2021
DOI: 10.1007/s11071-021-06237-1
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Robust fault accommodation strategy of the reentry vehicle: a disturbance estimate-triggered approach

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Cited by 9 publications
(4 citation statements)
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“…Spawned by the rapid advances in networked systems and distributed cooperation, there has been a flurry of activity on the topic of multi-agent systems (MASs). During the past few years, MASs have found extensive application in both industrial and military domains, such as multi-robot systems [ 1 ], satellite formation control [ 2 ], sensor networks [ 3 ], smart grids [ 4 ], flight control systems [ 5 ], etc.…”
Section: Introductionmentioning
confidence: 99%
“…Spawned by the rapid advances in networked systems and distributed cooperation, there has been a flurry of activity on the topic of multi-agent systems (MASs). During the past few years, MASs have found extensive application in both industrial and military domains, such as multi-robot systems [ 1 ], satellite formation control [ 2 ], sensor networks [ 3 ], smart grids [ 4 ], flight control systems [ 5 ], etc.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, it is significant to improve system reliability and safety not only by designing fault tolerant control (FTC) to compensate the effect caused by faults automatically, but also by enhancing reliability of signal components. The approaches of the fault-tolerant design can be broadly divided into two categories: the passive one [1][2][3][4][5] and the active one [6][7][8][9][10][11]. Although the passive approach is usually exploited to handle partial actuator faults [12][13][14] and complete actuator faults [15][16][17], it has also a limited capability of handling unknown actuator faults due to its passive control laws being fixed.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, the fault tolerant flight control is particularly important for flight safety. Recently, the faulttolerant control has attracted the global attention of researchers [5][6][7][8][9][10]. To enhance the reliability and availability of the attitude control for tailless aircraft suffering from actuator faults, a multiple time-scale reconfigurable sliding mode control has been proposed in [11], nevertheless, only a linear model was considered.…”
Section: Introductionmentioning
confidence: 99%