Pitch autopilot design using model-following adaptive sliding mode control

被引：9
作者：
Choe, DG
Kim, JH
机构：
[1] Korea Adv Inst Sci & Technol, Dept Elect Engn & Comp Sci, Yusong Ku, Taejon 305701, South Korea
[2] Korea Adv Inst Sci & Technol, Dept Elect Engn & Comp Sci, Yusong Ku, Taejon 305701, South Korea
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2002年 / 25卷 / 04期
关键词：
D O I：
10.2514/2.4954
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The pitch autopilot design using model-following adaptive sliding mode control was presented. The model-following pitch autopilot was presented for a sampled-data system with model uncertainties and disturbances. The proposed controller showed the asymptotic tracking of the pitch acceleration of the reference model and was able to provide robust performance of the system to the model uncertainties and disturbances.
引用
收藏
页码：826 / 829
页数：4
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