Flower Constellation theory offers an expanded framework to utilize constellations of satellites for tangible interests. To realize the full potential of… (more)

Subjects/Keywords: flower constellations; lattice flower constellations; satellites; walker constellations; visualization; simulation; editing; computer application; program

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APA (6th Edition):

Enkh, M. (2011). Bouquet: a Satellite Constellation Visualization Program for Walkers and Lattice Flower Constellations. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-08-10103

Chicago Manual of Style (16th Edition):

Enkh, Mandakh. “Bouquet: a Satellite Constellation Visualization Program for Walkers and Lattice Flower Constellations.” 2011. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-08-10103.

MLA Handbook (7th Edition):

Enkh, Mandakh. “Bouquet: a Satellite Constellation Visualization Program for Walkers and Lattice Flower Constellations.” 2011. Web. 25 Feb 2021.

Vancouver:

Enkh M. Bouquet: a Satellite Constellation Visualization Program for Walkers and Lattice Flower Constellations. [Internet] [Masters thesis]. Texas A&M University; 2011. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-08-10103.

Council of Science Editors:

Enkh M. Bouquet: a Satellite Constellation Visualization Program for Walkers and Lattice Flower Constellations. [Masters Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-08-10103


Texas A&M University

4. Hafer, William. Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats.

Degree: MS, Aerospace Engineering, 2012, Texas A&M University

 This thesis considers the Perspective-N-Point (PNP) problem with orthogonal target geometry, as seen in the problem of cubesat relative navigation. Cubesats are small spacecraft often… (more)

Subjects/Keywords: PNP problem; P3P problem; Known target geometry; Spacecraft relative navigation from vector measurements

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APA (6th Edition):

Hafer, W. (2012). Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10958

Chicago Manual of Style (16th Edition):

Hafer, William. “Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats.” 2012. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10958.

MLA Handbook (7th Edition):

Hafer, William. “Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats.” 2012. Web. 25 Feb 2021.

Vancouver:

Hafer W. Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10958.

Council of Science Editors:

Hafer W. Improvement of PNP Problem Computational Efficiency For Known Target Geometry of Cubesats. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10958


Texas A&M University

5. Yu, Dan. State Estimation of Spatio-Temporal Phenomena.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

 This dissertation addresses the state estimation problem of spatio-temporal phenomena which can be modeled by partial differential equations (PDEs), such as pollutant dispersion in the… (more)

Subjects/Keywords: model reduction; spatio-temporal system; sensor placement; unknown input filtering

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APA (6th Edition):

Yu, D. (2016). State Estimation of Spatio-Temporal Phenomena. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/159046

Chicago Manual of Style (16th Edition):

Yu, Dan. “State Estimation of Spatio-Temporal Phenomena.” 2016. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/159046.

MLA Handbook (7th Edition):

Yu, Dan. “State Estimation of Spatio-Temporal Phenomena.” 2016. Web. 25 Feb 2021.

Vancouver:

Yu D. State Estimation of Spatio-Temporal Phenomena. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/159046.

Council of Science Editors:

Yu D. State Estimation of Spatio-Temporal Phenomena. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/159046


Texas A&M University

6. Probe, Austin Breien. Development of a Robotic Simulation Platform for Spacecraft Proximity Operations and Contact Dynamics Experiments.

Degree: MS, Aerospace Engineering, 2013, Texas A&M University

 A major challenge facing the introduction of new technologies and techniques in space flight is the high cost required to raise the Technological Readiness Level… (more)

Subjects/Keywords: space proximity operations; contact dynamics; robotic motion emulation

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APA (6th Edition):

Probe, A. B. (2013). Development of a Robotic Simulation Platform for Spacecraft Proximity Operations and Contact Dynamics Experiments. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151932

Chicago Manual of Style (16th Edition):

Probe, Austin Breien. “Development of a Robotic Simulation Platform for Spacecraft Proximity Operations and Contact Dynamics Experiments.” 2013. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/151932.

MLA Handbook (7th Edition):

Probe, Austin Breien. “Development of a Robotic Simulation Platform for Spacecraft Proximity Operations and Contact Dynamics Experiments.” 2013. Web. 25 Feb 2021.

Vancouver:

Probe AB. Development of a Robotic Simulation Platform for Spacecraft Proximity Operations and Contact Dynamics Experiments. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/151932.

Council of Science Editors:

Probe AB. Development of a Robotic Simulation Platform for Spacecraft Proximity Operations and Contact Dynamics Experiments. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151932


Texas A&M University

7. Halder, Abhishek. Probabilistic Methods for Model Validation.

Degree: PhD, Aerospace Engineering, 2014, Texas A&M University

 This dissertation develops a probabilistic method for validation and verification (V&V) of uncertain nonlinear systems. Existing systems-control literature on model and controller V&V either deal… (more)

Subjects/Keywords: model validation; controller verification; refinement; optimal transport; Wasserstein distance; uncertainty propagation

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APA (6th Edition):

Halder, A. (2014). Probabilistic Methods for Model Validation. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152677

Chicago Manual of Style (16th Edition):

Halder, Abhishek. “Probabilistic Methods for Model Validation.” 2014. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/152677.

MLA Handbook (7th Edition):

Halder, Abhishek. “Probabilistic Methods for Model Validation.” 2014. Web. 25 Feb 2021.

Vancouver:

Halder A. Probabilistic Methods for Model Validation. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/152677.

Council of Science Editors:

Halder A. Probabilistic Methods for Model Validation. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/152677


Texas A&M University

8. Desai, Uri. A Comparative Study of Estimation Models for Satellite Relative Motion.

Degree: MS, Aerospace Engineering, 2013, Texas A&M University

 The problem of relative spacecraft motion estimation is considered with application to various reference and relative orbits. Mean circular and elliptic orbits are analyzed, with… (more)

Subjects/Keywords: relative navigation; Clohessy-Wiltshire Equations; Gim-Alfriend State Transition Matrix (GA-STM); estimation

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APA (6th Edition):

Desai, U. (2013). A Comparative Study of Estimation Models for Satellite Relative Motion. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149297

Chicago Manual of Style (16th Edition):

Desai, Uri. “A Comparative Study of Estimation Models for Satellite Relative Motion.” 2013. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/149297.

MLA Handbook (7th Edition):

Desai, Uri. “A Comparative Study of Estimation Models for Satellite Relative Motion.” 2013. Web. 25 Feb 2021.

Vancouver:

Desai U. A Comparative Study of Estimation Models for Satellite Relative Motion. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/149297.

Council of Science Editors:

Desai U. A Comparative Study of Estimation Models for Satellite Relative Motion. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149297


Texas A&M University

9. Taylor, Bradley Whitten. Experimental Investigation of Helicopter Weight and Mass Center Estimation.

Degree: MS, Aerospace Engineering, 2013, Texas A&M University

 Real-time estimates of weight and mass center location for helicopters are desirable for flight control and condition-based maintenance purposes. While methods to estimate mass parameters… (more)

Subjects/Keywords: Helicopter; Weight; Mass Center; Estimation

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APA (6th Edition):

Taylor, B. W. (2013). Experimental Investigation of Helicopter Weight and Mass Center Estimation. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149488

Chicago Manual of Style (16th Edition):

Taylor, Bradley Whitten. “Experimental Investigation of Helicopter Weight and Mass Center Estimation.” 2013. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/149488.

MLA Handbook (7th Edition):

Taylor, Bradley Whitten. “Experimental Investigation of Helicopter Weight and Mass Center Estimation.” 2013. Web. 25 Feb 2021.

Vancouver:

Taylor BW. Experimental Investigation of Helicopter Weight and Mass Center Estimation. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/149488.

Council of Science Editors:

Taylor BW. Experimental Investigation of Helicopter Weight and Mass Center Estimation. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149488


Texas A&M University

10. Kumar, Sandip. Generalized Sampling-Based Feedback Motion Planners.

Degree: PhD, Aerospace Engineering, 2012, Texas A&M University

 The motion planning problem can be formulated as a Markov decision process (MDP), if the uncertainties in the robot motion and environments can be modeled… (more)

Subjects/Keywords: Motion planning; Probabilistic RoadMaps (PRM); Semi-Markov Decision Process (SMDP); uncertainty, adaptive sampling; multi-agent motion planning problem; Multiple traveling salesman problem (MTSP); non-holonomic; heterogeneous agents; motion uncertainty; process uncertainty; collision detection; collision avoidance

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APA (6th Edition):

Kumar, S. (2012). Generalized Sampling-Based Feedback Motion Planners. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10663

Chicago Manual of Style (16th Edition):

Kumar, Sandip. “Generalized Sampling-Based Feedback Motion Planners.” 2012. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10663.

MLA Handbook (7th Edition):

Kumar, Sandip. “Generalized Sampling-Based Feedback Motion Planners.” 2012. Web. 25 Feb 2021.

Vancouver:

Kumar S. Generalized Sampling-Based Feedback Motion Planners. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10663.

Council of Science Editors:

Kumar S. Generalized Sampling-Based Feedback Motion Planners. [Doctoral Dissertation]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10663


Texas A&M University

11. Woodbury, Drew Patton. Accounting for Parameter Uncertainty in Reduced-Order Static and Dynamic Systems.

Degree: PhD, Aerospace Engineering, 2012, Texas A&M University

 Parametric uncertainty is one of many possible causes of divergence for the Kalman filter. Frequently, state estimation errors caused by imperfect model parameters are reduced… (more)

Subjects/Keywords: estimation; Kalman filter; reduced order; minimum variance filtering

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APA (6th Edition):

Woodbury, D. P. (2012). Accounting for Parameter Uncertainty in Reduced-Order Static and Dynamic Systems. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10220

Chicago Manual of Style (16th Edition):

Woodbury, Drew Patton. “Accounting for Parameter Uncertainty in Reduced-Order Static and Dynamic Systems.” 2012. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10220.

MLA Handbook (7th Edition):

Woodbury, Drew Patton. “Accounting for Parameter Uncertainty in Reduced-Order Static and Dynamic Systems.” 2012. Web. 25 Feb 2021.

Vancouver:

Woodbury DP. Accounting for Parameter Uncertainty in Reduced-Order Static and Dynamic Systems. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10220.

Council of Science Editors:

Woodbury DP. Accounting for Parameter Uncertainty in Reduced-Order Static and Dynamic Systems. [Doctoral Dissertation]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10220


Texas A&M University

12. Read, Julie Louise. Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

 The topic of this dissertation is the fusion of a novel integration method, Modified Chebyshev Picard Iteration (MCPI), with Gauss' Variational Equations using a set… (more)

Subjects/Keywords: Orbital Mechanics; Parallel Processing; Numerical Integration; Modified Chebyshev Picard Iteration; MCPI; Modified Equinoctial Elements; Chebyshev Polynomials

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APA (6th Edition):

Read, J. L. (2016). Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/159095

Chicago Manual of Style (16th Edition):

Read, Julie Louise. “Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements.” 2016. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/159095.

MLA Handbook (7th Edition):

Read, Julie Louise. “Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements.” 2016. Web. 25 Feb 2021.

Vancouver:

Read JL. Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/159095.

Council of Science Editors:

Read JL. Modified Chebyshev Picard Iteration: Integration of Perturbed Motion using Modified Equinoctial Elements. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/159095


Texas A&M University

13. Conway, Dylan Taylor. Vision-Aided Navigation: Improved Measurements Models and a Data Driven Approach.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

 Vision-aided navigation is the process of fusing data from visual cameras with other information sources to provide vehicle state estimation. Fusing information from multiple sources… (more)

Subjects/Keywords: Navigation; Computer vision; Robust estimation

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APA (6th Edition):

Conway, D. T. (2016). Vision-Aided Navigation: Improved Measurements Models and a Data Driven Approach. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/159100

Chicago Manual of Style (16th Edition):

Conway, Dylan Taylor. “Vision-Aided Navigation: Improved Measurements Models and a Data Driven Approach.” 2016. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/159100.

MLA Handbook (7th Edition):

Conway, Dylan Taylor. “Vision-Aided Navigation: Improved Measurements Models and a Data Driven Approach.” 2016. Web. 25 Feb 2021.

Vancouver:

Conway DT. Vision-Aided Navigation: Improved Measurements Models and a Data Driven Approach. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/159100.

Council of Science Editors:

Conway DT. Vision-Aided Navigation: Improved Measurements Models and a Data Driven Approach. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/159100


Texas A&M University

14. Aures-Cavalieri, Kurt D. Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense.

Degree: PhD, Aerospace Engineering, 2014, Texas A&M University

 Pursuit-evasion games reside at the intersection of game theory and optimal control theory. They are often referred to as differential games because the dynamics of… (more)

Subjects/Keywords: differential games; pursuit-evasion, game theory; estimation; optimal control; dynamic inversion; behavior learning; spacecraft rendezvous; missile defense; missile interception

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APA (6th Edition):

Aures-Cavalieri, K. D. (2014). Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154101

Chicago Manual of Style (16th Edition):

Aures-Cavalieri, Kurt D. “Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense.” 2014. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/154101.

MLA Handbook (7th Edition):

Aures-Cavalieri, Kurt D. “Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense.” 2014. Web. 25 Feb 2021.

Vancouver:

Aures-Cavalieri KD. Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/154101.

Council of Science Editors:

Aures-Cavalieri KD. Incomplete Information Pursuit-Evasion Games with Applications to Spacecraft Rendezvous and Missile Defense. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/154101


Texas A&M University

15. Satak, Neha. Behavior Learning in Differential Games and Reorientation Maneuvers.

Degree: PhD, Aerospace Engineering, 2013, Texas A&M University

 The purpose of this dissertation is to apply behavior learning concepts to incomplete-information continuous time games. Realistic game scenarios are often incomplete-information games in which… (more)

Subjects/Keywords: Differential Games; Reorientation Maneuvers; Behavior Learning

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APA (6th Edition):

Satak, N. (2013). Behavior Learning in Differential Games and Reorientation Maneuvers. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149467

Chicago Manual of Style (16th Edition):

Satak, Neha. “Behavior Learning in Differential Games and Reorientation Maneuvers.” 2013. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/149467.

MLA Handbook (7th Edition):

Satak, Neha. “Behavior Learning in Differential Games and Reorientation Maneuvers.” 2013. Web. 25 Feb 2021.

Vancouver:

Satak N. Behavior Learning in Differential Games and Reorientation Maneuvers. [Internet] [Doctoral dissertation]. Texas A&M University; 2013. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/149467.

Council of Science Editors:

Satak N. Behavior Learning in Differential Games and Reorientation Maneuvers. [Doctoral Dissertation]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149467


Texas A&M University

16. Restrepo, Carolina 1982-. An Analysis Tool for Flight Dynamics Monte Carlo Simulations.

Degree: PhD, Aerospace Engineering, 2011, Texas A&M University

 Spacecraft design is inherently difficult due to the nonlinearity of the systems involved as well as the expense of testing hardware in a realistic environment.… (more)

Subjects/Keywords: spacecraft design; nearest neighbors; kernel density estimation; guidance, navigation, and control; pattern recognition; data analysis; Monte Carlo simulation

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APA (6th Edition):

Restrepo, C. 1. (2011). An Analysis Tool for Flight Dynamics Monte Carlo Simulations. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/150935

Chicago Manual of Style (16th Edition):

Restrepo, Carolina 1982-. “An Analysis Tool for Flight Dynamics Monte Carlo Simulations.” 2011. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/150935.

MLA Handbook (7th Edition):

Restrepo, Carolina 1982-. “An Analysis Tool for Flight Dynamics Monte Carlo Simulations.” 2011. Web. 25 Feb 2021.

Vancouver:

Restrepo C1. An Analysis Tool for Flight Dynamics Monte Carlo Simulations. [Internet] [Doctoral dissertation]. Texas A&M University; 2011. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/150935.

Council of Science Editors:

Restrepo C1. An Analysis Tool for Flight Dynamics Monte Carlo Simulations. [Doctoral Dissertation]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/150935


Texas A&M University

17. Karimi, Reza. Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets.

Degree: PhD, Aerospace Engineering, 2012, Texas A&M University

 A perfect duality exists between the problem of space-based orbit determination from line-of-sight measurements and the problem of designing an interplanetary autonomous navigation system. Mathematically,… (more)

Subjects/Keywords: Initial Orbit Determination; Spacecraft Navigation; Extended Kalman Filter; Light-time correction; light Aberration

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APA (6th Edition):

Karimi, R. (2012). Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11084

Chicago Manual of Style (16th Edition):

Karimi, Reza. “Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets.” 2012. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11084.

MLA Handbook (7th Edition):

Karimi, Reza. “Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets.” 2012. Web. 25 Feb 2021.

Vancouver:

Karimi R. Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11084.

Council of Science Editors:

Karimi R. Designing An Interplanetary Autonomous Spacecraft Navigation System Using Visible Planets. [Doctoral Dissertation]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11084


Texas A&M University

18. Kumar, Mrinal. Design and Analysis of Stochastic Dynamical Systems with Fokker-Planck Equation.

Degree: PhD, Aerospace Engineering, 2011, Texas A&M University

 This dissertation addresses design and analysis aspects of stochastic dynamical systems using Fokker-Planck equation (FPE). A new numerical methodology based on the partition of unity… (more)

Subjects/Keywords: Stochastic dynamical systems; Fokker-Planck equation; Meshless finite-element methods; Nonlinear filtering; Stochastic optimal control; Partition of unity finite-element method

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APA (6th Edition):

Kumar, M. (2011). Design and Analysis of Stochastic Dynamical Systems with Fokker-Planck Equation. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7500

Chicago Manual of Style (16th Edition):

Kumar, Mrinal. “Design and Analysis of Stochastic Dynamical Systems with Fokker-Planck Equation.” 2011. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7500.

MLA Handbook (7th Edition):

Kumar, Mrinal. “Design and Analysis of Stochastic Dynamical Systems with Fokker-Planck Equation.” 2011. Web. 25 Feb 2021.

Vancouver:

Kumar M. Design and Analysis of Stochastic Dynamical Systems with Fokker-Planck Equation. [Internet] [Doctoral dissertation]. Texas A&M University; 2011. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7500.

Council of Science Editors:

Kumar M. Design and Analysis of Stochastic Dynamical Systems with Fokker-Planck Equation. [Doctoral Dissertation]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7500


Texas A&M University

19. Macomber, Brent David. Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems.

Degree: PhD, Aerospace Engineering, 2015, Texas A&M University

 Modified Chebyshev Picard Iteration (MCPI) is an iterative numerical method for solution of Ordinary Differential Equations (ODEs). This dissertation presents a body of work that… (more)

Subjects/Keywords: Numerical Methods; Ordinary Differential Equations; Parallel Computing; Orbit Propagation; Space Situational Awareness

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APA (6th Edition):

Macomber, B. D. (2015). Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/155745

Chicago Manual of Style (16th Edition):

Macomber, Brent David. “Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems.” 2015. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/155745.

MLA Handbook (7th Edition):

Macomber, Brent David. “Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems.” 2015. Web. 25 Feb 2021.

Vancouver:

Macomber BD. Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems. [Internet] [Doctoral dissertation]. Texas A&M University; 2015. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/155745.

Council of Science Editors:

Macomber BD. Enhancements to Chebyshev-Picard Iteration Efficiency for Generally Perturbed Orbits and Constrained Dynamical Systems. [Doctoral Dissertation]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/155745


Texas A&M University

20. Aghamohammadi, Aliakbar. Feedback-based Information Roadmap (FIRM): Graph-based Estimation and Control of Robotic Systems Under Uncertainty.

Degree: PhD, Computer Engineering, 2014, Texas A&M University

 This dissertation addresses the problem of stochastic optimal control with imperfect measurements. The main application of interest is robot motion planning under uncertainty. In the… (more)

Subjects/Keywords: Motion Planning; Stochastic Control; POMDP; Information; FIRM; Feedback-based Information Roadmap; belief; Robot

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APA (6th Edition):

Aghamohammadi, A. (2014). Feedback-based Information Roadmap (FIRM): Graph-based Estimation and Control of Robotic Systems Under Uncertainty. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152857

Chicago Manual of Style (16th Edition):

Aghamohammadi, Aliakbar. “Feedback-based Information Roadmap (FIRM): Graph-based Estimation and Control of Robotic Systems Under Uncertainty.” 2014. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/152857.

MLA Handbook (7th Edition):

Aghamohammadi, Aliakbar. “Feedback-based Information Roadmap (FIRM): Graph-based Estimation and Control of Robotic Systems Under Uncertainty.” 2014. Web. 25 Feb 2021.

Vancouver:

Aghamohammadi A. Feedback-based Information Roadmap (FIRM): Graph-based Estimation and Control of Robotic Systems Under Uncertainty. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/152857.

Council of Science Editors:

Aghamohammadi A. Feedback-based Information Roadmap (FIRM): Graph-based Estimation and Control of Robotic Systems Under Uncertainty. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/152857

21. Whitten, William Daniel. Improving the Robustness of Monocular Vision-Aided Navigation for Multirotors through Integrated Estimation and Guidance.

Degree: MS, Aerospace Engineering, 2017, Texas A&M University

 Multirotors could be used to autonomously perform tasks in search-and-rescue, reconnaissance, or infrastructure-monitoring applications. In these environments, the vehicle may have limited or degraded GPS… (more)

Subjects/Keywords: Simultaneous Localization and Mapping; SLAM; monocular; camera; aerospace; engineering; computer vision; estimation; navigation; drone; quadcopter; autonomous; guidance; inertial measurement unit; IMU; robotics; images

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APA (6th Edition):

Whitten, W. D. (2017). Improving the Robustness of Monocular Vision-Aided Navigation for Multirotors through Integrated Estimation and Guidance. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/161526

Chicago Manual of Style (16th Edition):

Whitten, William Daniel. “Improving the Robustness of Monocular Vision-Aided Navigation for Multirotors through Integrated Estimation and Guidance.” 2017. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/161526.

MLA Handbook (7th Edition):

Whitten, William Daniel. “Improving the Robustness of Monocular Vision-Aided Navigation for Multirotors through Integrated Estimation and Guidance.” 2017. Web. 25 Feb 2021.

Vancouver:

Whitten WD. Improving the Robustness of Monocular Vision-Aided Navigation for Multirotors through Integrated Estimation and Guidance. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/161526.

Council of Science Editors:

Whitten WD. Improving the Robustness of Monocular Vision-Aided Navigation for Multirotors through Integrated Estimation and Guidance. [Masters Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/161526

22. Davis, Jeremy John. Constellation Reconfiguration: Tools and Analysis.

Degree: PhD, Aerospace Engineering, 2011, Texas A&M University

 Constellation reconfi guration consists of transforming an initial constellation of satellites into some final constellation of satellites to maintain system optimality. Constellations with phased deployment,… (more)

Subjects/Keywords: constellation design; constellation reconfiguration; satellite constellation; orbit design; Kepler's equation

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APA (6th Edition):

Davis, J. J. (2011). Constellation Reconfiguration: Tools and Analysis. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8325

Chicago Manual of Style (16th Edition):

Davis, Jeremy John. “Constellation Reconfiguration: Tools and Analysis.” 2011. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8325.

MLA Handbook (7th Edition):

Davis, Jeremy John. “Constellation Reconfiguration: Tools and Analysis.” 2011. Web. 25 Feb 2021.

Vancouver:

Davis JJ. Constellation Reconfiguration: Tools and Analysis. [Internet] [Doctoral dissertation]. Texas A&M University; 2011. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8325.

Council of Science Editors:

Davis JJ. Constellation Reconfiguration: Tools and Analysis. [Doctoral Dissertation]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8325

23. Harris, Matthew Wade. Extremal Fields and Neighboring Optimal Control of Constrained Systems.

Degree: MS, Aerospace Engineering, 2012, Texas A&M University

 This work provides first and second-order expressions to approximate neighboring solutions to the m-point boundary value problem. Multi-point problems arise in optimal control because of… (more)

Subjects/Keywords: extremal field; neighboring optimal control

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

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APA (6th Edition):

Harris, M. W. (2012). Extremal Fields and Neighboring Optimal Control of Constrained Systems. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8748

Chicago Manual of Style (16th Edition):

Harris, Matthew Wade. “Extremal Fields and Neighboring Optimal Control of Constrained Systems.” 2012. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8748.

MLA Handbook (7th Edition):

Harris, Matthew Wade. “Extremal Fields and Neighboring Optimal Control of Constrained Systems.” 2012. Web. 25 Feb 2021.

Vancouver:

Harris MW. Extremal Fields and Neighboring Optimal Control of Constrained Systems. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8748.

Council of Science Editors:

Harris MW. Extremal Fields and Neighboring Optimal Control of Constrained Systems. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8748

24. Missel, Jonathan William. Active Space Debris Removal using Capture and Ejection.

Degree: PhD, Aerospace Engineering, 2013, Texas A&M University

 Low Earth Orbit is over-cluttered with rogue objects that threaten existing technological assets and interfere with allocating new ones. Traditional satellite missions are not efficient… (more)

Subjects/Keywords: Active; space; debris; removal; Sling-sat; sweeper

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APA (6th Edition):

Missel, J. W. (2013). Active Space Debris Removal using Capture and Ejection. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149391

Chicago Manual of Style (16th Edition):

Missel, Jonathan William. “Active Space Debris Removal using Capture and Ejection.” 2013. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/149391.

MLA Handbook (7th Edition):

Missel, Jonathan William. “Active Space Debris Removal using Capture and Ejection.” 2013. Web. 25 Feb 2021.

Vancouver:

Missel JW. Active Space Debris Removal using Capture and Ejection. [Internet] [Doctoral dissertation]. Texas A&M University; 2013. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/149391.

Council of Science Editors:

Missel JW. Active Space Debris Removal using Capture and Ejection. [Doctoral Dissertation]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149391

25. Aures-Cavalieri, Kurt Dale. Implementing Feedback Control on a Novel Proximity Operations Simulation Platform.

Degree: MS, Aerospace Engineering, 2012, Texas A&M University

 Recently, The Land, Air and Space Robotics (LASR) Laboratory has demonstrated a state-of-the-art proximity operations test bed that will revolutionize the concept of portable space… (more)

Subjects/Keywords: feedback control; simulation; space systems; robotics

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APA (6th Edition):

Aures-Cavalieri, K. D. (2012). Implementing Feedback Control on a Novel Proximity Operations Simulation Platform. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9406

Chicago Manual of Style (16th Edition):

Aures-Cavalieri, Kurt Dale. “Implementing Feedback Control on a Novel Proximity Operations Simulation Platform.” 2012. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9406.

MLA Handbook (7th Edition):

Aures-Cavalieri, Kurt Dale. “Implementing Feedback Control on a Novel Proximity Operations Simulation Platform.” 2012. Web. 25 Feb 2021.

Vancouver:

Aures-Cavalieri KD. Implementing Feedback Control on a Novel Proximity Operations Simulation Platform. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9406.

Council of Science Editors:

Aures-Cavalieri KD. Implementing Feedback Control on a Novel Proximity Operations Simulation Platform. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9406

26. Flewelling, Brien Roy. 3D Multi-Field Multi-Scale Features From Range Data In Spacecraft Proximity Operations.

Degree: PhD, Aerospace Engineering, 2012, Texas A&M University

 A fundamental problem in spacecraft proximity operations is the determination of the 6 degree of freedom relative navigation solution between the observer reference frame and… (more)

Subjects/Keywords: Scale Space; Image Processing; LIDAR; Range Sensing; Sensor Fusion; Feature Detection; Relative-Navigation; Vision

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APA (6th Edition):

Flewelling, B. R. (2012). 3D Multi-Field Multi-Scale Features From Range Data In Spacecraft Proximity Operations. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11105

Chicago Manual of Style (16th Edition):

Flewelling, Brien Roy. “3D Multi-Field Multi-Scale Features From Range Data In Spacecraft Proximity Operations.” 2012. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11105.

MLA Handbook (7th Edition):

Flewelling, Brien Roy. “3D Multi-Field Multi-Scale Features From Range Data In Spacecraft Proximity Operations.” 2012. Web. 25 Feb 2021.

Vancouver:

Flewelling BR. 3D Multi-Field Multi-Scale Features From Range Data In Spacecraft Proximity Operations. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11105.

Council of Science Editors:

Flewelling BR. 3D Multi-Field Multi-Scale Features From Range Data In Spacecraft Proximity Operations. [Doctoral Dissertation]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-11105

27. Biggers, Keith Edward. Inference-based Geometric Modeling for the Generation of Complex Cluttered Virtual Environments.

Degree: PhD, Computer Science, 2012, Texas A&M University

 As the use of simulation increases across many diff erent application domains, the need for high- fidelity three-dimensional virtual representations of real-world environments has never… (more)

Subjects/Keywords: Surface Reconstruction; Generative Modeling; Solid Modeling; Complex Cluttered Virtual Environments

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APA (6th Edition):

Biggers, K. E. (2012). Inference-based Geometric Modeling for the Generation of Complex Cluttered Virtual Environments. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9209

Chicago Manual of Style (16th Edition):

Biggers, Keith Edward. “Inference-based Geometric Modeling for the Generation of Complex Cluttered Virtual Environments.” 2012. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9209.

MLA Handbook (7th Edition):

Biggers, Keith Edward. “Inference-based Geometric Modeling for the Generation of Complex Cluttered Virtual Environments.” 2012. Web. 25 Feb 2021.

Vancouver:

Biggers KE. Inference-based Geometric Modeling for the Generation of Complex Cluttered Virtual Environments. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9209.

Council of Science Editors:

Biggers KE. Inference-based Geometric Modeling for the Generation of Complex Cluttered Virtual Environments. [Doctoral Dissertation]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9209

28. Masher, Abhay Hiren. Control of Active Pendulum for Contact Dynamics Simulation.

Degree: MS, Aerospace Engineering, 2016, Texas A&M University

 Space proximity missions essentially need on the ground hardware in the loop (HIL) testing of sensors, algorithms, and actuators. Such testing would surpass that of… (more)

Subjects/Keywords: proximity operations; contact dynamics; nonlinear control; underactuated; cart-pole

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APA (6th Edition):

Masher, A. H. (2016). Control of Active Pendulum for Contact Dynamics Simulation. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/158669

Chicago Manual of Style (16th Edition):

Masher, Abhay Hiren. “Control of Active Pendulum for Contact Dynamics Simulation.” 2016. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/158669.

MLA Handbook (7th Edition):

Masher, Abhay Hiren. “Control of Active Pendulum for Contact Dynamics Simulation.” 2016. Web. 25 Feb 2021.

Vancouver:

Masher AH. Control of Active Pendulum for Contact Dynamics Simulation. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/158669.

Council of Science Editors:

Masher AH. Control of Active Pendulum for Contact Dynamics Simulation. [Masters Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/158669

29. Kaushik, Arvind Shankar. A Statistical Comparison Between Gibbs and Herrick-Gibbs Orbit Determination Methods.

Degree: MS, Aerospace Engineering, 2016, Texas A&M University

 The detection, tracking, identification, and characterization (DTIC) of resident space objects (RSOs) is an important aspect of space situational awareness (SSA). Monitoring the space environment… (more)

Subjects/Keywords: Orbit Determination; Gibbs; Herrick-Gibbs; IOD; Space Situational Awareness

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APA (6th Edition):

Kaushik, A. S. (2016). A Statistical Comparison Between Gibbs and Herrick-Gibbs Orbit Determination Methods. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/157747

Chicago Manual of Style (16th Edition):

Kaushik, Arvind Shankar. “A Statistical Comparison Between Gibbs and Herrick-Gibbs Orbit Determination Methods.” 2016. Masters Thesis, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/157747.

MLA Handbook (7th Edition):

Kaushik, Arvind Shankar. “A Statistical Comparison Between Gibbs and Herrick-Gibbs Orbit Determination Methods.” 2016. Web. 25 Feb 2021.

Vancouver:

Kaushik AS. A Statistical Comparison Between Gibbs and Herrick-Gibbs Orbit Determination Methods. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/157747.

Council of Science Editors:

Kaushik AS. A Statistical Comparison Between Gibbs and Herrick-Gibbs Orbit Determination Methods. [Masters Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/157747

30. Katake, Anup Bharat. Modeling, image processing and attitude estimation of high speed star sensors.

Degree: PhD, Aerospace Engineering, 2009, Texas A&M University

 Attitude estimation and angular velocity estimation are the most critical components of a spacecraft's guidance, navigation and control. Usually, an array of tightlycoupled sensors (star… (more)

Subjects/Keywords: star trackers; stellar gyroscope; recentroiding; attitude determination; image intensification

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APA (6th Edition):

Katake, A. B. (2009). Modeling, image processing and attitude estimation of high speed star sensors. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1018

Chicago Manual of Style (16th Edition):

Katake, Anup Bharat. “Modeling, image processing and attitude estimation of high speed star sensors.” 2009. Doctoral Dissertation, Texas A&M University. Accessed February 25, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-1018.

MLA Handbook (7th Edition):

Katake, Anup Bharat. “Modeling, image processing and attitude estimation of high speed star sensors.” 2009. Web. 25 Feb 2021.

Vancouver:

Katake AB. Modeling, image processing and attitude estimation of high speed star sensors. [Internet] [Doctoral dissertation]. Texas A&M University; 2009. [cited 2021 Feb 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1018.

Council of Science Editors:

Katake AB. Modeling, image processing and attitude estimation of high speed star sensors. [Doctoral Dissertation]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1018

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