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You searched for +publisher:"University of Illinois – Urbana-Champaign" +contributor:("Conway, Bruce A."). Showing records 1 – 12 of 12 total matches.

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University of Illinois – Urbana-Champaign

1. Stanley, Aishwarya. Identifying near-earth asteroid targets for human exploration using particle swarm optimization.

Degree: MS, 4048, 2013, University of Illinois – Urbana-Champaign

 The goal of this thesis is to identify potential Near-Earth Asteroids (NEAs) that are viable candidates for human exploration. The computational method incorporated to help… (more)

Subjects/Keywords: Near-Earth Asteroids; Particle Swarm Optimization

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APA (6th Edition):

Stanley, A. (2013). Identifying near-earth asteroid targets for human exploration using particle swarm optimization. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/44435

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):

Stanley, Aishwarya. “Identifying near-earth asteroid targets for human exploration using particle swarm optimization.” 2013. Thesis, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/44435.

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

MLA Handbook (7th Edition):

Stanley, Aishwarya. “Identifying near-earth asteroid targets for human exploration using particle swarm optimization.” 2013. Web. 06 Apr 2020.

Vancouver:

Stanley A. Identifying near-earth asteroid targets for human exploration using particle swarm optimization. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2013. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/44435.

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

Council of Science Editors:

Stanley A. Identifying near-earth asteroid targets for human exploration using particle swarm optimization. [Thesis]. University of Illinois – Urbana-Champaign; 2013. Available from: http://hdl.handle.net/2142/44435

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


University of Illinois – Urbana-Champaign

2. De La Mata, Jorge. Optimal strategies for selecting from multiple asteroid interception targets.

Degree: MS, 4048, 2014, University of Illinois – Urbana-Champaign

 The goal of this thesis is to demonstrate the applicability of the discrimination time optimization problem to space systems. The concept is applied to an… (more)

Subjects/Keywords: Astrodynamics; Orbital Mechanics; Optimization; Nonlinear Programming; Space; Aerospace; Optimal trajectories; Controls

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APA (6th Edition):

De La Mata, J. (2014). Optimal strategies for selecting from multiple asteroid interception targets. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/50647

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):

De La Mata, Jorge. “Optimal strategies for selecting from multiple asteroid interception targets.” 2014. Thesis, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/50647.

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

MLA Handbook (7th Edition):

De La Mata, Jorge. “Optimal strategies for selecting from multiple asteroid interception targets.” 2014. Web. 06 Apr 2020.

Vancouver:

De La Mata J. Optimal strategies for selecting from multiple asteroid interception targets. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2014. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/50647.

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

Council of Science Editors:

De La Mata J. Optimal strategies for selecting from multiple asteroid interception targets. [Thesis]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/50647

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


University of Illinois – Urbana-Champaign

3. Ghosh, Alexander. Multi-CubeSat mission planning enabled through parallel computing.

Degree: PhD, 4048, 2013, University of Illinois – Urbana-Champaign

 Small CubeSat-class satellites are opening up new avenues for science and technology development within the space industry. What was once a purely educational tool has… (more)

Subjects/Keywords: satellite; trajectory; trajectory optimization; optimization; cubesat; picosatellite; earth orbit; Orbit; low thrust; low-thrust; automatic differentiation; algorithmic differentiation; parallel processing

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APA (6th Edition):

Ghosh, A. (2013). Multi-CubeSat mission planning enabled through parallel computing. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/45554

Chicago Manual of Style (16th Edition):

Ghosh, Alexander. “Multi-CubeSat mission planning enabled through parallel computing.” 2013. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/45554.

MLA Handbook (7th Edition):

Ghosh, Alexander. “Multi-CubeSat mission planning enabled through parallel computing.” 2013. Web. 06 Apr 2020.

Vancouver:

Ghosh A. Multi-CubeSat mission planning enabled through parallel computing. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2013. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/45554.

Council of Science Editors:

Ghosh A. Multi-CubeSat mission planning enabled through parallel computing. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2013. Available from: http://hdl.handle.net/2142/45554


University of Illinois – Urbana-Champaign

4. Morgan, Daniel James. Guidance and control of swarms of spacecraft.

Degree: PhD, Aerospace Engineering, 2015, University of Illinois – Urbana-Champaign

 There has been considerable interest in formation flying spacecraft due to their potential to perform certain tasks at a cheaper cost than monolithic spacecraft. Formation… (more)

Subjects/Keywords: swarms of spacecraft; sequential convex programming; model predictive control

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APA (6th Edition):

Morgan, D. J. (2015). Guidance and control of swarms of spacecraft. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/78367

Chicago Manual of Style (16th Edition):

Morgan, Daniel James. “Guidance and control of swarms of spacecraft.” 2015. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/78367.

MLA Handbook (7th Edition):

Morgan, Daniel James. “Guidance and control of swarms of spacecraft.” 2015. Web. 06 Apr 2020.

Vancouver:

Morgan DJ. Guidance and control of swarms of spacecraft. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2015. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/78367.

Council of Science Editors:

Morgan DJ. Guidance and control of swarms of spacecraft. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2015. Available from: http://hdl.handle.net/2142/78367

5. Stupik, Joan. Optimal pursuit/evasion spacecraft trajectories in the hill reference frame.

Degree: MS, 4048, 2013, University of Illinois – Urbana-Champaign

 The pursuit/evasion game for two spacecraft is significantly simplified by being described with a linearized system of equations of motion. A pursuit/evasion game is also… (more)

Subjects/Keywords: pursuit/evasion; Hill frame; Optimal trajectories; spacecraft; kriging; particle swarm optimization; Hill-Clohessy-Wiltshire (HCW); differential game; low-thrust propulsion

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APA (6th Edition):

Stupik, J. (2013). Optimal pursuit/evasion spacecraft trajectories in the hill reference frame. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/44224

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):

Stupik, Joan. “Optimal pursuit/evasion spacecraft trajectories in the hill reference frame.” 2013. Thesis, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/44224.

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

MLA Handbook (7th Edition):

Stupik, Joan. “Optimal pursuit/evasion spacecraft trajectories in the hill reference frame.” 2013. Web. 06 Apr 2020.

Vancouver:

Stupik J. Optimal pursuit/evasion spacecraft trajectories in the hill reference frame. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2013. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/44224.

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

Council of Science Editors:

Stupik J. Optimal pursuit/evasion spacecraft trajectories in the hill reference frame. [Thesis]. University of Illinois – Urbana-Champaign; 2013. Available from: http://hdl.handle.net/2142/44224

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

6. Ellison, Donald. Automated planetary satellite tour planning with a novel low-thrust direct transcription method.

Degree: MS, 4048, 2013, University of Illinois – Urbana-Champaign

 Upon completion of the heliocentric leg of its mission, it is almost always the case that an interplanetary spacecraft has scientific objectives to accomplish. This… (more)

Subjects/Keywords: Sims-Flanagan; Low-Thrust; Trajectory; Optimization; Spacecraft; Orbit; Genetic Algorithm; Sparse Nonlinear OPTimizer (SNOPT); Automatic Differentiation; Jacobian; Nonlinear Program; Jupiter; Monotonic Basin Hopping; Mission Analysis Low-Thrust Trajectory Optimization (MALTO)

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APA (6th Edition):

Ellison, D. (2013). Automated planetary satellite tour planning with a novel low-thrust direct transcription method. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/44236

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):

Ellison, Donald. “Automated planetary satellite tour planning with a novel low-thrust direct transcription method.” 2013. Thesis, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/44236.

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

MLA Handbook (7th Edition):

Ellison, Donald. “Automated planetary satellite tour planning with a novel low-thrust direct transcription method.” 2013. Web. 06 Apr 2020.

Vancouver:

Ellison D. Automated planetary satellite tour planning with a novel low-thrust direct transcription method. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2013. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/44236.

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

Council of Science Editors:

Ellison D. Automated planetary satellite tour planning with a novel low-thrust direct transcription method. [Thesis]. University of Illinois – Urbana-Champaign; 2013. Available from: http://hdl.handle.net/2142/44236

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

7. Aubin, Brianna S. Optimization of relative orbit transfers via particle swarm and primer vector theory.

Degree: MS, 4048, 2011, University of Illinois – Urbana-Champaign

 Satellite clusters are a useful tool to improve mission cost-effectiveness and redundancy, but controlling the satellites within the cluster is a difficult task. The particle… (more)

Subjects/Keywords: relative orbits; Clohessy Wiltshire; primer vector; particle swarm; relative orbit elements; evolutionary algorithms; satellite swarm

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APA (6th Edition):

Aubin, B. S. (2011). Optimization of relative orbit transfers via particle swarm and primer vector theory. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/24011

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):

Aubin, Brianna S. “Optimization of relative orbit transfers via particle swarm and primer vector theory.” 2011. Thesis, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/24011.

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

MLA Handbook (7th Edition):

Aubin, Brianna S. “Optimization of relative orbit transfers via particle swarm and primer vector theory.” 2011. Web. 06 Apr 2020.

Vancouver:

Aubin BS. Optimization of relative orbit transfers via particle swarm and primer vector theory. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2011. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/24011.

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

Council of Science Editors:

Aubin BS. Optimization of relative orbit transfers via particle swarm and primer vector theory. [Thesis]. University of Illinois – Urbana-Champaign; 2011. Available from: http://hdl.handle.net/2142/24011

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

8. Englander, Jacob. Automated trajectory planning for multiple-flyby interplanetary missions.

Degree: PhD, 4048, 2013, University of Illinois – Urbana-Champaign

 Many space mission planning problems may be formulated as hybrid optimal control problems (HOCP), i.e. problems that include both real-valued variables and categorical variables. In… (more)

Subjects/Keywords: optimization; trajectory; interplanetary; orbital mechanics; ceestial mechanics; hybrid optimal control; mission planning

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APA (6th Edition):

Englander, J. (2013). Automated trajectory planning for multiple-flyby interplanetary missions. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/44367

Chicago Manual of Style (16th Edition):

Englander, Jacob. “Automated trajectory planning for multiple-flyby interplanetary missions.” 2013. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/44367.

MLA Handbook (7th Edition):

Englander, Jacob. “Automated trajectory planning for multiple-flyby interplanetary missions.” 2013. Web. 06 Apr 2020.

Vancouver:

Englander J. Automated trajectory planning for multiple-flyby interplanetary missions. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2013. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/44367.

Council of Science Editors:

Englander J. Automated trajectory planning for multiple-flyby interplanetary missions. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2013. Available from: http://hdl.handle.net/2142/44367

9. Ghosh, Pradipto. New numerical methods for open-loop and feedback solutions to dynamic optimization problems.

Degree: PhD, 4048, 2014, University of Illinois – Urbana-Champaign

 The topic of the first part of this research is trajectory optimization of dynamical systems via computational swarm intelligence. Particle swarm optimization is a nature-inspired… (more)

Subjects/Keywords: Trajectory Optimization; Optimal Control Theory; Optimal Feedback Control; Feedback Guidance; Pursuit-Evasion Games; Dynamic Programming; Particle Swarm Optimization; Swarm Intelligence

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APA (6th Edition):

Ghosh, P. (2014). New numerical methods for open-loop and feedback solutions to dynamic optimization problems. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/46737

Chicago Manual of Style (16th Edition):

Ghosh, Pradipto. “New numerical methods for open-loop and feedback solutions to dynamic optimization problems.” 2014. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/46737.

MLA Handbook (7th Edition):

Ghosh, Pradipto. “New numerical methods for open-loop and feedback solutions to dynamic optimization problems.” 2014. Web. 06 Apr 2020.

Vancouver:

Ghosh P. New numerical methods for open-loop and feedback solutions to dynamic optimization problems. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2014. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/46737.

Council of Science Editors:

Ghosh P. New numerical methods for open-loop and feedback solutions to dynamic optimization problems. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/46737

10. Martin, Christopher S. A new numerical optimization method based on Taylor series for challenging trajectory optimization problems.

Degree: PhD, 4048, 2011, University of Illinois – Urbana-Champaign

 New methods to solve trajectory optimization problems are devised. The methods use direct transcription to convert the continuous optimal control problem into a parameter optimization… (more)

Subjects/Keywords: Taylor Series; Optimization; Trajectory; Circular restricted three body problem (CR3BP); Optimal Control; Direct Transcription; Collocation

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

APA (6th Edition):

Martin, C. S. (2011). A new numerical optimization method based on Taylor series for challenging trajectory optimization problems. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/26074

Chicago Manual of Style (16th Edition):

Martin, Christopher S. “A new numerical optimization method based on Taylor series for challenging trajectory optimization problems.” 2011. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/26074.

MLA Handbook (7th Edition):

Martin, Christopher S. “A new numerical optimization method based on Taylor series for challenging trajectory optimization problems.” 2011. Web. 06 Apr 2020.

Vancouver:

Martin CS. A new numerical optimization method based on Taylor series for challenging trajectory optimization problems. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2011. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/26074.

Council of Science Editors:

Martin CS. A new numerical optimization method based on Taylor series for challenging trajectory optimization problems. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2011. Available from: http://hdl.handle.net/2142/26074

11. Ellison, Donald Hamilton. Robust preliminary design for multiple gravity assist spacecraft trajectories.

Degree: PhD, Aerospace Engineering, 2018, University of Illinois – Urbana-Champaign

 The development of a new spacecraft trajectory design method most often occurs because a particular capability does not exist. The invention is usually considered successful… (more)

Subjects/Keywords: Sims-Flanagan; Low-Thrust; Trajectory; Optimization; Spacecraft; Orbit; Sparse Nonlinear OPTimizer (SNOPT); Automatic Differentiation; Jacobian; Partial Derivatives; State Transition Matrix; Nonlinear Program; Moon Tour; Monotonic Basin Hopping; Evolutionary Mission Trajectory Generator (EMTG); Sundman; Finite-Burn; MIRAGE; OpenMP; Parallel Computing

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APA (6th Edition):

Ellison, D. H. (2018). Robust preliminary design for multiple gravity assist spacecraft trajectories. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/101551

Chicago Manual of Style (16th Edition):

Ellison, Donald Hamilton. “Robust preliminary design for multiple gravity assist spacecraft trajectories.” 2018. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/101551.

MLA Handbook (7th Edition):

Ellison, Donald Hamilton. “Robust preliminary design for multiple gravity assist spacecraft trajectories.” 2018. Web. 06 Apr 2020.

Vancouver:

Ellison DH. Robust preliminary design for multiple gravity assist spacecraft trajectories. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2018. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/101551.

Council of Science Editors:

Ellison DH. Robust preliminary design for multiple gravity assist spacecraft trajectories. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2018. Available from: http://hdl.handle.net/2142/101551

12. Johnson, Miles. Inverse optimal control for deterministic continuous-time nonlinear systems.

Degree: PhD, 4048, 2014, University of Illinois – Urbana-Champaign

 Inverse optimal control is the problem of computing a cost function with respect to which observed state input trajectories are optimal. We present a new… (more)

Subjects/Keywords: optimal control; inverse reinforcement learning; inverse optimal control; apprenticeship learning; Learning from demonstration; iterative learning control

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

APA (6th Edition):

Johnson, M. (2014). Inverse optimal control for deterministic continuous-time nonlinear systems. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/46747

Chicago Manual of Style (16th Edition):

Johnson, Miles. “Inverse optimal control for deterministic continuous-time nonlinear systems.” 2014. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed April 06, 2020. http://hdl.handle.net/2142/46747.

MLA Handbook (7th Edition):

Johnson, Miles. “Inverse optimal control for deterministic continuous-time nonlinear systems.” 2014. Web. 06 Apr 2020.

Vancouver:

Johnson M. Inverse optimal control for deterministic continuous-time nonlinear systems. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2014. [cited 2020 Apr 06]. Available from: http://hdl.handle.net/2142/46747.

Council of Science Editors:

Johnson M. Inverse optimal control for deterministic continuous-time nonlinear systems. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/46747

.