Attitude Tracking Control for Rigid-Flexible Coupled Spacecraft with Guaranteed Performance Bounds

[1]  Yan Xiao,et al.  Observer-based continuous finite-time attitude control for rigid–flexible coupling satellites , 2019, Int. J. Control.

[2]  Guanghui Wen,et al.  Leader–Following Attitude Consensus for Spacecraft Formation with Rigid and Flexible Spacecraft , 2016 .

[3]  An-Min Zou,et al.  Distributed attitude synchronization control for a group of flexible spacecraft using only attitude measurements , 2016, Inf. Sci..

[4]  Christopher J. Damaren,et al.  Magnetic Attitude Control of a Flexible Satellite , 2013 .

[5]  Anton H. J. de Ruiter,et al.  Spacecraft Attitude Tracking with Guaranteed Performance Bounds , 2013 .

[6]  Yan Xiao,et al.  Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft , 2018, J. Frankl. Inst..

[7]  S. Gennaro,et al.  Active Vibration Suppression in Flexible Spacecraft Attitude Tracking , 1998 .

[8]  Anton H. J. de Ruiter.  Observer-Based Adaptive Spacecraft Attitude Control With Guaranteed Performance Bounds , 2016, IEEE Transactions on Automatic Control.

[9]  Youmin Zhang,et al.  Fault-Tolerant Attitude Control for Flexible Spacecraft Without Angular Velocity Magnitude Measurement , 2011 .

[10]  Qiang Shen,et al.  Velocity-Free Attitude Reorientation of a Flexible Spacecraft with Attitude Constraints , 2017 .

[11]  Jinjun Shan,et al.  Rotation-Matrix-Based Attitude Tracking for Multiple Flexible Spacecraft with Actuator Faults , 2019, Journal of Guidance, Control, and Dynamics.

[12]  Yan Xiao,et al.  Finite time fault-tolerant attitude control for rigid-flexible coupling satellites based on Legendre neural network , 2018 .

[13]  Chokri Sendi,et al.  Takagi-Sugeno Fuzzy Model-Based Control of Spacecraft with Flexible Appendage , 2014 .

[14]  Shihua Li,et al.  Attitude synchronization control for a group of flexible spacecraft , 2014, Autom..

[15]  S. Di Gennaro,et al.  Output stabilization of flexible spacecraft with active vibration suppression , 2003 .

[16]  S. Di Gennaro,et al.  Passive Attitude Control of Flexible Spacecraft from Quaternion Measurements , 2003 .

[17]  Haichao Gui,et al.  Robustness Analysis and Performance Tuning for the Quaternion Proportional–Derivative Attitude Controller , 2018, Journal of Guidance, Control, and Dynamics.