Attitude Control for Rigid Satellite Under Actuator Constraint

An attitude controller is proposed via employing backstepping control technique, and being represented by modified Rodriguez parameters. A general dynamic attitude model of satellites is deduced, along with a general model of actuator dynamics which can describe presumably all actuators for space application. External disturbances and actuator constraints are explicitly addressed. The control performance is proved in the numerical simulation experiences at last.

[1]  Maruthi R. Akella,et al.  High-Performance Spacecraft Adaptive Attitude-Tracking Control Through Attracting-Manifold Design , 2008 .

[2]  Yuri B. Shtessel,et al.  Advances in High Order and Adaptive Sliding Mode Control – Theory and Applications , 2011 .

[3]  Marcel J. Sidi,et al.  Spacecraft Dynamics and Control: A Practical Engineering Approach , 1997 .

[4]  Christopher D. Hall,et al.  Spacecraft Dynamics and Control , 2002 .

[5]  John L. Junkins,et al.  Adaptive Control of Nonlinear Attitude Motions Realizing Linear Closed Loop Dynamics , 2001 .

[6]  Brij N. Agrawal,et al.  Adaptive control of uncertain Hamiltonian Multi-Input Multi-Output systems : With application to spacecraft control , 2009, 2008 American Control Conference.

[7]  Tomislav B. Sekara,et al.  Optimization of PID Controller Based on Maximization of the Proportional Gain Under Constraints on Robustness and Sensitivity to Measurement Noise , 2009, IEEE Transactions on Automatic Control.

[8]  Zeng-Guang Hou,et al.  Quaternion-Based Adaptive Output Feedback Attitude Control of Spacecraft Using Chebyshev Neural Networks , 2010, IEEE Transactions on Neural Networks.

[9]  Steven X. Ding,et al.  A Review on Basic Data-Driven Approaches for Industrial Process Monitoring , 2014, IEEE Transactions on Industrial Electronics.

[10]  John L. Crassidis,et al.  Sliding Mode Control Using Modified Rodrigues Parameters , 1996 .

[11]  Maruthi R. Akella,et al.  Separation Property for the Rigid-Body Attitude Tracking Control Problem , 2007 .