Novel anti-saturation adaptive sliding-mode-assisted disturbance observer for aerial imaging systems.

IF 6.5
Yutang Wang, Wenhao Li, Yan Li, Dapeng Tian
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Abstract

Aerial imaging systems are subject to complex multisource disturbances, including high-frequency engine vibrations and abrupt aerodynamic turbulence, which critically hinder line-of-sight stabilization. Moreover, input saturation nonlinearities imposed by stringent onboard hardware constraints severely limit the capability of the system to reject highly dynamic perturbations. To address these challenges, this study proposes a novel anti-saturation adaptive sliding-mode-assisted disturbance observer. The proposed scheme integrates a dual-strategy anti-saturation mechanism. First, a dynamic unsaturation-scale factor mathematically quantifies the residual driving capacity of the actuator to actively regulate the adaptive sliding-mode gain in real time. Second, a describing-function-based constraint is strictly embedded into the exact observer error dynamics. This dual approach intelligently manages the control effort within absolute physical limits, preventing integral windup, gain over-regulation, and catastrophic observer divergence during deep saturation. Through rigorous Lyapunov stability analysis, all closed-loop signals are proven to exhibit global uniform ultimate boundedness. Finally, comparative experiments conducted on an equivalent gimbal platform validated the superiority of the proposed controller in achieving both high dynamic disturbance rejection and high-precision imaging in adverse aerial environments. The proposed algorithm outperformed existing anti-disturbance methods in terms of convergence speed and dynamic performance, thereby validating its robustness.

航空成像系统抗饱和自适应滑模辅助干扰观测器。
航空成像系统受到复杂的多源干扰,包括高频发动机振动和突然的气动湍流,这些干扰严重阻碍了视线的稳定。此外,由严格的板载硬件约束施加的输入饱和非线性严重限制了系统拒绝高动态摄动的能力。为了解决这些挑战,本研究提出了一种新的抗饱和自适应滑模辅助干扰观测器。该方案集成了一种双策略抗饱和机制。首先,动态不饱和比例因子数学量化执行器的剩余驱动能力,以实时主动调节自适应滑模增益。其次,将基于描述函数的约束严格嵌入到精确观测器误差动态中。这种双重方法在绝对物理限制内智能地管理控制工作,防止了积分上发条、增益过度调节和深度饱和期间灾难性的观测器偏离。通过严格的李雅普诺夫稳定性分析,证明了所有闭环信号都具有全局一致的最终有界性。最后,在等效框架平台上进行了对比实验,验证了该控制器在恶劣航空环境下实现高动态抗干扰和高精度成像的优越性。该算法在收敛速度和动态性能方面优于现有的抗干扰方法,从而验证了其鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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