Robust flight control design using incremental adaptive sliding mode control

2016 ◽  
Author(s):  
Idris E. Putro ◽  
Florian Holzapfel
Keyword(s):  
Sliding Mode Control ◽  
Flight Control ◽  
Sliding Mode ◽  
Control Design ◽  
Adaptive Sliding Mode Control ◽  
Adaptive Sliding Mode ◽  
Mode Control ◽  
Robust Flight Control

Autonomous Aerial Refueling Modeling and Dynamic Inversion Adaptive Sliding Mode Control

2013 ◽  
Vol 760-762 ◽  
pp. 1202-1206
Author(s):  
Xun Sun ◽  
Xin Guo Zhang
Keyword(s):  
Sliding Mode Control ◽  
Flight Control ◽  
Control Method ◽  
Sliding Mode ◽  
Adaptive Sliding Mode Control ◽  
Dynamic Inversion ◽  
Aerial Refueling ◽  
Adaptive Sliding Mode ◽  
Mode Control ◽  
And Performance

A dynamic inversion adaptive sliding mode flight control method for autonomous aerial refueling (AAR) is approved in this paper. The drogue model and refueling aircraft 6-DOF nonlinear model is built. In order to improve the flight control precision and performance, the dynamic inversion control method is used to design the flight control law. Fuzzy adaptive control is combined with the sliding mode control is used to compensate the error of inversion, so the robustness and transient characteristic performance could be improved. The simulation results show that the AAR flight control has excellent control performance.

Sliding Mode Control Design for Uncertain Singular Systems

2011 ◽  
Vol 145 ◽  
pp. 16-20 ◽  
Author(s):  
Kuo Jung Lin
Keyword(s):  
Sliding Mode Control ◽  
Sliding Mode ◽  
Singular Systems ◽  
Sufficient Conditions ◽  
Control Design ◽  
Adaptive Sliding Mode Control ◽  
Sliding Mode Controller ◽  
Adaptive Sliding Mode ◽  
Mode Control ◽  
Uncertain Singular Systems

This paper addresses the problem of sliding mode control design and adaptive sliding mode control design for robust stabilization of uncertain singular systems with guaranteed control performance. Based on the Lyapunov stability theorem, we solve two sufficient conditions for stabilization of the uncertain singular systems. The proposed sliding mode controller and adaptive sliding mode controller can reduce the effect of uncertainty. An electrical system is given to illustrate the validity of the proposed scheme. Simulation result shown that the adaptive sliding mode control design is better than sliding mode control design case.

Design of Reconfigurable Flight Control System Using Adaptive Sliding Mode Control: Actuator Fault

2005 ◽  
Vol 219 (4) ◽  
pp. 321-328 ◽  
Author(s):  
D Shin ◽  
G Moon ◽  
Y Kim
Keyword(s):  
Sliding Mode Control ◽  
Flight Control ◽  
Sliding Mode ◽  
System Stability ◽  
Control Technique ◽  
Adaptive Sliding Mode Control ◽  
Actuator Fault ◽  
Actuator Faults ◽  
Adaptive Sliding Mode ◽  
Mode Control

This article presents the reconfigurable flight controller using an adaptive sliding mode control scheme for actuator fault case. Sliding mode controller, which has good performance for the systems with various uncertainties, is used to deal with the actuator faults. Actuator fault can be considered as a disturbance or an unexpected parameter change, which degrades the system performance and may destabilize the system. In this study, the adaptive sliding mode control technique is adopted to compensate the effects of the disturbance generated by actuator faults. Lyapunov stability theory is used to derive the adaptive rule, and the closed-loop system stability analysis is performed. To demonstrate the effectiveness of the proposed controller, numerical simulation is performed for aircraft having redundant control surfaces.

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