The Development of an UAV Flight Simulator and Its Application -A Study on the Introduction of the Optimal Flight Controls-
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- Kinoshita Takuya
- 信州大学大学院工学系研究科
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- Imado Fumiaki
- 信州大学工学部機械システム工学科
Bibliographic Information
- Other Title
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- UAVフライト・シミュレータの開発とその応用 ―最適飛行制御の導入法に関する研究―
- UAV フライト シミュレータ ノ カイハツ ト ソノ オウヨウ サイテキ ヒコウ セイギョ ノ ドウニュウホウ ニ カンスル ケンキュウ
- The Development of an UAV Flight Simulator and Its Application
- —A Study on the Introduction of the Optimal Flight Controls—
- —最適飛行制御の導入法に関する研究—
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Abstract
This paper proposes a new method which employs the optimal flight controls of a point mass model to a rigid body model in order to realize the optimal guidance controls for an autonomous UAV. In the first stage of this study, we had developed an UAV flight simulator. A point mass model as well as a rigid body model is incorporated into the simulation programs because it is utilized in order to obtain optimal controls by solving two-point boundary-value problems. All proper model parameters of the point mass model were estimated by simulations with the flight simulator. Four control inputs of the rigid body model were produced based on three control inputs of the point mass model. Both models’ simulation results of some flight maneuvers showed good correspondence and our approach was justified by solving a simple optimal control problem of an UAV.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 55 (642), 309-317, 2007
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
- 1390001204470743808
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- NII Article ID
- 10019783866
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 8893858
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed