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Multivariable Sliding Mode Control for Aircraft Engines

Sangwian, Sirirat

Abstract Details

2011, Master of Science in Mechanical Engineering, Cleveland State University, Fenn College of Engineering.
Many control theories are used in controlling aircraft engines. However, the multivariable sliding mode control is not yet established in this application even though it has a lot of potential in dealing with complex and nonlinear systems such as aircraft engines. Therefore, a guideline in developing multivariable sliding mode control law for an aircraft engine is presented in this thesis. The problem of chattering in the sliding mode control is suppressed by the use of the boundary layer method. The control logic is tested by implementing NASA’s Commercial Modular Aero-Propulsion System Simulation 40k (C-MAPSS40k). Simulation results are analyzed and compared to the results obtained from the baseline controller. The robust property of multivariable sliding mode control is also examined by altering the flight condition of the engine.
Hanz Richter, PhD (Committee Chair)
Jerzy Sawicki, PhD (Committee Member)
Lili Dong, PhD (Committee Member)

Recommended Citations

Citations

  • Sangwian, S. (2011). Multivariable Sliding Mode Control for Aircraft Engines [Master's thesis, Cleveland State University]. OhioLINK Electronic Theses and Dissertations Center. http://rave.ohiolink.edu/etdc/view?acc_num=csu1315587541

    APA Style (7th edition)

  • Sangwian, Sirirat. Multivariable Sliding Mode Control for Aircraft Engines. 2011. Cleveland State University, Master's thesis. OhioLINK Electronic Theses and Dissertations Center, http://rave.ohiolink.edu/etdc/view?acc_num=csu1315587541.

    MLA Style (8th edition)

  • Sangwian, Sirirat. "Multivariable Sliding Mode Control for Aircraft Engines." Master's thesis, Cleveland State University, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=csu1315587541

    Chicago Manual of Style (17th edition)