Attitude Control of Spherical Liquid-Filled Spacecraft Based on High-Order Fully Actuated System Approaches
查看参考文献22篇
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文摘
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The attitude of spherical liquid-filled spacecraft is controlled based on the high-order fully actuated system approaches. The rigid-fluid coupling dynamic equation can be established in terms of the Euler angles of the spacecraft and the angular velocities of the liquid fuel. According to the dynamic equation, three kinds of input selections are presented. In the case of one control input, the dynamic equation is transformed into the third-order or the second-order differential equations of the Euler angle by the high-order fully actuated system approaches. Then a control law is designed to track the target. The effectiveness of the control law is demonstrated by numerical simulations. |
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来源
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Journal of Systems Science and Complexity
,2022,35(2):471-480 【核心库】
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DOI
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10.1007/s11424-022-2055-y
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关键词
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Attitude control
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high-order fully actuated system approaches
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spherical liquid-filled spacecraft
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地址
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School of Science, Harbin Institute of Technology (Shenzhen), Shenzhen, 518055
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语种
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英文 |
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文献类型
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研究性论文 |
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ISSN
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1009-6124 |
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学科
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自动化技术、计算机技术;航天(宇宙航行) |
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基金
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国家自然科学基金
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文献收藏号
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CSCD:7238855
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参考文献 共
22
共2页
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1.
Yang D D. Attitude maneuver of liquid-filled spacecraft with a flexible appendage by momentum wheel.
Acta Mechanica Sinica,2012,28(2):543-550
|
CSCD被引
4
次
|
|
|
|
|
2.
Shi X Y. Using sliding mode control method to suppress fuel sloshing of a liquidfilled spacecraft.
The 27th Chinese Control and Decision Conference (2015 CCDC),2015:1268-1273
|
CSCD被引
1
次
|
|
|
|
|
3.
Zhang H H. Attitude control and sloshing suppression for liquid-filled spacecraft in the presence of sinusoidal disturbance.
Journal of Sound and Vibration,2016,383:64-75
|
CSCD被引
4
次
|
|
|
|
|
4.
Deng M L. Attitude dynamics and control of liquid filled spacecraft with large amplitude fuel slosh.
Journal of Mechanics,2017,33(1):125-136
|
CSCD被引
7
次
|
|
|
|
|
5.
Deng M L. Position and attitude control of spacecraft with large amplitude propellant slosh and depletion.
Journal of Aerospace Engineering,2017,30(6):04017075
|
CSCD被引
1
次
|
|
|
|
|
6.
Huo J H. Adaptive prediction backstepping attitude control for liquidfilled micro-satellite with flexible appendages.
Acta Astronautica,2018,152:557-566
|
CSCD被引
3
次
|
|
|
|
|
7.
Deng M L. Attitude tracking control of flexible spacecraft with large amplitude slosh.
Acta Mechanica Sinica,2017,33(6):1095-1102
|
CSCD被引
1
次
|
|
|
|
|
8.
Liu F. Attitude dynamics and control of spacecraft with a partially filled liquid tank and flexible panels.
Acta Astronautica,2018,143:327-336
|
CSCD被引
13
次
|
|
|
|
|
9.
Deng M L. Attitude dynamics and control of spacecraft with multiple liquid propellant tanks.
Journal of Aerospace Engineering,2016,29(6):04016042
|
CSCD被引
3
次
|
|
|
|
|
10.
Song X J. Attitude maneuver control of liquid-filled spacecraft with unknown inertia and disturbances.
Journal of Vibration and Control,2019,25(8):1460-1469
|
CSCD被引
6
次
|
|
|
|
|
11.
Deng M L. Coupling dynamics of flexible spacecraft filled with liquid propellant.
Journal of Aerospace Engineering,2019,32(5):04019077
|
CSCD被引
1
次
|
|
|
|
|
12.
Song X J. Adaptive backstepping attitude control for liquid-filled spacecraft without angular velocity measurement.
Journal of Aerospace Engineering,2021,34(3):04021021
|
CSCD被引
1
次
|
|
|
|
|
13.
Duan G R. High-order fully actuated system approaches: Part I. Models and basic procedure.
International Journal of Systems Science,2021,52(2):422-435
|
CSCD被引
31
次
|
|
|
|
|
14.
Duan G R. High-order fully actuated system approaches: Part IV. Adaptive control and highorder backstepping.
International Journal of Systems Science,2021,52(5):972-989
|
CSCD被引
21
次
|
|
|
|
|
15.
Duan G R. High-order fully actuated system approaches: Part VIII. Optimal control with application in spacecraft attitude stabilisation.
International Journal of Systems Science,2021,53(1):54-73
|
CSCD被引
4
次
|
|
|
|
|
16.
Duan G R. High-order fully actuated system approaches: Part II. Generalized strict-feedback systems.
International Journal of Systems Science,2021,52(3):437-454
|
CSCD被引
22
次
|
|
|
|
|
17.
Yue B Z. Hybrid control of liquid-filled spacecraft maneuvers by dynamic inversion and input shaping.
AIAA Journal,2014,52(3):618-626
|
CSCD被引
12
次
|
|
|
|
|
18.
Duan G R. High-order fully actuated system approaches: Part V. Robust adaptive control.
International Journal of Systems Science,2021,52(10):2129-2143
|
CSCD被引
21
次
|
|
|
|
|
19.
Duan G R. High-order fully actuated system approaches: Part III. Robust control and high-order backstepping.
International Journal of Systems Science,2021,52(5):952-971
|
CSCD被引
25
次
|
|
|
|
|
20.
Duan G R. High-order fully-actuated system approaches: Part VI. Disturbance attenuation and decoupling.
International Journal of Systems Science,2021,52(10):2161-2181
|
CSCD被引
19
次
|
|
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