ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Attitude control scheme for morphing vehicles with output error constraints and input saturation
Received date: 2023-03-29
Revised date: 2023-04-28
Accepted date: 2023-05-19
Online published: 2023-05-22
The attitude control problem of hypersonic morphing vehicles considering output error constraints and input saturation is investigated. Firstly， the dynamic model with uncertainties is established， and the input-saturation-oriented control system is derived based on hyperbolic tangent function and auxiliary system. The transformed error is then designed for the system to facilitate output error constraints under more relaxed convergency conditions. Then， the Fuzzy Disturbance Observer （FDO） is designed based on fuzzy logic system and finite-time theory， which enables the estimation error of disturbance converging to the origin in finite time. Subsequently， the back-stepping control scheme is proposed and the convergency of the closed-loop system with output error constraints and input saturation is ensured via Lyapunov synthesis. Finally， numerical simulation results are presented to demonstrate the effectiveness of the designed control scheme.
Haolan CHEN , Peng WANG , Guojian TANG . Attitude control scheme for morphing vehicles with output error constraints and input saturation[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023 , 44(15) : 528762 -528762 . DOI: 10.7527/S1000-6893.2023.28762
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