2013 Fiscal Year Final Research Report
Research of the pendulum gravity control postural stabilization flight robot using dynamic inversion control
| Project/Area Number |
23560963
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| Research Category |
Grant-in-Aid for Scientific Research (C)
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| Allocation Type | Multi-year Fund |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | National Institute of Advanced Industrial Science and Technology |
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Principal Investigator |
IWATA Kakuya 独立行政法人産業技術総合研究所, 知能システム研究部門, 主任研究員 (70356533)
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| Project Period (FY) |
2011 – 2013
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| Keywords | 無人航空機 |
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| Research Abstract |
The design of an inclusion control circuit and the manufacture of an electric circuit which put into dynamic inversion control software were performed, and it built in the test prototype of 1/3 scale, and conducted the attitude control experiment of as opposed to aerial disturbance for an experiment. It became clear that the effect which controls rolling motion is reduced by combining angular velocity sensor (gyroscope sensor) feedback and the angular acceleration sensor of a high sampling frequency. Using these results, in the Niigata sky project, the research and development of the turbojet engine which is a lightweight body, development of the electric high thrust control actuator of 2 axes, and lightweight body using a carbon fiber composite material is developed, and a pendulum stable control type unmanned aerial vehicle is manufactured.
Real application of the result of research is aimed at.
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