Adaptive Integral-type Sliding Mode Control for Spacecraft Attitude Maneuvering Under Actuator Stuck Failures
Failures
24
TB3;O39
National Natural Science Foundation of China61004072;Fundamental Research Funds for the Central UniversitiesHIT.NSRIF.2009003;Research Fund for the Doctoral Program of Higher Education of China20070213061,20102302110031;Scientific Research Foundation for the Returned Overseas Chinese Scholars of Harbin2010RFLXG001
2011-09-15(万方平台首次上网日期,不代表论文的发表时间)
共14页
32-45