2019
DOI: 10.1002/acs.2976
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Adaptive finite‐time actuator fault‐tolerant coordinated attitude control of multispacecraft with input saturation

Abstract: SummaryIn this study, for nonrigid spacecraft formation, a distributed adaptive finite‐time actuator fault‐tolerant (FTAFT) coordinated attitude tracking control (CATC) issue is addressed. Aiming at stabilizing the spacecraft formation flying system during a limited time, two distributed adaptive FTAFT CATC strategies are presented. Initially, on basis of distributed finite‐time observer (DFTO), adaptive control, consensus approach, graph theory, and finite‐time theory, we develop a distributed adaptive FTAFT … Show more

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Cited by 10 publications
(10 citation statements)
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“…Then, we can get that v 1 and 𝜔 1 are bounded, due to z 1 = v 1 + 𝜔 1 , z 1 is bounded. Because of 𝛼 i being bounded, from ( 9), (22), and ( 35), x i,c is bounded. From (5), y d is bounded, so x i is bounded.…”
Section: Resultsmentioning
confidence: 99%
“…Then, we can get that v 1 and 𝜔 1 are bounded, due to z 1 = v 1 + 𝜔 1 , z 1 is bounded. Because of 𝛼 i being bounded, from ( 9), (22), and ( 35), x i,c is bounded. From (5), y d is bounded, so x i is bounded.…”
Section: Resultsmentioning
confidence: 99%
“…By using 0 < 𝜏 k,n (t) ≤ 𝜏 2 , and 0 < d(t) ≤ d 2 , applying the Wirtinger-based inequality from Reference 3 and Jenson's inequality to the integral term in (21), we get that…”
Section: Memory Event-triggered Schemementioning
confidence: 99%
“…On another frontier, the definition of finite-time stability (FTS) characterizes the trajectories of the system within a fixed-time interval and has grabbed enormous attention from researchers. [20][21][22] In contrast to asymptotic Lyapunov stability, FTS implies that system states must be kept within certain limits in the finite-time interval. From a practical point of view, the dynamic behavior of the systems must not exceed specified limits during a fixed time interval.…”
Section: Introductionmentioning
confidence: 99%
“…Considering the aforementioned issues, this paper aims to develop a finite time attitude controller for solar sail due to its good performance in fast convergence and the wide applications in attitude control of spacecraft (Zhong et al, 2016;Hu and Tan, 2017;Zhu and Guo, 2017;Zhu et al, 2019), to obtain a fast tracking control of sail's attitude required by orbit mission. A solar sail equipped with sliding masses and RSB is investigated, taking into account the changing inertia, the unknown SRP disturbance, as well as the torque constraints caused by actuator saturation and attitude maneuver.…”
Section: Introductionmentioning
confidence: 99%