Fixed-Time Attitude Tracking Control for Spacecraft With Input Quantization

This paper investigates the fixed-time attitude tracking control problem for rigid spacecraft with input quantization and external disturbances. A novel fixed-time disturbance observer is designed to estimate unknown disturbances. By using adding a power integrator technique, a fixed-time controller is constructed, which can guarantee system states converge to a neighborhood of origin in fixed time. The parameter of quantizer can be coarsely chosen. Finally, simulation results are employed to demonstrate the effectiveness of the developed control scheme.

[1]  Sahjendra N. Singh,et al.  Nonlinear decoupling sliding mode control and attitude control of spacecraft , 1989 .

[2]  Baolin Wu.  Spacecraft Attitude Control with Input Quantization , 2016 .

[3]  M. Shuster.  A survey of attitude representation , 1993 .

[4]  Verzekeren Naar Sparen,et al.  Cambridge , 1969, Humphrey Burton: In My Own Time.

[5]  M. Basin,et al.  Multivariable continuous fixed-time second-order sliding mode control: design and convergence time estimation , 2017 .

[6]  Neil Genzlinger.  A. and Q , 2006 .

[7]  Yuanqing Xia,et al.  Finite-Time Tracking Control of Rigid Spacecraft Under Actuator Saturations and Faults , 2018, IEEE Transactions on Automation Science and Engineering.

[8]  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.

[9]  Andrey Polyakov,et al.  Nonlinear Feedback Design for Fixed-Time Stabilization of Linear Control Systems , 2012, IEEE Transactions on Automatic Control.

[10]  Guang-Hong Yang,et al.  Adaptive Backstepping Stabilization of Nonlinear Uncertain Systems With Quantized Input Signal , 2014, IEEE Transactions on Automatic Control.

[11]  John T. Wen,et al.  Attitude control without angular velocity measurement: a passivity approach , 1995, Proceedings of 1995 IEEE International Conference on Robotics and Automation.

[12]  Christopher J. Damaren,et al.  Geometric Approach to Spacecraft Attitude Control Using Magnetic and Mechanical Actuation , 2010 .

[13]  An-Min Zou,et al.  Adaptive attitude control of spacecraft without velocity measurements using Chebyshev neural network , 2010 .

[14]  Zongyu Zuo,et al.  A new class of finite-time nonlinear consensus protocols for multi-agent systems , 2014, Int. J. Control.

[15]  P. Tsiotras.  Stabilization and optimality results for the attitude control problem , 1996 .

[16]  J. Junkins,et al.  Stereographic Orientation Parameters for Attitude Dynamics: A Generalization of the Rodrigues Parameters , 1996 .

[17]  Linlin Hou,et al.  Disturbance attenuation and rejection for stochastic Markovian jump system with partially known transition probabilities , 2018, Autom..

[18]  Michael I. Friswell,et al.  Fixed-time rendezvous control of spacecraft with a tumbling target under loss of actuator effectiveness , 2016, IEEE Transactions on Aerospace and Electronic Systems.

[19]  Yuanqing Xia,et al.  Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation , 2011, IEEE Transactions on Industrial Electronics.

[20]  Guang-Hong Yang,et al.  Adaptive asymptotic tracking control of uncertain nonlinear systems with input quantization and actuator faults , 2016, Autom..

[21]  Wei Lin,et al.  A continuous feedback approach to global strong stabilization of nonlinear systems , 2001, IEEE Trans. Autom. Control..

[22]  Michael I. Friswell,et al.  Fixed-Time Attitude Control for Rigid Spacecraft With Actuator Saturation and Faults , 2016, IEEE Transactions on Control Systems Technology.

[23]  W. Marsden.  I and J , 2012 .

[24]  Xiaowei Yu,et al.  Adaptive Backstepping Quantized Control for a Class of Nonlinear Systems , 2017, IEEE Transactions on Automatic Control.