H∞ Inverse Optimal Adaptive Fault-Tolerant Attitude Control for Flexible Spacecraft with Input Saturation

LONG Hai-hui (龙海辉), ZHAO Jian-kang*(赵健康), LAI Jian-qing (赖剑清)

Journal of shanghai Jiaotong University (Science) . 2015, (5): 513 -527 . DOI: 10.1007/s12204-015-1659-y