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Fault Tolerant Control Method for Discrete Uncertain Multi-Delay Quadrotor System

A quad-rotor system, fault-tolerant control technology, applied in the field of sliding mode predictive fault-tolerant control, can solve problems such as insufficient research on fault-tolerant problems of multi-delay systems, and achieve a balance between local development capabilities and global search capabilities, good convergence speed, and improved fault tolerance. The effect of controlling precision

Active Publication Date: 2021-10-12
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

According to the current research status, researchers mostly study the problem of fault-tolerant control of systems with single time-delay (generally state time-delay), but the research on the fault-tolerant problem of uncertain multi-time-delay systems with actuator failures has not yet been carried out. deep enough

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  • Fault Tolerant Control Method for Discrete Uncertain Multi-Delay Quadrotor System
  • Fault Tolerant Control Method for Discrete Uncertain Multi-Delay Quadrotor System
  • Fault Tolerant Control Method for Discrete Uncertain Multi-Delay Quadrotor System

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Embodiment Construction

[0099] The present invention will be further explained below in conjunction with the accompanying drawings.

[0100] Such as figure 1 As shown in , in order to eliminate the approaching process of the system state, the system state is located on the sliding surface from the beginning to ensure the global robustness, and the quasi-integral sliding surface is designed as the prediction model; considering multiple time delays, faults, uncertain In order to reduce the influence of time-delay and disturbance on the system, a double-power function reference trajectory that can effectively weaken the influence of time-delay on the system is designed; and an improved fault compensation is added to the design of the reference trajectory, which reduces the bandwidth of the quasi-sliding mode and improves the Control accuracy; in the rolling optimization algorithm design, an improved inverse-time coyote optimization algorithm is designed; on the basis of the traditional coyote algorithm,...

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Abstract

The invention discloses a novel sliding mode predictive fault-tolerant control algorithm for discrete uncertain multi-time-delay four-rotor systems under actuator faults. Aiming at the fault-tolerant control problem of discrete uncertain multi-delay quadrotor system in the presence of actuator faults, a quasi-integral sliding surface is designed as a predictive model to eliminate approaching modes and ensure global robustness. Secondly, aiming at actuator faults and multiple time delays, an improved fault compensation double power function reference trajectory is designed to weaken the influence of time delays on the system and improve the accuracy of fault-tolerant control. Thirdly, an improved Inverse Coyote Algorithm (ICOA) is designed for rolling optimization, which can avoid falling into local extremum during the optimization process while obtaining good convergence speed, and balances the performance of local exploitation and global search. The invention is used for the robust fault-tolerant control of a class of multi-time-delay discrete uncertain systems with actuator faults.

Description

technical field [0001] The invention relates to a sliding mode predictive fault-tolerant control method based on an improved coyote optimization algorithm (ICOA) designed for a multi-time-delay quadrotor system with actuator faults, and belongs to the technical field of robust fault-tolerant control for discrete uncertain systems. Background technique [0002] In recent years, with the rapid development of artificial intelligence and industrial technology, the demand for fault-tolerant control systems with superior performance and robustness that can cope with various disturbances and faults is also increasing. The most critical part of these control systems is the intelligent algorithm. Nowadays, more and more advanced intelligent algorithms have been successfully applied to specific control systems, and they exhibit superior performance. However, during the long-term operation of smart devices, some failures are inevitable. Faults will have harmful effects on the control...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 杨蒲张芷晴王梓欣
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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