Perpustakaan Digital ITB

This undergraduate final project aims to address several uncertainties that can contribute to the formulation of pilot-induced oscillation (PIO) by augmenting an adaptive control scheme. A series of control input manipulation is introduced in the form of control deficiency feedback and rate saturation to prevent actuator rate and position limits. Furthermore, the error is adjusted to account for actuator physical limitations, preventing the system to track errors that are beyond the capability of the actuator and ensuring stable adaptation. The simulations are limited to pitch pointing and Handling Qualities During Tracking (HQDT) tasks. The augmentation of the proposed adaptive model successfully prevents PIO observed in the baseline model.