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Guidance of a Small Spacecraft for Soft Landing on an Asteroid using Fuzzy Control

Abstract Details

2015, MS, University of Cincinnati, Engineering and Applied Science: Aerospace Engineering.
The problem of landing a small spacecraft on the surface of an asteroid is analyzed in this thesis. The main effort of the thesis is focused around developing a fuzzy logic system to act as the controller. The fuzzy logic system is paired with a genetic algorithm to optimize the controller’s membership functions. This optimized controller is then compared with two established controllers: an Optimal Control approach, and a Multiple Sliding-Surfaces Guidance algorithm. The genetic-fuzzy approach presented is applicable to designing controllers for various spacecraft and asteroid profiles.
Grant Schaffner, Ph.D. (Committee Chair)
Kelly Cohen, Ph.D. (Committee Member)
Elad Kivelevitch, Ph.D. (Committee Member)
82 p.

Recommended Citations

Citations

  • Hartmann, J. (2015). Guidance of a Small Spacecraft for Soft Landing on an Asteroid using Fuzzy Control [Master's thesis, University of Cincinnati]. OhioLINK Electronic Theses and Dissertations Center. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1439300900

    APA Style (7th edition)

  • Hartmann, Jacob. Guidance of a Small Spacecraft for Soft Landing on an Asteroid using Fuzzy Control. 2015. University of Cincinnati, Master's thesis. OhioLINK Electronic Theses and Dissertations Center, http://rave.ohiolink.edu/etdc/view?acc_num=ucin1439300900.

    MLA Style (8th edition)

  • Hartmann, Jacob. "Guidance of a Small Spacecraft for Soft Landing on an Asteroid using Fuzzy Control." Master's thesis, University of Cincinnati, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1439300900

    Chicago Manual of Style (17th edition)