论文信息 - Spacecraft Robust Attitude Control With Saturation Nonlinearity

Spacecraft Robust Attitude Control With Saturation Nonlinearity

The paper presents a robust nonlinear ∞ H control design method for rigid spacecraft asymptotic attitude control with input saturation nonlinearity. The solution of the nonlinear ∞ H control problem is known to related to the existence of solution to a Hamilton-Jacobi partially differential inequality (HJPDI). The papers proposes a candidate solution to the HJPDI for spacecraft attitude control that is subject to nonlinear dynamics and input saturation. The method is applied to the ROCSAT-3 attitude control problem to verify its effectiveness.

Jyh-Ching Juang | Chen-Tsung Lin | Long-Life Show | Ying-Wen Jan

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