2018
DOI: 10.1016/j.ifacol.2018.12.003
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Decentralized Formation Flight via PID and Integral Sliding Mode Control

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Cited by 15 publications
(18 citation statements)
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“…Two reasons lead to this choice. First, PID controller could be used however we assume the disturbances to be time-varying, and PID is bad at rejecting time-varying disturbances [29].…”
Section: Performance Very Good Good Excellentmentioning
confidence: 99%
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“…Two reasons lead to this choice. First, PID controller could be used however we assume the disturbances to be time-varying, and PID is bad at rejecting time-varying disturbances [29].…”
Section: Performance Very Good Good Excellentmentioning
confidence: 99%
“…Further, the development of an Integral sliding mode controller (ISC) for GCP was approached with the aim of sustaining the motion [28]. In situ situations were also covered in [29], where authors compared a PID controller with an ISC to maintain the formation of a MAS subjected to constant and time-varying disturbances or commands. The conclusion was made that the ISC presents better stability in case of communication failure.…”
Section: Introductionmentioning
confidence: 99%
“…The mathematical model in the Matlab [2][3][4][5][6][7][8][9][10] environment of the vibration damping unit is shown in Fig. 3.…”
Section: Mathematical Model Of the Vibration Damping Unitmentioning
confidence: 99%
“…To enhance the reliability and safety of these applications, researchers have developed many cooperative strategies of quad-rotor systems, one of which is the leader-follower formation scheme that allows for steering multiple quadrotors to form a geometric pattern while tracking a leader/reference. For this sake, three classical approaches can be applied, that is, linearization [11,15,23,24,26,29], inner-outer loop method [18,19,22,25,27,28,31] and feedback linearization approach [4,5,8,20].…”
Section: Introductionmentioning
confidence: 99%