L1 Adaptive Output Feedback Controller for Tilt-rotor Aircraft

被引：0
|
作者：
Lu, K. [1 ]
Liu, Chunsheng [2 ]
Wang, Zhengzhong [3 ]
Wang, Weihong [4 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Sci & Technol Rotorcraft Aeromech Lab, CHRDl, Jingdezhen 333001, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Jiangsu, Peoples R China
[3] CHRDl, Sci & Technol Aeromech Lab, Jingdezhen 333001, Peoples R China
[4] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
来源：
2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2016年
关键词：
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
this paper considers application of L-1 adaptive output feedback controller to tilt-rotor aircraft longitudinal autopilot design. The proposed adaptive controller has satisfactory performance which meets ADS-33E-PRF Military Rotorcraft handing qualities specifications in the presence of unknown time-varying nonlinearities. Simulations verify the controller,
引用
收藏
页码：2488 / 2491
页数：4
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