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      Detumbling a Non-Cooperative Tumbling Target Using a Low-Thrust Device

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          Abstract

          This paper presents a new detumbling strategy for non-cooperative tumbling targets using a low-thrust device. The device with a harpoon on the front is released from the servicing satellite and embedded in the target. Then, the device’s thrusters are used to reduce the target’s angular velocity. In this paper, an impact model between the target and the device is established based on the conservative principle of linear and angular momentum. The dynamic equation of the combined system after impact is derived based on the principle of virtual power. A detumbling control scheme combining the linear quadratic regulator (LQR), pulse-width pulse-frequency (PWPF) modulation, and particle swarm optimization (PSO) is developed. The continuous optimal control signal obtained by LQR is transformed into a series of pulse signals by a PWPF modulator. To improve the performance of the detumbling controller, the weighting matrices of LQR are optimized by PSO, and two constrained optimization problems are studied. Finally, the effectiveness and robustness of the proposed strategy are verified by numerical simulations.

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          Most cited references35

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          Defining a Standard for Particle Swarm Optimization

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            Solving ODEs with MATLAB

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              Space debris removal system using a small satellite

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                Author and article information

                Contributors
                Journal
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                1533-385X
                08 January 2022
                May 2022
                : 60
                : 5
                : 2718-2729
                Affiliations
                Shanghai Jiao Tong University , 200240 Shanghai, People’s Republic of China
                Shanghai Institute of Aerospace System Engineering , 201109 Shanghai, People’s Republic of China
                Author notes
                [*]

                Ph.D. Candidate, State Key Laboratory of Ocean Engineering, Department of Engineering Mechanics; liuyuanqing@ 123456sjtu.edu.cn .

                [†]

                Associate Professor, State Key Laboratory of Ocean Engineering, Department of Engineering Mechanics; peterliuxiaofeng@ 123456163.com .

                [‡]

                Professor, State Key Laboratory of Ocean Engineering, Department of Engineering Mechanics; caigp@ 123456sjtu.edu.cn (Corresponding Author).

                [§]

                Senior Engineer; xufeng_1976@ 123456126.com .

                [¶]

                Senior Engineer; shermantang@ 123456163.com .

                Article
                J060982 J060982
                10.2514/1.J060982
                fd39c82c-4ddf-4f77-afa8-eaf756086635
                Copyright © 2021 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 07 June 2021
                : 25 October 2021
                : 29 November 2021
                Page count
                Figures: 14, Tables: 4
                Funding
                Funded by: National Natural Science Foundation of Chinahttp://dx.doi.org/10.13039/501100001809
                Award ID: 11772187
                Award ID: 12172215
                Categories
                Regular Articles
                p2263, Fluid Dynamics
                p1804, Aerodynamics
                p3282, Computational Fluid Dynamics
                p28724, Runge-Kutta Methods
                p2228, Aerospace Sciences
                p1986, Aerospace Electronics
                p6797, Space Debris
                p2370, Aerospace Engineering
                p1814, Attitude Control
                p2406, Spacecraft Attitude Control

                Engineering,Physics,Mechanical engineering,Space Physics
                Space Debris,Liquid Sloshing,Schmitt Trigger,Fuel Consumption,Optimal Control,Numerical Simulation,CubeSat,Particle Swarm Optimization,Linear Quadratic Regulator,Thrust

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