Fault-Tolerant Attitude Control for Flexible Spacecraft Without Angular Velocity Magnitude Measurement

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS

AMER INST AERONAUT ASTRONAUT

1. National Natural Science Foundation of China [61004072]
2. Fundamental Research Funds for the Central Universities [HIT.NSRIF.2009003]
3. Research Fund for the Doctoral Program of Higher Education of China [20070213061, 20102302110031]
4. Scientific Research Foundation for the Returned Overseas Chinese Scholars of Harbin [2010RFLXG001]
5. Natural Sciences and Engineering Research Council of Canada