Discontinuous maneuver trajectory prediction based on HOA-GRU method for the UAVs

Autor: Zhizhou Zhang, Zhenglei Wei, Bowen Nie, Yang Li

Publikováno v: Electronic Research Archive, Vol 30, Iss 8, Pp 3111-3129 (2022)

With the rapid development of artificial intelligence technology, the intelligence and autonomy of Unmanned Aerial Vehicles (UAVs) have been significantly improved. Because the real trajectory data is often discontinuous and random, the current aircr

Externí odkaz: https://doaj.org/article/2dbaffd60c064bc4b666442d718568c8

Design and Validation of Disturbance Rejection Dynamic Inverse Control for a Tailless Aircraft in Wind Tunnel

Autor: Bowen Nie, Zhitao Liu, Tianhao Guo, Litao Fan, Hongxu Ma, Olivier Sename

Publikováno v: Applied Sciences, Vol 11, Iss 4, p 1407 (2021)

This paper focuses on the design of a disturbance rejection controller for a tailless aircraft based on the technique of nonlinear dynamic inversion (NDI). The tailless aircraft model mounted on a three degree-of-freedom (3-DOF) dynamic rig in the wi

Externí odkaz: https://doaj.org/article/5d7164a839ab42689eaff1b556e401c9

Wind Tunnel Free Flight Model Attitude Determination Based on Non-contact IR Optical Measurement

Autor: Litao Fan, Bowen Nie, Yong Jiang

Publikováno v: Lecture Notes in Electrical Engineering ISBN: 9789811926884

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::4524e89ad34b51e5dd9b8b2597bda5bb
https://doi.org/10.1007/978-981-19-2689-1_19

An Innovative Experimental Approach to Lateral-Directional Flying Quality Investigation for Tailless Aircraft

Autor: Zhitao Liu, Liu Duoneng, Hongxu Ma, Cen Fei, Olivier Sename, Bowen Nie

Publikováno v: IEEE Access, Vol 8, Pp 109543-109556 (2020)
IEEE Access
IEEE Access, IEEE, 2020, 8, pp.109543-109556. ⟨10.1109/ACCESS.2020.3001913⟩

International audience; Tailless aircraft suffers from limited yaw control power and poor directional stability inherently. To address these issues in the early design process of a tailless configuration with low costs and risks, this paper presents

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4338c8000ab9b3f3719aee717a4ebdd7
https://ieeexplore.ieee.org/document/9115649/

Design and Validation of Disturbance Rejection Dynamic Inverse Control for a Tailless Aircraft in Wind Tunnel

Autor: Fan Litao, Tianhao Guo, Olivier Sename, Bowen Nie, Hongxu Ma, Zhitao Liu

Publikováno v: Applied Sciences
Applied Sciences, MDPI, 2021, 11 (4), pp.1407. ⟨10.3390/app11041407⟩
Applied Sciences, Vol 11, Iss 1407, p 1407 (2021)
Volume 11
Issue 4

This paper focuses on the design of a disturbance rejection controller for a tailless aircraft based on the technique of nonlinear dynamic inversion (NDI). The tailless aircraft model mounted on a three degree-of-freedom (3-DOF) dynamic rig in the wi

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f12c1c493c057a670c423327fce029ab
https://hal.univ-grenoble-alpes.fr/hal-03132427