哈尔滨工业大学学报（英文版）2019，Vol.26Issue(5)：51-59,9.DOI:10.11916/j.issn.1005-9113.18017
Novel Logarithmic Non-Singular Terminal Sliding Mode and Its Application in Attitude Control of QTR
Novel Logarithmic Non-Singular Terminal Sliding Mode and Its Application in Attitude Control of QTR
Haibo Liu 1Heping Wang 1Junlei Sun2
作者信息
- 1. College of Aeronautics,Northwestern Polytechnical University, Xi' an 710072, China
- 2. Shenzhen Research Institute of Northwestern Polytechnical University,Shenzhen 518057,Guangdong, China
- 折叠
摘要
关键词
tilt rotor/nonsingular/sliding mode control/attitude control/reaching law/extended state/disturbance observerKey words
tilt rotor/nonsingular/sliding mode control/attitude control/reaching law/extended state/disturbance observer分类
航空航天引用本文复制引用
Haibo Liu,Heping Wang,Junlei Sun..Novel Logarithmic Non-Singular Terminal Sliding Mode and Its Application in Attitude Control of QTR[J].哈尔滨工业大学学报（英文版）,2019,26(5):51-59,9.
