| Budget Amount *help |
¥4,940,000 (Direct Cost: ¥3,800,000、Indirect Cost: ¥1,140,000)
Fiscal Year 2017: ¥1,300,000 (Direct Cost: ¥1,000,000、Indirect Cost: ¥300,000)
Fiscal Year 2016: ¥2,080,000 (Direct Cost: ¥1,600,000、Indirect Cost: ¥480,000)
Fiscal Year 2015: ¥1,560,000 (Direct Cost: ¥1,200,000、Indirect Cost: ¥360,000)
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| Outline of Final Research Achievements |
The results of the research carried out throughout the research period are summarized as follows: 1) We established LPV control theory via Parameter-Dependent Coordinate Transformation and confirmed its effectiveness and usefulness by actual design calculations and simulations. 2. By moving the boundary between control and steering laws, we made it easy to design GS control systems when there exist scheduling parameters in the input matrix. 3. The target of this research has been extended from the spacecraft attitude control to orbit / vibration control, parabola antenna control, and aircraft gust alleviation. This extends the possibility of applying the LPV control theory to various control subjects in the aerospace field. It is considered that it will contribute to the academic development in this field and greatly contribute to the development of the control technology in the field.
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