書誌事項
- タイトル別名
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- A210 Construction of guidance control system for high precision formation flight of small unmanned helicopter
抄録
In this study, we aim at realizing autonomous formation flight of multiple small unmanned helicopters. In such situation, collision avoidance of the helicopters should be considered in guidance control system to improve safety and reliability of the flight system. In our previous study, collision-free guidance control system has been designed by using Model Predictive Control (MPC). Trajectory generation considering collision avoidance has been realized by MPC. However, tracking performance has not been considered, and it is necessary for precise formation flight. In this paper, Differencial Flatness based tracking controller is designed to improve the tracking performance. Then, MPC and Differencial Flatness based guidance control system is proposed for precise formation flight of multiple small unmanned helicopter. Finally, numerical simulation is carried out to verify the effectiveness of proposed guidance control system.
収録刊行物
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- 「運動と振動の制御」シンポジウム講演論文集
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「運動と振動の制御」シンポジウム講演論文集 2015.14 (0), 240-245, 2015
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390001205885654528
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- NII論文ID
- 110010050244
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- ISSN
- 24243000
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可