An overview of prescribed performance control and its application to spacecraft attitude system

Wei, Caisheng; Chen, Qifeng; Liu, Jun; Zhao, Yin; Luo, Jianjun

doi:10.1177/0959651820952552

Cited by 55 publications

(30 citation statements)

References 81 publications

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“…Recently, lots of successful applications of PPC have been reported. Notice that the brief overview on PPC presented in Wei et al [30] only focuses on the applications to spacecraft. In this section, we will make a more comprehensive survey on the latest developments of PPC's applications in aircraft, spacecraft, vehicles, mechanical systems, surface vessels, underwater vehicles, multiagent systems, constrained systems, and some other dynamic systems.…”

Section: Applications Of Ppcmentioning

confidence: 99%

Prescribed performance control approaches, applications and challenges: A comprehensive survey

2022

Asian Journal of Control

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As to control systems, transient performance is as important as steady‐state performance. For some special dynamic systems, transient performance is a more prior index in comparison with the steady‐state one. Prescribed performance control (PPC) has been proved to be a powerful tool that guarantees control system outputs/errors with desired transient performance as well as steady‐state performance. The purpose of this paper is to give a comprehensive review on the latest developments of PPC theories and applications. The existing performance functions are classified into five different categories, and their features are comprehensively compared, providing a useful guidance for further applications. Then, the latest developments of PPC's applications in all kinds of control systems are recalled. Specially, the faced challenges and theoretical defects of PPC are discussed, which is expected to point out the further research direction for PPC.

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Section: Applications Of Ppcmentioning

confidence: 99%

Prescribed performance control approaches, applications and challenges: A comprehensive survey

2022

Asian Journal of Control

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“…For example, quadcopters are now commonly used to photograph landscapes. The quadcopter's roll pitch Euler angle has a significant impact on the final images, thus it must be controlled with high quality performance [40]. So, the attitude stability was met with great interest which is clearly shown in flexible flight movement [3].…”

Section: A Attitude Controllermentioning

confidence: 99%

Attitude and Altitude Nonlinear Control Regulation of a Quadcopter Using Quaternion Representation

et al. 2022

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Controlling a quadcopter is a challenging task because of the inherent high nonlinearity of a quadcopter system. In this paper, a new quaternion-based nonlinear feedback controller for attitude and altitude regulation of a quadcopter is proposed. The dynamic model of the quadcopter is derived using Newton and Euler equations. The proposed controller is established based on a feedback linearization technique to control and regulate the quadcopter. Global asymptotic stability of the designed controller is verified using Lyapunov stability criterion. A comparison between the proposed controller and two states of the art quadcopter controller is performed to evaluate its efficiency and performance. The efficiency of the proposed controller is clearly shown when the quadcopter is in or near a critical position. Simulations are performed to assess the transient and steady state performance. Steady state error and Max error indicators demonstrate the validity and effectiveness of the proposed algorithm with different reference controllers.

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“…The spacecraft attitude control system is one of the essential fundamental modules (Fayyaz and Vladimirova, 2016;Zhang et al, 2021b;Wei et al, 2020). Spacecraft needs to realize precise attitude pointing in the operation of a specific mission, which relies on high-precision control algorithms (Zhang et al, 2021a).…”

Section: Motivationmentioning

confidence: 99%

Fault-tolerant control of spacecraft attitude regulation: a concise adaptive dual-mode scheme

Dai

et al. 2021

AEAT

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Purpose This paper aims to address the spacecraft attitude regulation problem in the presence of extrinsic disturbances and actuator faults. Design/methodology/approach Based on adaptive backstepping design technique, a new concise adaptive dual-mode control scheme is proposed, which can either use the fault information detected by fault diagnosis mechanisms or switch to the fault-unknown mode when the fault diagnosis information is non-existent for control signal generation. These two modes share an adaptive mechanism that reduces the complexity of the algorithm. Findings The new fault-tolerant attitude control algorithm can accommodate both modes with and without fault diagnosis mechanisms. Originality/value The proposed algorithm in this paper can be applied to both cases when the attitude control system is equipped with or without fault diagnosis capability. This also enhances the robustness of attitude control algorithm. This study performs numerical simulations and verifies that the algorithm could effectively adapt to both modes.

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An overview of prescribed performance control and its application to spacecraft attitude system

Cited by 55 publications

References 81 publications

Prescribed performance control approaches, applications and challenges: A comprehensive survey

Prescribed performance control approaches, applications and challenges: A comprehensive survey

Attitude and Altitude Nonlinear Control Regulation of a Quadcopter Using Quaternion Representation

Fault-tolerant control of spacecraft attitude regulation: a concise adaptive dual-mode scheme

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