Abstract
This paper is mainly focused on the attitude dynamics and control of a fuel-filled flexible spacecraft subjected to the thermal payload during eclipse transitions. The flexible appendages are considered as Euler–Bernoulli beams, and the sloshing liquid is modeled as in two modes multi-spring-mass models; the governing equations of this coupled system are developed by using Hamilton’s principle. Numerical results show that the spacecraft attitude responses consist of a quasi-static displacement and superimposed vibration. Then, we design an adaptive sliding mode and use the Lyapunov approach control law to control the attitude disturbance and suppress the thermal jitter and liquid sloshing for the fuel filled flexible spacecraft subject to the thermal payload. Numerical results are presented to verify the efficiency of the hybrid control methods. The results show that the adaptive sliding mode method might be effective to handle the steady-state errors and the Lyapunov control algorithm would suppress the residual vibration.
Graphical Abstract
The attitude dynamics control and vibration suppression are investigated for a fuel-filled spacecraft with single solar panel subjected to thermal bending moment during eclipse transitions.
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Banerjee, A.K., Pedreiro, N., Singhose, W.E.: Vibration reduction for flexible spacecraft following momentum dumping with/without slewing. J. Guid. Control Dyn. 24, 417–427 (2001)
Azadi, M., Fazelzadeh, S.A., Eghtesad, M., et al.: Vibration suppression and adaptive-robust control of a smart flexible satellite with three axes maneuvering. Acta Astronaut. 69, 307–322 (2011)
Hu, Q., Ma, G.: Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver. Aerosp. Sci. Technol. 9, 307–317 (2005)
Azadi, E., Eghtesad, M., Fazelzadeh, S.A., et al.: Vibration suppression of smart nonlinear flexible appendages of a rotating satellite by using hybrid adaptive sliding mode/Lyapunov control. J. Vib. Control 19, 975–991 (2013)
Hu, Q., Xiao, B.: Robust adaptive backstepping attitude stabilization and vibration reduction of flexible spacecraft subject to actuator saturation. J. Vib. Control 17, 1657–1671 (2011)
Krenk, S., Hgsberg, J.: Optimal resonant control of flexible structures. J. Sound Vib. 323, 530–554 (2009)
Hu, Q., Ma, G.: Variable structure maneuvering control and vibration suppression for flexible spacecraft subject to input nonlinearities. Smart Mater. Struct. 15, 1899 (2006)
Qi, N., Dong, K., Wang, X., et al.: Spacecraft propellant sloshing suppression using input shaping technique. In: International conference on computer modeling and simulation, Macau, IEEE, pp. 162–166 (2009)
Yue, B., Zhu, L.M.: Hybrid control of liquid-filled spacecraft maneuvers by dynamic inversion and input shaping. AIAA J. 52, 618–626 (2014)
Pridgen, B., Bai, K., Singhose, W.: Slosh suppression by robust input shaping. In: 49th IEEE conference on decision and control. pp. 2316–2321 (2010)
Cho, S., Mcclamroch, N.H., Reyhanoglu, M.: Feedback control of a space vehicle with unactuated fuel slosh dynamics. In: AIAA guidance, navigation, and control conference and exhibit, Denver (2000)
Kang, J., Coverstone, V.L.: Analytical model for momentum transfer of spacecraft containing liquid. J. Guid. Control Dyn. 33, 991–994 (2010)
Reyhanoglu, M., Hervas, J.R.: Robotically controlled sloshing suppression in point-to-point liquid container transfer. J. Vib. Control 19, 2137–2144 (2013)
Reyhanoglu, M., Hervas, J.R.: Point-to-point liquid container transfer via a PPR robot with sloshing suppression. In: American Control Conference, pp. 5490–5494 (2012)
Yang, D., Yue, B.: Attitude maneuver of spacecraft with long cantilever beam appendage by momentum wheel. Int. J. Control 86, 360–368 (2013)
Yang, D., Yue, B., Wu, W., et al.: Attitude maneuver of liquid-filled spacecraft with a flexible appendage by momentum wheel. Acta Mech. Sin. 28, 543–550 (2012)
Da Fonseca, I.M., Bainum, P.M.: CSI due to sloshing motion on LEO LSS. Adv. Astronaut. Sci. 145, 1073–1086 (2012)
Walchko, K.J.: Robust nonlinear attitude control with disturbance compensation. [Ph.D. Thesis], University of Florida, USA (2003)
Thornton, E.A.: Thermal buckling of plates and shells. Appl. Mech. Rev. 46, 485–506 (1993)
Johnston, J.D., Thornton, E.A.: Thermally induced dynamics of satellite solar panels. J. Spacecr. Rocket. 37, 604–613 (2000)
Johnston, J.D., Thornton, E.A.: Thermally induced attitude dynamics of a spacecraft with a flexible appendage. J. Guid. Control Dyn. 21, 581–587 (1998)
Reyhanoglu, M., Hervas, J.R.: Nonlinear control of space vehicles with multi-mass fuel slosh dynamics. In: 5th International conference on recent advances in space technologies, pp. 247–252 (2011)
Park, S.: Thermally induced attitude disturbance control for spacecraft with a flexible boom. J. Spacecr. Rocket. 39, 325–328 (2002)
Sales, T.P., Rade, D.A., de Souza, L.: Passive vibration control of flexible spacecraft using shunted piezoelectric transducers. Aerosp. Sci. Technol. 29, 403–412 (2013)
Hu, Q.: A composite control scheme for attitude maneuvering and elastic mode stabilization of flexible spacecraft with measurable output feedback. Aerosp. Sci. Technol. 13, 81–91 (2009)
Acknowledgments
The project was supported by the National Natural Science Foundation of China (NNSFC) (Grant 11472041) and the Research Fund for the Doctoral Program of Higher Education of China (Grant 20131101110002).
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Song, XJ., Yue, BZ. & Wu, WJ. Investigation on attitude disturbance control and vibration suppression for fuel-filled flexible spacecraft. Acta Mech. Sin. 31, 581–588 (2015). https://doi.org/10.1007/s10409-015-0431-8
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DOI: https://doi.org/10.1007/s10409-015-0431-8