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2017
DOI: 10.1002/rnc.3889
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Retrofit fault‐tolerant tracking control design of an unmanned quadrotor helicopter considering actuator dynamics

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

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Cited by 26 publications
(7 citation statements)
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“…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.…”
Section: Introductionmentioning
confidence: 99%
“…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.…”
Section: Introductionmentioning
confidence: 99%
“…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.…”
Section: Introductionmentioning
confidence: 99%
“…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.…”
Section: Introductionmentioning
confidence: 99%