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[HTML][HTML] Flight evaluation of a sliding mode online control allocation scheme for fault tolerant control
This paper develops a sliding mode fault tolerant control scheme based on a Linear
Parameter Varying (LPV) system representation of the plant. The scheme includes a control …
Parameter Varying (LPV) system representation of the plant. The scheme includes a control …
Control method for determining feasible pre-stresses of cable-struts structure
The structural stiffness of a cable-struts structure is dependent on its feasible pre-stresses.
The search for the pre-stresses is an inverse problem, and classical approaches for this …
The search for the pre-stresses is an inverse problem, and classical approaches for this …
Simple adaptive wing-aileron flutter suppression system
In this work a simple adaptive flutter suppression system is designed in order to increase the
operative speed range of a wing-aileron aeroelastic plant. The equivalent beam finite …
operative speed range of a wing-aileron aeroelastic plant. The equivalent beam finite …
Sliding mode observers for robust fault estimation in linear parameter varying systems
A linear parameter varying sliding mode fault reconstruction scheme is proposed. Compared
with other conventional sliding mode observer designs, the estimate emerges quite naturally …
with other conventional sliding mode observer designs, the estimate emerges quite naturally …
Simple adaptive V-stack piezoelectric based airfoil flutter suppression system
The suppression of aeroelastic vibrations due to flutter using a trailing edge flap is analyzed
to increase the speed operability range of wings. The aeroelastic model of a 3DOF airfoil in …
to increase the speed operability range of wings. The aeroelastic model of a 3DOF airfoil in …
Nose landing gear simple adaptive shimmy suppression system
The occurrence of shimmy vibration in aircraft nose landing gear can cause an increase of
fatigue stress on the nose landing gear mechanical elements that can eventually lead to …
fatigue stress on the nose landing gear mechanical elements that can eventually lead to …
Simple adaptive control with an adaptive anti-windup compensator for the unmanned aerial vehicle attitude control
W Gai, Y Zhou, M Zhong, C Sheng, J Zhang - IEEE Access, 2020 - ieeexplore.ieee.org
This paper presents an extension of the simple adaptive control (SAC) deal with input
saturation for the attitude control of the unmanned aerial vehicle (UAV). A new SAC structure …
saturation for the attitude control of the unmanned aerial vehicle (UAV). A new SAC structure …
[HTML][HTML] Pilot-in-the-loop simulation of simple adaptive fault-tolerant controller
A piloted simulator evaluation is an important step for making a Fault-Tolerant Flight Control
(FTFC) system more practical and reliable. Especially, in the case of an adaptive technique …
(FTFC) system more practical and reliable. Especially, in the case of an adaptive technique …
[HTML][HTML] The Application and Optimisation of a Neural Network PID Controller for Trajectory Tracking Using UAVs
This paper considers the problem of flying a UAV along a given trajectory at speeds close to
the speed of sound and above. A novel pitch channel control system is presented using the …
the speed of sound and above. A novel pitch channel control system is presented using the …
A hybrid scheme to improve transient and recover performance in a fault-tolerant control system with loss of actuator effectiveness
In the context of fault-tolerant control (FTC), we propose a hybrid fault-tolerant control
scheme for single-input single-output systems with piecewise continuous dynamic and …
scheme for single-input single-output systems with piecewise continuous dynamic and …