Adaptive terminal super-twisting prescribed performance controller for near-space vehicle based on data-driven model

IF 6.3 2区 计算机科学 Q1 AUTOMATION & CONTROL SYSTEMS
Tianchen Zhang , Yibo Ding , Xiaokui Yue , Naying Li
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引用次数: 0

Abstract

A data-driven adaptive terminal super-twisting prescribed performance controller (DASTPC) is designed for near-space vehicle (NSV) to satisfy transient and steady-state performance, and prevent scramjet choking. Firstly, a novel predetermined-time performance function is proposed to guarantee that tracking error can converge to a prescribed bound of small residual sets at the predetermined time. Compared with traditional performance functions, the predetermined-time performance function can achieve faster respond speed, realize more accurate convergence, and avoid overlarge initial value of actuators. Secondly, by combining the predetermined-time performance function with sliding mode control, a novel non-singular fast terminal sliding surface and an improved adaptive super-twisting reaching law are proposed to improve computational efficiency and accelerate convergent rate of system. The adaptive reaching law can avoid excessive gains and attenuate chattering by automatically tuning control gain. Thirdly, a deep recurrent neural network-based long-short term memory (LSTM) is employed to learn time-series historical flight dynamics data offline, so as to construct a data-driven LSTM training model. This data-driven model replaces nominal dynamics model of NSV in DASTPC, effectively suppressing model uncertainties. In addition, a homogeneous high-order sliding mode observer is utilized to compensate for external disturbances, avoiding excessive parameter estimation. Since boundary conditions of the predetermined-time performance function are fully satisfied, the DASTPC can effectively restrict amplitude of angle of attack, thus ensuring the intake condition of scramjet. Ultimately, to illustrate the superiority of DASTPC, several sets of simulations are performed on NSV subject to prescribed performance bound, external disturbances and parameter perturbations.
基于数据驱动模型的近空飞行器自适应末端超扭规定性能控制器。
为满足近空飞行器瞬态和稳态性能要求,防止超燃冲压发动机呛流,设计了数据驱动的自适应末端超扭规定性能控制器(DASTPC)。首先,提出了一种新的预定时间性能函数,以保证跟踪误差在预定时间收敛于小残差集的规定界;与传统性能函数相比,预定时间性能函数可以实现更快的响应速度,实现更精确的收敛,避免执行器初始值过大。其次,将预定时间性能函数与滑模控制相结合,提出了一种新的非奇异快速终端滑动面和改进的自适应超扭逼近律,提高了计算效率,加快了系统的收敛速度;自适应趋近律通过自动调节控制增益,避免增益过大,减弱抖振。第三,采用基于深度递归神经网络的长短期记忆(LSTM)离线学习时间序列历史飞行动力学数据,构建数据驱动的LSTM训练模型。该数据驱动模型取代了DASTPC中的非NSV标称动力学模型,有效地抑制了模型的不确定性。此外,利用齐次高阶滑模观测器补偿外部干扰,避免了过多的参数估计。由于完全满足预定时间性能函数的边界条件,DASTPC可以有效地限制迎角的幅值,从而保证超燃冲压发动机的进气条件。最后,为了说明DASTPC的优越性,在规定的性能界限、外部干扰和参数扰动的情况下,对NSV进行了几组模拟。
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来源期刊
ISA transactions
ISA transactions 工程技术-工程:综合
CiteScore
11.70
自引率
12.30%
发文量
824
审稿时长
4.4 months
期刊介绍: ISA Transactions serves as a platform for showcasing advancements in measurement and automation, catering to both industrial practitioners and applied researchers. It covers a wide array of topics within measurement, including sensors, signal processing, data analysis, and fault detection, supported by techniques such as artificial intelligence and communication systems. Automation topics encompass control strategies, modelling, system reliability, and maintenance, alongside optimization and human-machine interaction. The journal targets research and development professionals in control systems, process instrumentation, and automation from academia and industry.
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