Verification of Fully Autonomous Flight from Takeoff to Landing of a Low-Speed Model Airplane with Application to a Small Unmanned Supersonic Airplane
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- UEBA Masazumi
- Graduate School, Muroran Institute of Technology
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- KAMATA Tomohiro
- Graduate School, Muroran Institute of Technology
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- NAKAJIMA Sakurako
- Graduate School, Muroran Institute of Technology
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- MAEDA Yosuke
- Graduate School, Muroran Institute of Technology
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説明
<p>To realize innovative transportation systems for intercontinental flight and orbital spaceflight, it is essential to establish the necessary aerodynamic, structural, propulsion, and control technologies for a vehicle to fly at high altitudes and speeds within the atmosphere and to verify those technologies by using small unmanned supersonic experimental aircraft. This paper describes the switching conditions at waypoints from one flight mode to another for fully autonomous flight and the verification results of the flight path from takeoff to landing via a circuit by a 3 kg low-speed model airplane. It is confirmed that the switching conditions worked well and thereby the airplane flew on the designated flight path. Based on the results, a flight path is designed for a small unmanned supersonic airplane.</p>
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 19 (5), 667-675, 2021
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390852252714011264
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- NII論文ID
- 130008084477
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- ISSN
- 18840485
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
- OpenAIRE
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- 抄録ライセンスフラグ
- 使用不可