Design of Thrust Vectoring Vertical/Short Takeoff and Landing Aircraft Stability Augmentation Controller Based on L1 Adaptive Control Law

نویسندگان

چکیده

Aiming at the conversion process of thrust vectoring vertical/short takeoff and landing (V/STOL) aircraft with a symmetrical structure in transition stage landing, there is problem coupling redundancy control quantities. To solve this problem, corresponding inner loop stabilization controller distribution strategy are designed. In paper, dynamic system model established. Based on outer adopting conventional nonlinear inverse control, an L1 adaptive designed based as to compensate mismatch uncertainty system. The key feature architecture ensuring robustness presence fast adaptation, so achieve unified performance boundary transient steady-state operations, thus eliminating need for rate gain scheduling. verified by simulation shooting Monte Carlo approach. results show that can still track reference input well has good when large parameter perturbation.

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ژورنال

عنوان ژورنال: Symmetry

سال: 2022

ISSN: ['0865-4824', '2226-1877']

DOI: https://doi.org/10.3390/sym14091837