Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits
Work
Year: 2008
Type: article
Source: Nonlinear Dynamics
Author Qinglei Hu
Institution Harbin Institute of Technology
Cites: 36
Cited by: 137
Related to: 10
FWCI: 9.912
Citation percentile (by year/subfield): 98.09
Subfield: Control and Systems Engineering
Field: Engineering
Domain: Physical Sciences
Sustainable Development Goal Affordable and clean energy
Open Access status: closed