Active Disturbance Rejection Altitude Control for a QuadPlane
Lecture Notes in Electrical Engineering, ISSN: 1876-1119, Vol: 644 LNEE, Page: 329-342
2022
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Example: if you select the 1-year option for an article published in 2019 and a metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019. If you select the 3-year option for the same article published in 2019 and the metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019, 2018 and 2017.
Citation Benchmarking is provided by Scopus and SciVal and is different from the metrics context provided by PlumX Metrics.
Conference Paper Description
Quadplane is a hybrid aircraft which combines both quadrotor and traditional fixed-wing aircraft, and is also called fixed-wing vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV). Quadplane keeps the high speed and endurance of fixed-wing UAVs, and has the ability of VTOL hovering as quadrotors. In this paper, a quadplane platform is constructed. Moreover, to improve the altitude control performance during the transition phase between two flight modes, a model-based nonlinear weight assignment principle and an active disturbance rejection control (ADRC) strategy are proposed. Finally, the effectiveness of aerodynamic modelling and controller is verified via simulations.
Bibliographic Details
http://www.scopus.com/inward/record.url?partnerID=HzOxMe3b&scp=85120612810&origin=inward; http://dx.doi.org/10.1007/978-981-15-8155-7_27; https://link.springer.com/10.1007/978-981-15-8155-7_27; https://link.springer.com/content/pdf/10.1007/978-981-15-8155-7_27; https://dx.doi.org/10.1007/978-981-15-8155-7_27; https://link.springer.com/chapter/10.1007/978-981-15-8155-7_27
Springer Science and Business Media LLC
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