2014
DOI: 10.1016/j.actaastro.2014.10.011
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Decentralized sliding-mode control for spacecraft attitude synchronization under actuator failures

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Cited by 37 publications
(21 citation statements)
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“…Apparently, according to the reverse of the previous procedure, the predefined constraint condition (8) can be satisfied under the condition (11).…”
Section: Prescribed Performancementioning
confidence: 99%
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“…Apparently, according to the reverse of the previous procedure, the predefined constraint condition (8) can be satisfied under the condition (11).…”
Section: Prescribed Performancementioning
confidence: 99%
“…It is proved that all the signals in the closed-loop system are bounded, and the prescribed tracking performances are guaranteed. Two decentralized sliding mode control laws were proposed and analyzed for spacecraft attitude synchronization under actuator failures, and the results could be extended to the case with control input saturation in the second controller [11]. 256 R. CHANG ET AL.…”
mentioning
confidence: 99%
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“…Many works on attitude control have been reported, and different approaches are proposed [3][4][5][6]. Due to their small weight, high reliability and agility, reaction wheels are commonly used actuators that store and exchange angular momentum to generate the necessary torques to perform attitude maneuvers.…”
Section: Introductionmentioning
confidence: 99%