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You searched for +publisher:"Texas A&M University" +contributor:("Alfriend, Kyle T."). Showing records 1 – 10 of 10 total matches.

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Texas A&M University

1. Mahajan, Bharat. Absolute and Relative Motion Satellite Theories for Zonal and Tesseral Gravitational Harmonics.

Degree: PhD, Aerospace Engineering, 2018, Texas A&M University

 In 1959, Dirk Brouwer pioneered the use of the Hamiltonian perturbation methods for constructing artificial satellite theories with effects due to nonspherical gravitational perturbations included.… (more)

Subjects/Keywords: Artificial Satellite Theories; Zonal and Tesseral Spherical Harmonics; Canonical Perturbation Methods; Satellite Relative Motion; Formation Flying; Relative Motion STM; Perturbed Lambert Solver; Formation Drift Mitigation

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APA (6th Edition):

Mahajan, B. (2018). Absolute and Relative Motion Satellite Theories for Zonal and Tesseral Gravitational Harmonics. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/173295

Chicago Manual of Style (16th Edition):

Mahajan, Bharat. “Absolute and Relative Motion Satellite Theories for Zonal and Tesseral Gravitational Harmonics.” 2018. Doctoral Dissertation, Texas A&M University. Accessed April 14, 2021. http://hdl.handle.net/1969.1/173295.

MLA Handbook (7th Edition):

Mahajan, Bharat. “Absolute and Relative Motion Satellite Theories for Zonal and Tesseral Gravitational Harmonics.” 2018. Web. 14 Apr 2021.

Vancouver:

Mahajan B. Absolute and Relative Motion Satellite Theories for Zonal and Tesseral Gravitational Harmonics. [Internet] [Doctoral dissertation]. Texas A&M University; 2018. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1969.1/173295.

Council of Science Editors:

Mahajan B. Absolute and Relative Motion Satellite Theories for Zonal and Tesseral Gravitational Harmonics. [Doctoral Dissertation]. Texas A&M University; 2018. Available from: http://hdl.handle.net/1969.1/173295


Texas A&M University

2. Johnson, Kirk Wayne. Approaches for Modeling Satellite Relative Motion.

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

 This dissertation explores new approaches for modeling perturbed and unperturbed satellite relative motion. It extends Hoots orbit theory, an analytical averaging-method perturbation solution to the… (more)

Subjects/Keywords: Satellite Relative Motion; Satellite Formation Flying; Zonal Problem; Astrodynamics

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APA (6th Edition):

Johnson, K. W. (2016). Approaches for Modeling Satellite Relative Motion. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/158945

Chicago Manual of Style (16th Edition):

Johnson, Kirk Wayne. “Approaches for Modeling Satellite Relative Motion.” 2016. Doctoral Dissertation, Texas A&M University. Accessed April 14, 2021. http://hdl.handle.net/1969.1/158945.

MLA Handbook (7th Edition):

Johnson, Kirk Wayne. “Approaches for Modeling Satellite Relative Motion.” 2016. Web. 14 Apr 2021.

Vancouver:

Johnson KW. Approaches for Modeling Satellite Relative Motion. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1969.1/158945.

Council of Science Editors:

Johnson KW. Approaches for Modeling Satellite Relative Motion. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/158945


Texas A&M University

3. Weisman, Ryan Michael 1984-. Nonlinear Transformations and Filtering Theory for Space Operations.

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

 Decisions for asset allocation and protection are predicated upon accurate knowledge of the current operating environment as well as correctly characterizing the evolution of the… (more)

Subjects/Keywords: filter initialization; uncertainty estimation; bayesian filtering; nonlinear estimation; space surveillance

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APA (6th Edition):

Weisman, R. M. 1. (2012). Nonlinear Transformations and Filtering Theory for Space Operations. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148211

Chicago Manual of Style (16th Edition):

Weisman, Ryan Michael 1984-. “Nonlinear Transformations and Filtering Theory for Space Operations.” 2012. Doctoral Dissertation, Texas A&M University. Accessed April 14, 2021. http://hdl.handle.net/1969.1/148211.

MLA Handbook (7th Edition):

Weisman, Ryan Michael 1984-. “Nonlinear Transformations and Filtering Theory for Space Operations.” 2012. Web. 14 Apr 2021.

Vancouver:

Weisman RM1. Nonlinear Transformations and Filtering Theory for Space Operations. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1969.1/148211.

Council of Science Editors:

Weisman RM1. Nonlinear Transformations and Filtering Theory for Space Operations. [Doctoral Dissertation]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148211

4. Roscoe, Christopher. Satellite Formation Design in Orbits of High Eccentricity for Missions with Performance Criteria Specified over a Region of Interest.

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

 Several methods are presented for the design of satellite formations for science missions in high-eccentricity reference orbits with quantifiable performance criteria specified throughout only a… (more)

Subjects/Keywords: Third-Body Perturbation; Orbital Elements; Magnetospheric Multiscale; Robust; Formation Flying; Astrodynamics

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APA (6th Edition):

Roscoe, C. (2012). Satellite Formation Design in Orbits of High Eccentricity for Missions with Performance Criteria Specified over a Region of Interest. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148360

Chicago Manual of Style (16th Edition):

Roscoe, Christopher. “Satellite Formation Design in Orbits of High Eccentricity for Missions with Performance Criteria Specified over a Region of Interest.” 2012. Doctoral Dissertation, Texas A&M University. Accessed April 14, 2021. http://hdl.handle.net/1969.1/148360.

MLA Handbook (7th Edition):

Roscoe, Christopher. “Satellite Formation Design in Orbits of High Eccentricity for Missions with Performance Criteria Specified over a Region of Interest.” 2012. Web. 14 Apr 2021.

Vancouver:

Roscoe C. Satellite Formation Design in Orbits of High Eccentricity for Missions with Performance Criteria Specified over a Region of Interest. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1969.1/148360.

Council of Science Editors:

Roscoe C. Satellite Formation Design in Orbits of High Eccentricity for Missions with Performance Criteria Specified over a Region of Interest. [Doctoral Dissertation]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148360


Texas A&M University

5. Vaddi, Veera Venkata Sesha Sai. Modelling and control of satellite formations.

Degree: PhD, Aerospace Engineering, 2004, Texas A&M University

 Formation flying is a new paradigm in space mission design, aimed at replacing large satellites with multiple small satellites. Some of the proposed benefits of… (more)

Subjects/Keywords: Formation Flying; Spacecraft Control

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APA (6th Edition):

Vaddi, V. V. S. S. (2004). Modelling and control of satellite formations. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/329

Chicago Manual of Style (16th Edition):

Vaddi, Veera Venkata Sesha Sai. “Modelling and control of satellite formations.” 2004. Doctoral Dissertation, Texas A&M University. Accessed April 14, 2021. http://hdl.handle.net/1969.1/329.

MLA Handbook (7th Edition):

Vaddi, Veera Venkata Sesha Sai. “Modelling and control of satellite formations.” 2004. Web. 14 Apr 2021.

Vancouver:

Vaddi VVSS. Modelling and control of satellite formations. [Internet] [Doctoral dissertation]. Texas A&M University; 2004. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1969.1/329.

Council of Science Editors:

Vaddi VVSS. Modelling and control of satellite formations. [Doctoral Dissertation]. Texas A&M University; 2004. Available from: http://hdl.handle.net/1969.1/329


Texas A&M University

6. Sengupta, Prasenjit. Satellite relative motion propagation and control in the presence of J2 perturbations.

Degree: MS, Aerospace Engineering, 2004, Texas A&M University

 Formation flying is a new satellite mission concept that is concerned with clusters of satellites in neighboring orbits cooperating to perform a specific task. The… (more)

Subjects/Keywords: Satellite Formations; J2; Relative Motion

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APA (6th Edition):

Sengupta, P. (2004). Satellite relative motion propagation and control in the presence of J2 perturbations. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/518

Chicago Manual of Style (16th Edition):

Sengupta, Prasenjit. “Satellite relative motion propagation and control in the presence of J2 perturbations.” 2004. Masters Thesis, Texas A&M University. Accessed April 14, 2021. http://hdl.handle.net/1969.1/518.

MLA Handbook (7th Edition):

Sengupta, Prasenjit. “Satellite relative motion propagation and control in the presence of J2 perturbations.” 2004. Web. 14 Apr 2021.

Vancouver:

Sengupta P. Satellite relative motion propagation and control in the presence of J2 perturbations. [Internet] [Masters thesis]. Texas A&M University; 2004. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1969.1/518.

Council of Science Editors:

Sengupta P. Satellite relative motion propagation and control in the presence of J2 perturbations. [Masters Thesis]. Texas A&M University; 2004. Available from: http://hdl.handle.net/1969.1/518


Texas A&M University

7. Lee, Deok-Jin. Nonlinear bayesian filtering with applications to estimation and navigation.

Degree: PhD, Aerospace Engineering, 2005, Texas A&M University

 In principle, general approaches to optimal nonlinear filtering can be described in a unified way from the recursive Bayesian approach. The central idea to this… (more)

Subjects/Keywords: statistical nonlinear filtering; estimation and navigation; Bayesian filter

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APA (6th Edition):

Lee, D. (2005). Nonlinear bayesian filtering with applications to estimation and navigation. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/2269

Chicago Manual of Style (16th Edition):

Lee, Deok-Jin. “Nonlinear bayesian filtering with applications to estimation and navigation.” 2005. Doctoral Dissertation, Texas A&M University. Accessed April 14, 2021. http://hdl.handle.net/1969.1/2269.

MLA Handbook (7th Edition):

Lee, Deok-Jin. “Nonlinear bayesian filtering with applications to estimation and navigation.” 2005. Web. 14 Apr 2021.

Vancouver:

Lee D. Nonlinear bayesian filtering with applications to estimation and navigation. [Internet] [Doctoral dissertation]. Texas A&M University; 2005. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1969.1/2269.

Council of Science Editors:

Lee D. Nonlinear bayesian filtering with applications to estimation and navigation. [Doctoral Dissertation]. Texas A&M University; 2005. Available from: http://hdl.handle.net/1969.1/2269


Texas A&M University

8. Yan, Hui. Dynamics and real-time optimal control of satellite attitude and satellite formation systems.

Degree: PhD, Aerospace Engineering, 2006, Texas A&M University

 In this dissertation the solutions of the dynamics and real-time optimal control of magnetic attitude control and formation flying systems are presented. In magnetic attitude… (more)

Subjects/Keywords: Optimal Control; Real-Time; Formation Flying; Magnetic Attitude Control; Pseudospectral Methods

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APA (6th Edition):

Yan, H. (2006). Dynamics and real-time optimal control of satellite attitude and satellite formation systems. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/4283

Chicago Manual of Style (16th Edition):

Yan, Hui. “Dynamics and real-time optimal control of satellite attitude and satellite formation systems.” 2006. Doctoral Dissertation, Texas A&M University. Accessed April 14, 2021. http://hdl.handle.net/1969.1/4283.

MLA Handbook (7th Edition):

Yan, Hui. “Dynamics and real-time optimal control of satellite attitude and satellite formation systems.” 2006. Web. 14 Apr 2021.

Vancouver:

Yan H. Dynamics and real-time optimal control of satellite attitude and satellite formation systems. [Internet] [Doctoral dissertation]. Texas A&M University; 2006. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1969.1/4283.

Council of Science Editors:

Yan H. Dynamics and real-time optimal control of satellite attitude and satellite formation systems. [Doctoral Dissertation]. Texas A&M University; 2006. Available from: http://hdl.handle.net/1969.1/4283


Texas A&M University

9. Wilkins, Matthew Paul. The Flower Constellations - theory, design process, and applications.

Degree: PhD, Aerospace Engineering, 2006, Texas A&M University

 In this research, constellations of satellites all having orbits compatible with rotating reference frames are considered. That is to say, no matter how many satellites… (more)

Subjects/Keywords: Satellites; Constellations; Formations; Design

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APA (6th Edition):

Wilkins, M. P. (2006). The Flower Constellations - theory, design process, and applications. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/3053

Chicago Manual of Style (16th Edition):

Wilkins, Matthew Paul. “The Flower Constellations - theory, design process, and applications.” 2006. Doctoral Dissertation, Texas A&M University. Accessed April 14, 2021. http://hdl.handle.net/1969.1/3053.

MLA Handbook (7th Edition):

Wilkins, Matthew Paul. “The Flower Constellations - theory, design process, and applications.” 2006. Web. 14 Apr 2021.

Vancouver:

Wilkins MP. The Flower Constellations - theory, design process, and applications. [Internet] [Doctoral dissertation]. Texas A&M University; 2006. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1969.1/3053.

Council of Science Editors:

Wilkins MP. The Flower Constellations - theory, design process, and applications. [Doctoral Dissertation]. Texas A&M University; 2006. Available from: http://hdl.handle.net/1969.1/3053


Texas A&M University

10. Sengupta, Prasenjit. Dynamics and control of satellite relative motion in a central gravitational field.

Degree: PhD, Aerospace Engineering, 2007, Texas A&M University

 The study of satellite relative motion has been of great historic interest, primarily due to its application to rendezvous, intercept, and docking maneuvers, between spacecraft… (more)

Subjects/Keywords: Relative Motion; Rendezvous; Formation Flight; J2

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APA (6th Edition):

Sengupta, P. (2007). Dynamics and control of satellite relative motion in a central gravitational field. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/4724

Chicago Manual of Style (16th Edition):

Sengupta, Prasenjit. “Dynamics and control of satellite relative motion in a central gravitational field.” 2007. Doctoral Dissertation, Texas A&M University. Accessed April 14, 2021. http://hdl.handle.net/1969.1/4724.

MLA Handbook (7th Edition):

Sengupta, Prasenjit. “Dynamics and control of satellite relative motion in a central gravitational field.” 2007. Web. 14 Apr 2021.

Vancouver:

Sengupta P. Dynamics and control of satellite relative motion in a central gravitational field. [Internet] [Doctoral dissertation]. Texas A&M University; 2007. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1969.1/4724.

Council of Science Editors:

Sengupta P. Dynamics and control of satellite relative motion in a central gravitational field. [Doctoral Dissertation]. Texas A&M University; 2007. Available from: http://hdl.handle.net/1969.1/4724

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