Applying LESO for Disturbance Rejection of Space Station

Author:

Liu Ping1,Sun Wei Jie1

Affiliation:

1. South China University of Technology

Abstract

In this paper, a combing method based on the linear extended state observer (LESO) and the LQR controller is presented. The LESO is applied to estimate the total disturbance of the space station, and an effective disturbance compensation strategy is proposed for the attitude control and moment management. The simulation results illustrate this method is effective

Publisher

Trans Tech Publications, Ltd.

Reference8 articles.

1. Han J.Q. The Extended State Observer, of a Class of Uncertain Systems [J]. Control and Decision, 1995, 10(1): 85- 88.

2. Han J.Q. Active Disturbance Rejection Control [M]. Beijing: National Defense Industry Press, (2007).

3. Yuan G.P., Shi X.P., Li L. Adaptive Controller for Spacecraft Attitude Maneuver Based on Extended State Observer [J]. Chinese Space Science and Technology, 2011, 10(5): 9-17.

4. Wu Z., Huang L.Y., Wei K.M., Guo L. Active Disturbance Rejection of Attitude for Spacecraft [J]. Control Theory &Applications, 2013, 30(12): 1617-1622.

5. Mapar J. Innovative Approach to the Momentum Management Control for Space Station Freedom [J]. Journal of Guidance, Control and Dynamics, 1993, 16(1): 175-181.

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