Distributed Finite-Time Fault-Tolerant Containment Control for Multiple Unmanned Aerial Vehicles

Yu, Ziquan; Liu, Zhixiang; Qu, Yaohong; Su, Chun-Yi

doi:10.1109/tnnls.2019.2927887

Cited by 156 publications

(98 citation statements)

References 59 publications

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“…is helps the WSN using LEACH-IBABC runs 58 more rounds. e total residual energy by using the LEACH-IBABC algorithm 6 Complexity reduces slower than that of the LEACH algorithm in the early stage. erefore, the LEACH-IBABC approach can be used to organize the global optimal topology and reduce the overall energy consumption of the network.…”

Section: Simulation and Analysis Of The Proposed Methodsmentioning

confidence: 99%

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A Novel Dynamic Routing Approach to Distributed Wireless Sensor Network in Aircraft Environment

Sun

Bai

et al. 2021

Complexity

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The trend to implement the monitoring system with a wireless sensor network has been becoming urgent due to guaranteed flight safety and the passengers comfortability in travel. In this paper, a new dynamic routing algorithm is proposed to prolong the lifetime of the monitoring system with a distributed network based on the K-coverage method, and filter algorithm to be used for data fusion. Finally, the simulation results validate the effectiveness of the proposed approach.

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Section: Simulation and Analysis Of The Proposed Methodsmentioning

confidence: 99%

“…Furthermore, this kind of network can be applied in different areas such as UAV systems and environment monitoring. [5][6][7][8]. Wang et al designed a WSN for pollutant monitoring in the cabin [7] and analyzed network failures cases [8].…”

Section: Introductionmentioning

confidence: 99%

A Novel Dynamic Routing Approach to Distributed Wireless Sensor Network in Aircraft Environment

Sun

Bai

et al. 2021

Complexity

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“…为确保故障情况下群体无人机编队飞行的安全性, Xu等人 [29] 和Yu等人 [30] 基于领航-跟随通信架构, 设计了固定翼无人机容错编队控制方案. 基于无人机分布式通信架构, 本文作者针对多无人机纵向跟踪控制 [31] 和纵向有限时间合围控制 [32] 中的容错协同控制问题展开了研究. Zhao等人 [ [34,35] x F m…”

Section: 与整数阶控制方法相比分数阶控制方法可以从unclassified

Fractional-order intelligent fault-tolerant synchronization tracking control of UAV swarms

Zhang

Jiang

2020

Sci. Sin.-Tech.

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“…The guardian map approach for control system design identifies the boundary of the controller gain with a suitable initial solution by calculating the roots of Equation (16). Likewise, a feasible solution of the controller gain can be formulated as inequality constraints if the topological structure International Journal of Aerospace Engineering of the null space of the guardian maps does not change.…”

Section: Longitudinal Dynamics With Inputmentioning

confidence: 99%

“…However, relaxed static stability margin results in stability problem in the flight control system, especially for an unstable plant with limited control authority [14]. The achievable flight stability and performance is closely related to the control authority [15], especially input saturation, control rate, and control failure [16]. Many anti-windup strategies have been proposed, such as introducing auxiliary dynamic systems to regulate the inputs [17].…”

Section: Introductionmentioning

confidence: 99%

Guardian Map Approach to Feasible Range of Static Stability Margin of Hypersonic Flight Vehicles with Input Saturation

Hao

Chen

Liu

et al. 2020

International Journal of Aerospace Engineering

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Static stability margin is a critical parameter in flight control design. The feasible range of it must cover the uncertainty through the flight. To reasonably identify the feasible range of static stability margin in advance, an approach based on guardian maps is proposed for flight control of hypersonic flight vehicles with input saturation. First, the model of hypersonic flight vehicle (HFV) is established as a parametric plant. Then, flying quality requirements for the closed-loop system are formulated as inequality constraints using guardian maps. Moreover, by using linear matrix inequality, the saturation of elevators is taken into account in the integrated control of attitude control. The prescribed minimum of static stability margin that ensures the flying quality of hypersonic flight vehicles with input saturation is obtained. Furthermore, from the prospective of integrated control, it is shown that the feasible range of static stability margin can be enlarged by changing aerodynamic characteristics. The effectiveness of the proposed approach is validated by numerical simulation.

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Distributed Finite-Time Fault-Tolerant Containment Control for Multiple Unmanned Aerial Vehicles

Cited by 156 publications

References 59 publications

A Novel Dynamic Routing Approach to Distributed Wireless Sensor Network in Aircraft Environment

A Novel Dynamic Routing Approach to Distributed Wireless Sensor Network in Aircraft Environment

Fractional-order intelligent fault-tolerant synchronization tracking control of UAV swarms

Guardian Map Approach to Feasible Range of Static Stability Margin of Hypersonic Flight Vehicles with Input Saturation

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