Author Info
Name
Affiliation
Papers
XUEHUI LI
Harbin Inst Technol, Ctr Control Theory & Guidance Technol, 92 West Dazhi St, Harbin 150001, Heilongjiang, Peoples R China
1
Collaborators
Citations 
PageRank 
2
1
0.36
Referers 
Referees 
References 
4
46
16
Title
Citations
PageRank
Year
Robust spacecraft attitude tracking control with integral terminal sliding mode surface considering input saturation10.362019