Finite-Time Adaptive Sliding Mode Fault-Tolerant Attitude Control for Flexible Spacecraft
Year: 2025
Type: article
Institutions: Harbin Institute of Technology, Beihang University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G123774316, G5022381051, G7584486368
OpenAlex ID: W4409077344
