This article proposes a novel adaptive switching control of hypersonic aircraft based on type-
2 Takagi–Sugeno–Kang fuzzy sliding mode control and focuses on the problem of stability …

This paper presents a novel adaptive mode switching scheme for hypersonic morphing
aircraftwith retracted winglets based on type-2 Takagi-Sugeno-Kang (TSK) fuzzy sliding …

This paper proposes a type-2 fuzzy adaptive sliding mode control scheme for tracking
control of hypersonic aircraft with uncertainties. This method uses full-state feedback to …

In this paper, the adaptive fuzzy sliding mode control is applied to the hypersonic vehicle.
The detailed design procedure of the fuzzy sliding mode control system is presented. The …

This paper proposes a fuzzy integral sliding mode control strategy for flexible air-breathing
hypersonic vehicles with input nonlinearity. Based on the complex nonlinear dynamics in the …

This paper presents a fuzzy smooth-switching coordinate strategy for air-breathing
hypersonic vehicle with variable geometry scramjet inlet (AHV-VGI), which can improve the …

The interval type-2 fuzzy, combined with sliding mode control, is proposed in this paper to
design a novel nonlinear robust controller for a hypersonic aircraft. In this method, sliding …

An adaptive fuzzy sliding mode control (AFSMC) approach is proposed for a robotic airship.
First, the mathematical model of an airship is derived in the form of a nonlinear control …

The conversion mode control scheme for tilt-rotor aircraft is provided with a switched Takagi-
Sugeno (TS) fuzzy modeling method and an adaptive anti-disturbance reference model …

A novel learning method of control law of mode switching for hypersonic morphing aircraft,
based on type-2 Takagi-Sugeno-Kang (TSK) fuzzy neural network, is proposed in this paper …