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In this paper, we propose and demonstrate an adaptive-sliding mode control for trajectory tracking control of robot manipulators subjected to uncertain dynamics, vibration disturbance, and payload variation disturbance. Throughout this work…

系统与控制 · 电气工程与系统科学 2024-08-07 Mustafa M. Mustafa , Carl D. Crane , Ibrahim Hamarash

Atmospheric flight phase of a launch vehicle is utilized to evaluate the performance of an H-infinity controller in the presence of disturbances. Dynamics of the vehicle is linearly modeled using time-varying parameters. An operating point…

系统与控制 · 计算机科学 2016-11-22 Antonio Graells , Francisco Carrabina

In this paper the problem of guidance formulation for autonomous soft landing of unmanned aerial vehicles on stationary, moving, or accelerating / maneuvering ground vehicles at desired approach angles in both azimuth and elevation is…

系统与控制 · 电气工程与系统科学 2020-10-01 Sashank Modali , Satadal Ghosh , Sujit P. B

Air-to-air missiles are used on many modern military combat aircraft for self-defence. It is imperative for the pilots using the weapons that the missiles hit their target first time. The important goals for a missile control system to…

系统与控制 · 电气工程与系统科学 2024-11-13 Joshua Farrington , Xinhua Wang

This paper investigates an adaptive sliding-mode control for an integrated UAV autopilot and guidance system. First, a two-dimensional mathematical model of the system is derived by considering the incorporated lateral dynamics and relative…

机器人学 · 计算机科学 2025-01-20 Minh Tu Nguyen , Van Truong Hoang , Manh Duong Phung , Van Hoa Doan

Successful aerial manipulation largely depends on how effectively a controller can tackle the coupling dynamic forces between the aerial vehicle and the manipulator. However, this control problem has remained largely unsolved as the…

机器人学 · 计算机科学 2024-10-14 Rishabh Dev Yadav , Swati Dantu , Wei Pan , Sihao Sun , Spandan Roy , Simone Baldi

This paper proposes a sliding mode controller with smooth control effort for a class of nonlinear plants. The proposed controller is created by allowing some constant parameters of the earlier smooth sliding control (SSC) to vary as a…

系统与控制 · 电气工程与系统科学 2023-10-31 Alessandro Jacoud Peixoto , Wenderson G. Serrantola , Fernando Lizarralde

Stable aerial manipulation during dynamic tasks such as object catching, perching, or contact with rigid surfaces necessarily requires compliant behavior, which is often achieved via impedance control. Successful manipulation depends on how…

系统与控制 · 电气工程与系统科学 2025-04-04 Amitabh Sharma , Saksham Gupta , Shivansh Pratap Singh , Rishabh Dev Yadav , Hongyu Song , Wei Pan , Spandan Roy , Simone Baldi

This paper proposes an adaptive dynamic programming-based adaptive-gain sliding mode control (ADP-ASMC) scheme for a fixed-wing unmanned aerial vehicle (UAV) with matched and unmatched disturbances. Starting from the dynamic of fixed-wing…

系统与控制 · 电气工程与系统科学 2021-07-14 Chaofan Zhang , Guoshan Zhang , Qi Dong

The recent development of novel aerial vehicles capable of physically interacting with the environment leads to new applications such as contact-based inspection. These tasks require the robotic system to exchange forces with…

机器人学 · 计算机科学 2022-07-06 Weixuan Zhang , Lionel Ott , Marco Tognon , Roland Siegwart

In this paper, an adaptive super-twisting controller is designed for an agile maneuvering quadrotor unmanned aerial vehicle to achieve accurate trajectory tracking in the presence of external disturbances. A cascaded control architecture is…

系统与控制 · 电气工程与系统科学 2023-09-15 D. M. K. K. Venkateswara Rao , Hamed Habibi , Jose Luis Sanchez-Lopez , Prathyush P. Menon , Christopher Edwards , Holger Voos

This paper presents the development of a sliding mode controller using the backstepping approach. The controller is employed to synthesize tracking errors and Lyapunov functions. A novel state-space representation is formulated by…

系统与控制 · 电气工程与系统科学 2025-11-21 Thien Nhan Vo

Unmanned aerial vehicle (UAV) with slung load system is a classic air transportation system. In practical applications, the suspension point of the slung load does not always align with the center of mass (CoM) of the UAV due to mission…

系统与控制 · 电气工程与系统科学 2026-01-13 Zongyang Lv , Yanmei Jia , Yongqing Liu , Alan F. Lynch , Qing Zhao , Yuhu Wu

Aerial manipulator, which is composed of an UAV (Unmanned Aerial Vehicle) and a multi-link manipulator and can perform aerial manipulation, has shown great potential of applications. However, dynamic coupling between the UAV and the…

机器人学 · 计算机科学 2024-01-12 Guangyu Zhang , Yuqing He , Bo Dai , Feng Gu , Jianda Han , Guangjun Liu

Multi-robot formation control has various applications in domains such as vehicle troops, platoons, payload transportation, and surveillance. Maintaining formation in a vehicle platoon requires designing a suitable control scheme that can…

机器人学 · 计算机科学 2026-03-17 Rishabh Dev Yadav

This paper presents an agile Unmanned Aerial Vehicle (UAV) landing control by considering the effect of ship's oscillations and moving, and also disturbance (i.e., crosswind) is considered. The presented control system can make the…

系统与控制 · 电气工程与系统科学 2024-11-11 James Mordaunt , Xinhua Wang

Satellite dynamics in unknown environments are inherently uncertain due to factors such as varying gravitational fields, atmospheric drag, and unpredictable interactions with space debris or other celestial bodies. Traditional sliding mode…

系统与控制 · 电气工程与系统科学 2025-05-13 Rakesh Kumar Sahoo , Manoranjan Sinha

Autonomous unpowered flight is a challenge for control and guidance systems: all the energy the aircraft might use during flight has to be harvested directly from the atmosphere. We investigate the design of an algorithm that optimizes the…

机器学习 · 计算机科学 2017-07-19 Erwan Lecarpentier , Sebastian Rapp , Marc Melo , Emmanuel Rachelson

Unmanned aircraft systems can perform some more dangerous and difficult missions than manned aircraft systems. In some highly complicated and changeable tasks, such as air combat, the maneuvering decision mechanism is required to sense the…

机器人学 · 计算机科学 2019-08-29 Zhencai Hu , Peng Gao , Fei Wang

Within the missile guidance and control system the autopilot must overcome an array of variables and uncertainties to maintain tracking trajectory. A large uncertainty explored in this paper is the difference between the assumed flight…

系统与控制 · 电气工程与系统科学 2024-11-12 Eerik Cockin , Xinhua Wang
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