An RPRV Flight Experiment System for the Estimation of the Airplane Aerodynamic Characteristics.
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- HIGASHINO Shin'ichiro
- 九州大学工学部航空工学科
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- MATSUBARA Manabu
- 九州大学工学部航空工学科
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- KUDO Natsuko
- 近畿大学九州工学部計算機センター
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- SAKURAI Akira
- 九州大学工学部航空工学科
Bibliographic Information
- Other Title
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- RPRVを用いた空力特性推定のための飛行実験システム
Abstract
A low-cost, RPRV (Remotely-Piloted Research Vehicle) flight experiment system for the study of the aerodynamic characteristics of airplanes has been developed. The cost has been kept to a minimum by utilizing devices and techniques of radio-controlled models. Severe limitations on size and weight have to be met by all airborne components. On the ground, computerized data processing and test-sequence handling have been necessary. It has been necessary to select appropriate sensors, especially for the airdata sensors working in very low dynamic pressures, and to make careful calibrations both in the laboratory and on the field. Attentions have been paid to keep errors of the measured data within 1% of maximum variation to enable meaningful comparison with other measurements and calculations.
Journal
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- Aeronautical and Space Sciences Japan
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Aeronautical and Space Sciences Japan 44 (504), 56-62, 1996
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390001204479088512
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- NII Article ID
- 130003783032
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- ISSN
- 24241369
- 00214663
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- Text Lang
- ja
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- Data Source
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- JaLC
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed