论文信息 - Finite Time Fault-Tolerant Control of Spacecraft Rendezvous and Docking Based on Linear Sliding Mode - 字舞流文

Finite Time Fault-Tolerant Control of Spacecraft Rendezvous and Docking Based on Linear Sliding Mode

Fei Han | Xiande Wu | Junting Lv | Wengao Lu | Yong Hao

[1] A. Niederlinski. A heuristic approach to the design of linear multivariable interacting control systems , 1971 .

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

[3] Xiuyun Meng,et al. Mixed H∞/H2 gain-scheduled control for spacecraft rendezvous in elliptical orbits , 2014 .

[4] Wei Huo,et al. Disturbance observer based fault-tolerant control for cooperative spacecraft rendezvous and docking with input saturation , 2017 .

[5] Wei Huo,et al. Adaptive fault-tolerant control for cooperative spacecraft rendezvous and docking , 2017, 2017 American Control Conference (ACC).

[6] Zongli Lin,et al. Lyapunov Differential Equation Approach to Elliptical Orbital Rendezvous with Constrained Controls , 2011 .

[7] Shijie Xu,et al. Approach Guidance with Double-Line-of-Sight Measuring Navigation Constraint for Autonomous Rendezvous , 2011 .

[8] Yuanqing Xia,et al. Attitude stabilization of rigid spacecraft with finite‐time convergence , 2011 .

[9] Q. Hu,et al. Fault-Tolerant Tracking Control of Spacecraft with Attitude-Only Measurement Under Actuator Failures , 2014 .

[10] Krishna Dev Kumar,et al. Fault Tolerant Reconfigurable Satellite Formations Using Adaptive Variable Structure Techniques , 2010 .