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Teleoperation Control Based on Combination of Wave Variable and Neural Networks
In this paper, a novel control scheme is developed for a teleoperation system, combining the radial basis function (RBF) neural networks (NNs) and wave variable technique to simultaneously compensate for the effects caused by communication delays and dynamics uncertainties. Expand
Active Fault Tolerant Control for Vertical Tail Damaged Aircraft with Dissimilar Redundant Actuation System
Abstract This paper proposes an active fault-tolerant control strategy for an aircraft with dissimilar redundant actuation system (DRAS) that has suffered from vertical tail damage. A damage degreeExpand
Active fault-tolerant control strategy of large civil aircraft under elevator failures
Abstract Aircraft longitudinal control is the most important actuation system and its failures would lead to catastrophic accident of aircraft. This paper proposes an active fault-tolerant controlExpand
Adaptive decoupling synchronous control of dissimilar redundant actuation system for large civil aircraft
Abstract In order to meet the increasing reliability requirements of actuation system for large civil aircraft, the novel distributed dissimilar redundant actuation system composed of one hydraulicExpand
Active fault-tolerant control of dissimilar redundant actuation system based on performance degradation reference models
This paper investigates performance degradation of DRAS under the system malfunctions and addresses the problem of active switching of DRas from HA to EHA to ensure reliable actuation and efficient control. Expand
Adaptive Fuzzy Torque Control of Passive Torque Servo Systems Based on Small Gain Theorem and Input-to-state Stability
Passive torque servo system (PTSS) simulates aerodynamic load and exerts the load on actuation system, but PTSS endures position coupling disturbance from active motion of actuation system, and thisExpand
Linear Extended State Observer-Based Motion Synchronization Control for Hybrid Actuation System of More Electric Aircraft
This paper proposes a novel linear extended state observer (LESO)-based motion synchronization control method for a hybrid actuation system composed of two hybrid actuators. Expand
High performance torque controller design for electric load simulator
  • X. Wang, S. Wang
  • Engineering
  • 6th IEEE Conference on Industrial Electronics and…
  • 21 June 2011
Electric load simulator (ELS) is an important equipment in hardware-in-loop (HIL) simulation which exerts aerodynamic load to the actuation system according to the flight condition. Due to theExpand
Fault tolerant control strategy based on actuation switch mechanism for more-electric aircraft with vertical tail damage
This paper proposes a fault tolerant control strategy with an actuation switch mechanism for different degrees of vertical tail damage of more-electric aircraft (MEA). A damage degree coefficient ofExpand
Dynamic Friction Parameter Identification Method with LuGre Model for Direct-Drive Rotary Torque Motor
Attainment of high-performance motion/velocity control objectives for the Direct-Drive Rotary (DDR) torque motor should fully consider practical nonlinearities in controller design, such as dynamicExpand