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浏览/检索结果: 共3条，第1-3条 帮助 已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Fault-tolerant control for a Multi-propeller Aerostat based on sliding mode control allocation method 会议论文 Xiamen, China, July 5-7, 2019 作者:  Liang, K.K.;  Chen L(陈丽);  Liu JG(刘金国) 收藏  |  浏览/下载：17/0  |  提交时间：2020/11/14 Multi-propeller Aerostat  fault-tolerant control  trajectory tacking control  sliding mode control  control allocation   Integrated Cooperative Control Scheme for Multiple Quadrotors Based on Improved Adaptive Disturbance Rejection Control 会议论文 Qingdao, China, Dec. 3 -Dec. 7, 2016 作者:  Han Du;  Zhiqiang Pu;  Jianqiang Yi 收藏  |  浏览/下载：20/0  |  提交时间：2016/11/08 Multiple Quadrotors   Trajectory tacking control of a quad-rotor based on active disturbance rejection control (EI CONFERENCE) 会议论文 2012 IEEE International Conference on Automation and Logistics, ICAL 2012, August 15, 2012 - August 17, 2012, Zhengzhou, China Gong X.; Tian Y.; Bai Y.; Zhao C. 收藏  |  浏览/下载：21/0  |  提交时间：2013/03/25 The objective of this paper is to deal with a trajectory tracking of a Quad-rotor unmanned aerial vehicle (UAV). For the model uncertainty  the external disturbance and the coupling factor are considered  an active disturbance rejection control (ADRC) algorithm is introduced into the designing procedure. The aircraft dynamic model is proposed in this article  based on which the closed-loop control system is divided into four independent channels with the coupling factor compensated by the extended state observer (ESO). The nonlinear state error feedback (NLSEF) algorithm is designed in each channel to improve the closed-loop dynamics. In this article  the ADRC controller is expressed in the discrete form. And finally  the simulation results show that the proposed control algorithm achieves a favourable tracking performance. 2012 IEEE.