제어로봇시스템학회:학술대회논문집
- 2001.10a
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- Pages.166.6-166
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- 2001
Attitude Control of a Vehicle under the Disturbances by Sliding Mode Controller with Reaction Jets
- Son, Sung-Han (Korea Univ.) ;
- Kim, Jinsu (Korea Univ.) ;
- Park, Kang-Bak (Korea Univ.) ;
- Teruo Tsuji (Kyushu Institute of Technology) ;
- Tsuyoshi Hanamoto (Kyushu Institute of Technology)
- Published : 2001.10.01
Abstract
An attitude control of an air vehicle based on the variable structure control is proposed. For an air vehicle, minimum weight is required. Thus, it is desired to reduce the input energy. The optimal state portrait curve using time-varying sliding surface is proposed to reduce the control energy. Tracking performance of the closed loop system is guaranteed under the existence of parameter variation and external disturbances.
Keywords