Nonlinear Attitude Control for Spacecraft

Li Na Wang; Bing Wang

doi:10.4028/www.scientific.net/AMM.394.421

Paper Titles

Velocity Tracking Control for Hydraulic Lifting System Based on Adaptive PSD Controller
p.398

Self-Tuning Fuzzy Adaptive PID Pitch Control of Wind Power Systems
p.404

Region Merging Based Segmentation with Cellular Automaton
p.410

Experimental Study on a Gyromagnetic Piezo-Cantilever Generator
p.416

Nonlinear Attitude Control for Spacecraft
p.421

Robust Control Analysis Techniques Applied to a Mini Aircraft
p.427

A Design of Multi-Band UHF Sensor for Partial Discharge Detection
p.435

Teleoperated Robotic Cleaning Systems for Use in a Hazardous Radioactive Environment
p.441

Learning from Demonstration with State Based Obstacle Avoidance for Mobile Service Robots
p.448

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 394Nonlinear Attitude Control for Spacecraft

Nonlinear Attitude Control for Spacecraft

Abstract:

In this paper the spacecraft attitude stability problem with external disturbance are considered. A nonlinear attitude controller introducing disturbance suppression for spacecraft is designed using internal model principle. The effectiveness and robustness are demonstrated through a series of numerical simulations.

You might also be interested in these eBooks

Mechatronics, Applied Mechanics and Energy Engineering

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 394)

Pages:

421-426

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.394.421

Citation:

Cite this paper

Online since:

September 2013

Authors:

Li Na Wang, Bing Wang

Keywords:

External Disturbance, Nonlinear Control, Quaternion, Spacecraft Attitude

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] S. M. Joshi, A.G. Kelkar, J. T. Wen. Robust Attitude Stabilization of Spacecraft Using Nonlinear Quaternion Feedback. IEEE Transactions on Automatic Control. Vol. 40, (1995), pp.1800-1803.

DOI: 10.1109/9.467669

Google Scholar

[2] P. Tsiotras. Further Passivity Results for the Attitude Control Problem. IEEE Transactions on Automatic Control. Vol. 43, (1998), pp.1597-1600.

DOI: 10.1109/9.728877

Google Scholar

[3] T. A. Dwyer, R. H. Sira. Variable-Structure Control of Spacecraft Attitude Maneuvers. Journal of Guidance, Control and Dynamics. Vol. 11, (1988), pp.262-270.

DOI: 10.2514/3.20303

Google Scholar

[4] F. Alonge, F. Dippolito, F. M. Raimondi. Globally Convergent Adaptive and Robust Control of Robotic Manipulators for Trajectory Tracking. Control Engineering Practice, Vol. 12, (2004), pp.1091-1100.

DOI: 10.1016/j.conengprac.2003.11.007

Google Scholar

[5] S. H. Dong, S. H. Li. Stabilization of the Attitude of A Rigid Spacecraft with External Disturbances Using Finite-Time Control Techniques. Aerospace Science and Technology, Vol. 13, (2009), pp.256-265.

DOI: 10.1016/j.ast.2009.05.001

Google Scholar

[6] Z. W. Sun, S. N. Wu, H. Li. Variable Structure Attitude Control of Staring Mode Spacecraft with Disturbance Observer. Journal of Harbin Institute of Technology. Vol. 42, (2010), pp.1374-1378.

Google Scholar

[7] Y. Q. Xia, Zh. Zhu, M. Y. Fu, Sh. Wang. Attitude Tracking of Rigid Spacecraft with Bounded Disturbances. IEEE Transactions on Industrial Electronics, (2011), pp.647-659.

DOI: 10.1109/tie.2010.2046611

Google Scholar