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| Content Provider | IEEE Xplore Digital Library |
|---|---|
| Author | Chao Zhang Jihong Zhu Kai Liu Xiaming Yuan Yakui Gao |
| Copyright Year | 2013 |
| Description | Author affiliation: Aircraft Inst., AVIC, Xi'an, China (Yakui Gao) || Dept. of Comput. Sci. & Technol., Tsinghua Univ., Beijing, China (Chao Zhang; Jihong Zhu; Kai Liu; Xiaming Yuan) |
| Abstract | Vertical take-off and landing (VTOL) aircraft are more and more important as they combine the benefits of both fixed-wing aircraft and rotary-wing aircraft, and tail-sitting is the simplest way to achieve VTOL maneuvers. However, conventional tail-sitting airplanes are made with propellers or duct fans, which have less thrust and less efficiency. This paper introduces a conceptual thrust-vectored unmanned tail-sitter which is controlled only by thrust vectors (2 engines) while no other control surfaces, thus, they can achieve larger thrust and better maneuverability. However, this configuration is extremely unstable and hard to control. In order to verify its feasibility, a dynamic model is constructed and a linear control strategy has been established to stabilize the platform in hover mode. Simulation results with reference aero data are presented to show the performance, with small disturbances, and its feasibility is validated. |
| Starting Page | 1714 |
| Ending Page | 1717 |
| File Size | 270904 |
| Page Count | 4 |
| File Format | |
| ISBN | 9781467347075 |
| ISSN | 19483449 |
| e-ISBN | 9781467347082 |
| DOI | 10.1109/ICCA.2013.6564878 |
| Language | English |
| Publisher | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Publisher Date | 2013-06-12 |
| Publisher Place | China |
| Access Restriction | Subscribed |
| Rights Holder | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Subject Keyword | Aircraft Vectors Mathematical model Engines Equations Aerospace control Military aircraft |
| Content Type | Text |
| Resource Type | Article |
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