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The attitude control performance of the bank-to-turn (BTT) missiles are severely interrupted by heavy nonlinear crossing couplings, time-varying aerodynamic parameters, and external disturbances. A distributed composite control framework consisting of a high-level model predictive control, a low-level state feedback stabilizer, and a feedforward compensation based on disturbance observer is proposed...
Robust autopilot design for bank-to-turn missiles under disturbances and uncertainties is investigated in this paper using the disturbance observer concept. In this setting, the influences caused by parameter variations are merged into a disturbance term and regarded as a part of the lumped disturbances. Disturbance observers are employed to estimate the lumped disturbances. However, the lumped disturbances...
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