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Magnetic attitude tracking control of gravity gradient microsatellite in orbital transfer

Published online by Cambridge University Press:  04 September 2019

Liang Sun Open the ORCID record for Liang Sun [Opens in a new window] ,
Zhiwen Wang ,
Guowei Zhao  and
Hai Huang
Liang Sun
Affiliation:
School of Astronautics, BeihangUniversity and Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies, Ministry of EducationChina
Zhiwen Wang
Affiliation:
School of Astronautics, BeihangUniversity and Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies, Ministry of EducationChina
Guowei Zhao*
Affiliation:
School of Astronautics, BeihangUniversity and Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies, Ministry of EducationChina
Hai Huang
Affiliation:
School of Astronautics, BeihangUniversity and Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies, Ministry of EducationChina
*
zhaoguowei@buaa.edu.cn
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Abstract

The problem of the magnetic attitude tracking control is studied for a gravity gradient microsatellite in orbital transfer. The contributions of the work are mainly shown in two aspects: (1) the design of an expected attitude trajectory; (2) a method of the magnetic attitude tracking control. In orbital transfer, the gravity gradient microsatellite under a constant thrust shows complicated dynamic behaviours. In order to damp out the pendular motion, the gravity gradient microsatellite is subject to the the attitude tracking problem. An expected attitude trajectory is designed based on dynamic characteristics revealed in the paper, which not only ensures the flight safety of the system, but also reduces the energy consumption of the controller. Besides, the control torque produced by a magnetorquer is constrained to lie in a two-dimensional plane orthogonal to the magnetic field, so an auxiliary compensator is proposed to improve the control performance, which is different from existing magnetic control methods. In addition, a sliding mode control based on the compensator is presented, and the Lyapunov stability analysis is performed to show the global convergence of the tracking error. Finally, a numerical case of the gravity gradient microsatellite is studied to demonstrate the effectiveness of the proposed tracking control.

Keywords

Gravity gradientMagnetic controlAttitude trackingElectric thrust
Type
Research Article
Information
The Aeronautical Journal , Volume 123 , Issue 1269 , November 2019 , pp. 1881 - 1894
Copyright
© Royal Aeronautical Society 2019 

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References

REFERENCES

Burton, R., Rock, S., Springmann, J. and Cutler, J. Online attitude determination of a passively magnetically stabilized spacecraft, Acta Astronautica, April 2017, 133, pp 269–281.CrossRefGoogle Scholar
Vatankhahghadim, B. and Damaren, C.J. Magnetic attitude control with impulsive thrusting using the hybrid passivity theorem, Journal of Guidance, Control and Dynamics, August 2017, 40, (8), pp 1860–1876.CrossRefGoogle Scholar
Ehrpais, H., Kutt, J., Kulu, E., Slavinskis, A. and Noorma, M. Nanosatellite spin-up using magnetic actuators: ESTCube-1 flight results, Acta Astronautica, November–December 2016, 128, pp 210–216.CrossRefGoogle Scholar
Inamori, T., Otsuki, K. and Sugawara, Y. Three-axis attitude control by two-step rotations using only magnetic torquers in a low Earth orbit near the magnetic equator, Acta Astronautica, November–December 2016, 128, pp 696–706.CrossRefGoogle Scholar
Walker, A.R. and Putman, P.T. Solely Magnetic Genetic/Fuzzy-Attitude-Control Algorithm for a CubeSat, Journal of Spacecraft and Rockets, November 2015, 52, (6), pp 1627–1639.CrossRefGoogle Scholar
Rodriquez-Vazquez, A.L., Martin-Prats, M.A. and Bernelli-Zazzer, F. Spacecraft magnetic attitude control using approximating sequence Riccati equations, IEEE Transactions on Aerospace and Electronic Systems, October 2015, 51, (4), pp 3374–3385.CrossRefGoogle Scholar
Ovchinnikov, M.Y., Roldugin, D.S., Penkov, V.I., Tkachev, S.S. and Mashtakov, Y.V. Fully magnetic sliding mode control for acquiring three-axis attitude, Acta Astronautica, April–May 2016, 121, pp 59–62.CrossRefGoogle Scholar
Luo, W.W. and Zhou, B. Magnetic attitude control of bias momentum spacecraft by bounded linear feedback, Aerospace Science and Technology, November 2017, 70, pp 419–427.CrossRefGoogle Scholar
Huang, X. and Yan, Y. Fully Actuated Spacecraft Attitude Control via the Hybrid Magnetocoulombic and Magnetic Torques, Journal of Guidance, Control and Dynamics, December 2017, 40, (12), pp 3353–3360.CrossRefGoogle Scholar
Zhou, K.X., Huang, H., Wang, X.S. and Sun, L. Magnetic attitude control for Earth-pointing satellites in the presence of gravity gradient, Aerospace Science and Technology, January 2017, 60, (12), pp 115–123.CrossRefGoogle Scholar
Lovera, M. and Astolfi, A. Global magnetic attitude control of spacecraft in the presence of gravity gradient, IEEE Transaction on Aerospace Electronic Systems, July 2006, 42, (3), pp 796–805.CrossRefGoogle Scholar
Sofyali, A., Jafarov, E.M. and Wisniewski, R. Robust and global attitude stabilization of magnetically actuated spacecraft through sliding mode, Aerospace Science and Technology, May 2018, 76, pp 91–104.CrossRefGoogle Scholar
Zhu, R.Z. and Wang, X.G. Continuous constant thrust maneuver in polar coordinate system, Spacecraft Engineering, 2008, 17, (2), pp 31–37.Google Scholar
Chovotov, V.A. Spacecraft attitude dynamics and control, NASA Sti/recon Technical Report A, 1991, 92, (2), pp 195–221.Google Scholar
Bechlioulis, C.P. and Rovithakis, G.A. Adaptive control with guaranteed transient and steady state tracking error bounds for strict feedback systems, Automatica, 2009, 45, (2), pp 532–538.CrossRefGoogle Scholar
Vadali, S.R. Variable-structure control of spacecraft large-angle maneuvers, Journal of Guidance, Control and Dynamics, 1986, 9, (2), pp 235–239.CrossRefGoogle Scholar