Attitude tracking control of flexible spacecraft with large amplitude slosh

Deng, Mingle; Yue, Baozeng

doi:10.1007/s10409-017-0700-9

Cited by 12 publications

(4 citation statements)

References 15 publications

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“…To accomplish space missions, the flexible satellite needs to track desired attitude signal by real-time attitude manoeuvre. 1,2 Due to the highaccuracy tracking demands for flexible satellites, many attitude tracking control methods such as robust control, [3][4][5] sliding mode control (SMC) 6,7 and adaptive control 8,9 have been proposed to achieve ideal attitude tracking performance. In Zhu et al, 10 a stable flexible satellite attitude tracking result was obtained based on the nonsingular terminal SMC and adaptive control methods.…”

Section: Introductionmentioning

confidence: 99%

Composite attitude fault tolerant tracking control for flexible satellite with time delay

Xiao-li

Shao

et al. 2021

Proceedings of the Institution of Mechanical Engineers, Part G:

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This article deals with the problem of attitude tracking control for flexible satellite under flexible vibration disturbance, actuator fault and time delay. Based on disturbance observer and fault tolerant control techniques, the flexible vibration disturbance and actuator fault are effectively estimated by disturbance observer and fault estimation observer, respectively. Meanwhile, a delay-dependent attitude tracking feedback controller is designed to ensure that the reference attitude is stably tracked. To reduce the conservatism of the designed algorithm, a time delay correlative decomposition factor is introduced to make the flexible satellite have a better performance for attitude tracking control. Finally, the effectiveness of the proposed method is illustrated by numerical simulations.

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Section: Introductionmentioning

confidence: 99%

Composite attitude fault tolerant tracking control for flexible satellite with time delay

Xiao-li

Shao

et al. 2021

Proceedings of the Institution of Mechanical Engineers, Part G:

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“…Haghighi and Pang (2018) developed a control framework to achieve formation flight of a group of underactuated nanosatellites – the controller is designed by using an adaptive finite-time attitude controller. Deng and Yue (2017a) focused on the attitude tracking control of a spacecraft with flexible appendage and partially liquid-filled propellant tank. Deng and Yue (2017b) established the mathematical model of a spacecraft with large amplitude propellant sloshing and depletion, and studied the position and attitude maneuver using an adaptive sliding mode controller.…”

Section: Introductionmentioning

confidence: 99%

Attitude maneuver control of liquid-filled spacecraft with unknown inertia and disturbances

Song

2019

Journal of Vibration and Control

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The attitude maneuver dynamics and control strategy for a fuel-filled spacecraft with uncertain inertia and external disturbances are studied. The mathematical model of a three-axis stabilized spacecraft is established based on the law of conservation of momentum, and the liquid fuel inside the partially-filled fuel tank is represented by an equivalent two-mode spring-mass model. The adaptive sliding mode control law is designed for this kind of underactuated system, and the Lyapunov stability analysis guarantees that all system trajectories reach and remain on the sliding surface. Then, the multiple mode input shapers are used to suppress the sloshing of the fluid fuel. The numerical results show good performance and effectiveness of the control strategy.

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“…Storage tank is one of the basic components for spacecraft, in which the behavior of liquid is mostly responsible for the safety, stability, fuel supply, and so on. Correspondingly, researchers pay close attentions to the shape of free surface (Kulev and Dreyer 2010;Park et al 2015;Zhou et al 2016;Zwicke et al 2017), the pressure control inside tank (Lopez et al 2008; Barsi and Kassemi 2013;Chen and Liang 2013;Kassemi and Kartuzova 2016), the liquid sloshing (Zhou and Huang 2015;Deng and Yue 2017), and the measurement of the residual liquid. Among these aspects, the dynamic evolution of the free surface of the liquid inside tank is the key topic, which is principally determined by the surface tension force in microgravity environment.…”

Section: Introductionmentioning

confidence: 99%

“…Monaghan and Meriaux (2018) numerically studied the two-dimensional turbulence near free surface based on smoothed particle hydrodynamics (SPH). Deng and Yue (2017) focused on attitude tracking control of a spacecraft with partially filled tank. They found that the improved moving pulsating ball model (MPBM) was useful for an approximate estimates of the liquid's location.…”

Section: Introductionmentioning

confidence: 99%

Dynamic Behaviors of Liquid in Partially Filled Tank in Short-term Microgravity

Lin

Zhao

et al. 2018

Microgravity Sci. Technol.

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The oscillation of liquid/gas free surface in a partially filled storage tank caused by an abrupt drop of gravity level is of critical importance for the fluids management in space. In present study we investigate the dynamic behavior of free surface in tank models (tubes) using water as the working medium utilizing the Drop Tower Beijing, which can provide a 3.6s short-term microgravity condition. Meanwhile, the corresponding numerical simulation using volume of fluids (VOF) methods was carried out. It is shown that the dynamic behavior of free surface, which belongs to the typical phenomenon of capillary flow, is affected by the properties of working medium and the geometry and surface properties of the storage tank (especially the contact angle) jointly. The numerical simulation could capture the major characteristic oscillation frequency of free surface revealed by experiment. The oscillation frequency of free surface increases with the increasing air fraction and remains nearly constant at large air fraction. For the same air fraction, the oscillation frequency significantly increases with the decreasing tank diameter. Keywords Storage tank • Dynamic behavior • Oscillation frequency • Microgravity Ji-Cheng LI performed the numerical simulation and experimental data processing. Hai LIN carried out the experiment.

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Attitude tracking control of flexible spacecraft with large amplitude slosh

Cited by 12 publications

References 15 publications

Composite attitude fault tolerant tracking control for flexible satellite with time delay

Composite attitude fault tolerant tracking control for flexible satellite with time delay

Attitude maneuver control of liquid-filled spacecraft with unknown inertia and disturbances

Dynamic Behaviors of Liquid in Partially Filled Tank in Short-term Microgravity

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