Actuator Layout Optimization for Active Vibration Control of Rigid-Flexible Spacecraft Using Genetic Algorithm

Zeqiang Han; Hongwei Xia; Xudong Li; Haoran Sun; Zening Li; Guangcheng Ma

doi:10.1007/978-981-96-4652-4_57

Actuator Layout Optimization for Active Vibration Control of Rigid-Flexible Spacecraft Using Genetic Algorithm

Zeqiang Han^*
, Hongwei Xia
, Xudong Li
, Haoran Sun
, Zening Li
, Guangcheng Ma

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology
Shanghai Key Laboratory of Space Intelligent Control Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

This paper considers the actuator installation optimization problem of the flexible appendage to control the vibration when rigid-flexible spacecraft is in large-range planar motion. Firstly, a novel dynamic model is obtained using Hamilton’s principle containing more nonlinear terms. The vibration is decomposed with the Rayleigh–Ritz method. Based on the new model and Euler–Bernoulli beam theory, a new cost function is proposed to describe the energy cost of the vibration controller. In addition, Genetic Algorithm is used to optimize the installation positions. Eventually, the optimal installation of actuators is calculated with the optimization algorithm, and numerical simulations are presented to compare the control effect in different installation positions.

Original language	English
Title of host publication	Proceeding of the 10th CSA-IAA Conference on Advanced Space Technology - Space in Future
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	821-831
Number of pages	11
ISBN (Print)	9789819646517
DOIs	https://doi.org/10.1007/978-981-96-4652-4_57
State	Published - 2026
Event	10th CSA-IAA Conference on Advanced Space Technology, CSA-IAA 2023 - Shanghai, China Duration: 13 Sep 2023 → 16 Sep 2023

Publication series

Name	Lecture Notes in Mechanical Engineering
Volume	Part94
ISSN (Print)	2195-4356
ISSN (Electronic)	2195-4364

Conference

Conference	10th CSA-IAA Conference on Advanced Space Technology, CSA-IAA 2023
Country/Territory	China
City	Shanghai
Period	13/09/23 → 16/09/23

Access to Document

10.1007/978-981-96-4652-4_57

Cite this

Han, Z., Xia, H., Li, X., Sun, H., Li, Z., & Ma, G. (2026). Actuator Layout Optimization for Active Vibration Control of Rigid-Flexible Spacecraft Using Genetic Algorithm. In Proceeding of the 10th CSA-IAA Conference on Advanced Space Technology - Space in Future (pp. 821-831). (Lecture Notes in Mechanical Engineering; Vol. Part94). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-96-4652-4_57

@inproceedings{6c766c67fad244a59b3867e9be6d4b14,

title = "Actuator Layout Optimization for Active Vibration Control of Rigid-Flexible Spacecraft Using Genetic Algorithm",

abstract = "This paper considers the actuator installation optimization problem of the flexible appendage to control the vibration when rigid-flexible spacecraft is in large-range planar motion. Firstly, a novel dynamic model is obtained using Hamilton{\textquoteright}s principle containing more nonlinear terms. The vibration is decomposed with the Rayleigh{\textendash}Ritz method. Based on the new model and Euler{\textendash}Bernoulli beam theory, a new cost function is proposed to describe the energy cost of the vibration controller. In addition, Genetic Algorithm is used to optimize the installation positions. Eventually, the optimal installation of actuators is calculated with the optimization algorithm, and numerical simulations are presented to compare the control effect in different installation positions.",

author = "Zeqiang Han and Hongwei Xia and Xudong Li and Haoran Sun and Zening Li and Guangcheng Ma",

note = "Publisher Copyright: {\textcopyright} Chinese Society of Astronautics 2026.; 10th CSA-IAA Conference on Advanced Space Technology, CSA-IAA 2023 ; Conference date: 13-09-2023 Through 16-09-2023",

year = "2026",

doi = "10.1007/978-981-96-4652-4\_57",

language = "英语",

isbn = "9789819646517",

series = "Lecture Notes in Mechanical Engineering",

publisher = "Springer Science and Business Media Deutschland GmbH",

pages = "821--831",

booktitle = "Proceeding of the 10th CSA-IAA Conference on Advanced Space Technology - Space in Future",

address = "德国",

}

Han, Z, Xia, H, Li, X, Sun, H, Li, Z & Ma, G 2026, Actuator Layout Optimization for Active Vibration Control of Rigid-Flexible Spacecraft Using Genetic Algorithm. in Proceeding of the 10th CSA-IAA Conference on Advanced Space Technology - Space in Future. Lecture Notes in Mechanical Engineering, vol. Part94, Springer Science and Business Media Deutschland GmbH, pp. 821-831, 10th CSA-IAA Conference on Advanced Space Technology, CSA-IAA 2023, Shanghai, China, 13/09/23. https://doi.org/10.1007/978-981-96-4652-4_57

Actuator Layout Optimization for Active Vibration Control of Rigid-Flexible Spacecraft Using Genetic Algorithm. / Han, Zeqiang; Xia, Hongwei; Li, Xudong et al.
Proceeding of the 10th CSA-IAA Conference on Advanced Space Technology - Space in Future. Springer Science and Business Media Deutschland GmbH, 2026. p. 821-831 (Lecture Notes in Mechanical Engineering; Vol. Part94).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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N2 - This paper considers the actuator installation optimization problem of the flexible appendage to control the vibration when rigid-flexible spacecraft is in large-range planar motion. Firstly, a novel dynamic model is obtained using Hamilton’s principle containing more nonlinear terms. The vibration is decomposed with the Rayleigh–Ritz method. Based on the new model and Euler–Bernoulli beam theory, a new cost function is proposed to describe the energy cost of the vibration controller. In addition, Genetic Algorithm is used to optimize the installation positions. Eventually, the optimal installation of actuators is calculated with the optimization algorithm, and numerical simulations are presented to compare the control effect in different installation positions.

AB - This paper considers the actuator installation optimization problem of the flexible appendage to control the vibration when rigid-flexible spacecraft is in large-range planar motion. Firstly, a novel dynamic model is obtained using Hamilton’s principle containing more nonlinear terms. The vibration is decomposed with the Rayleigh–Ritz method. Based on the new model and Euler–Bernoulli beam theory, a new cost function is proposed to describe the energy cost of the vibration controller. In addition, Genetic Algorithm is used to optimize the installation positions. Eventually, the optimal installation of actuators is calculated with the optimization algorithm, and numerical simulations are presented to compare the control effect in different installation positions.

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BT - Proceeding of the 10th CSA-IAA Conference on Advanced Space Technology - Space in Future

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T2 - 10th CSA-IAA Conference on Advanced Space Technology, CSA-IAA 2023

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Han Z, Xia H, Li X, Sun H, Li Z, Ma G. Actuator Layout Optimization for Active Vibration Control of Rigid-Flexible Spacecraft Using Genetic Algorithm. In Proceeding of the 10th CSA-IAA Conference on Advanced Space Technology - Space in Future. Springer Science and Business Media Deutschland GmbH. 2026. p. 821-831. (Lecture Notes in Mechanical Engineering). doi: 10.1007/978-981-96-4652-4_57

Actuator Layout Optimization for Active Vibration Control of Rigid-Flexible Spacecraft Using Genetic Algorithm

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