Abstract:Summary
This paper presents a retrofit fault‐tolerant tracking control (FTTC) design method with application to an unmanned quadrotor helicopter (UQH). The proposed retrofit fault‐tolerant tracking controller is developed to accommodate loss‐of‐effectiveness faults in the actuators of UQH. First, a state feedback tracking controller acting as the normal controller is designed to guarantee the stability and satisfactory performance of UQH in the absence of actuator faults, while actuator dynamics of UQH are als… Show more
“…Viable structure control [ 7 ], sliding mode control [ 8 ], fuzzy control [ 9 ], model predictive control [ 10 ], neural networks theory [ 11 ], and passivity theory [ 12 ] techniques have been proposed for reducing or even eliminating the impact of the failures. From the point of practical application, a significant amount of research on FTC schemes is applied to aerospace aircraft [ 13 ], power equipment [ 14 , 15 ], industrial processes [ 16 ], etc.…”
This paper considers an adaptive fault-tolerant control problem for a class of uncertain strict feedback nonlinear systems, in which the actuator has an unknown drift fault and the loss of effectiveness fault. Based on the event-triggered theory, the adaptive backstepping technique, and Lyapunov theory, a novel fault-tolerant control strategy is presented. It is shown that an appropriate comprise between the control performance and the sensor data real-time transmission consumption is made, and the fault-tolerant tracking control problem of the strict feedback nonlinear system with uncertain and unknown control direction is solved. The adaptive backstepping method is introduced to compensate the actuator faults. Moreover, a new adjustable event-triggered rule is designed to determine the sampling state instants. The overall control strategy guarantees that the output signal tracks the reference signal, and all the signals of the closed-loop systems are convergent. Finally, the fan speed control system is constructed to demonstrate the validity of the proposed strategy and the application of the general systems.
“…Viable structure control [ 7 ], sliding mode control [ 8 ], fuzzy control [ 9 ], model predictive control [ 10 ], neural networks theory [ 11 ], and passivity theory [ 12 ] techniques have been proposed for reducing or even eliminating the impact of the failures. From the point of practical application, a significant amount of research on FTC schemes is applied to aerospace aircraft [ 13 ], power equipment [ 14 , 15 ], industrial processes [ 16 ], etc.…”
This paper considers an adaptive fault-tolerant control problem for a class of uncertain strict feedback nonlinear systems, in which the actuator has an unknown drift fault and the loss of effectiveness fault. Based on the event-triggered theory, the adaptive backstepping technique, and Lyapunov theory, a novel fault-tolerant control strategy is presented. It is shown that an appropriate comprise between the control performance and the sensor data real-time transmission consumption is made, and the fault-tolerant tracking control problem of the strict feedback nonlinear system with uncertain and unknown control direction is solved. The adaptive backstepping method is introduced to compensate the actuator faults. Moreover, a new adjustable event-triggered rule is designed to determine the sampling state instants. The overall control strategy guarantees that the output signal tracks the reference signal, and all the signals of the closed-loop systems are convergent. Finally, the fan speed control system is constructed to demonstrate the validity of the proposed strategy and the application of the general systems.
“…To avoid the catastrophes induced by the actuator faults, advanced fault-tolerant control (FTC) strategies must be developed to enhance flight safety. Recently, plentiful of FTC schemes have been proposed for single UAV [25][26][27][28][29]. By utilising the approximation capability of FNN, [20] presented a sliding-mode FTC scheme for an aircraft to counteract actuator faults.…”
Section: Introductionmentioning
confidence: 99%
“…(ii) Compared with the FTC methods developed for a single UAV, including [27,29], an FTCC scheme is proposed in this paper for networked UAVs in the presence of actuator faults. Moreover, in contrast to the centralised leader-follower FTCC schemes presented in [30,31], which may induce instability to the formation team if a group of follower UAVs loses the communications with the leader UAV since all follower UAVs only communicate with the leader UAV in this scheme, the FTCC scheme presented in this paper is developed for UAVs in a distributed communication network, in which each follower UAV can communicate with its neighbouring UAVs to eventually achieve the attitude tracking with respect to the leader UAV.…”
“…As an ideal platform, innovative unmanned aerial vehicles (UAVs) have been strongly demanded by commercial, scientific, and military communities [1] for a variety of applications, such as environmental monitoring and surveillance [2,3], testing and validation platforms for newly developed control techniques [4][5][6], postdisaster search and rescue [7], cooperative and formation control [8][9][10][11], goods delivery and in-flight refueling [12][13][14], and various military missions [15]. e deployment of UAVs, however, is generally in confined space and hostile environment and subjects to environmental disturbances and sideslip effects.…”
With growing worldwide interests in commercial, scientific, and military issues, there has been a corresponding rapid growth in demand for the development of unmanned aerial vehicles (UAVs) with more reliable and safer motion control abilities. This paper presents a new nonlinear path following scheme integrated with a heading control law for achieving accurate and reliable path following performance. Both backstepping and finite-time techniques are employed for developing the path following and heading control strategies capable of minimizing cross-track errors in finite-time with elegant transient performance, while the barrier Lyapunov function scheme is adopted to limit turning rates of the UAV for preventing it from capsizing which may be induced by overquick steering actions. A fixed-time nonlinear estimator, based on UAV kinematics, is designed for estimating the uncertainties with sideslip angles caused by external disturbances and inertial motions. To avoid the complicated calculation of derivatives of virtual control terms in backstepping, command filters and auxiliary systems are likewise introduced in the design of control laws. Extensive numerical simulation studies on a nonlinear UAV model are conducted to demonstrate the effectiveness of the proposed methodologies.
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