Takagi-Sugeno Fuzzy Model-Based Attitude Control of Spacecraft with Partially-Filled Fuel Tank

نویسندگان

  • Lilit Mazmanyan
  • Mohammad A. Ayoubi
چکیده

This paper presents a Takagi-Sugeno fuzzy model-based controller which stabilizes the attitude of spacecraft with a partially-filled fuel tank. First, the nonlinear equations of motion of spacecraft containing a liquid fuel store is presented briefly. Then, the fuzzy modeling and the parallel distributed compensation control technique are applied. The proposed fuzzy controller is a nonlinear controller which utilizes full-state feedback with bounded control input. Using a quadratic Lyapunov function, the fuzzy control design problem can be formulated in terms of linear matrix inequalities. In the end, we evaluate the proposed control system performance via numerical simulation results.

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تاریخ انتشار 2014