书目名称 | Fault-tolerant Flight Control and Guidance Systems |
副标题 | Practical Methods fo |
编辑 | Guillaume J.J. Ducard |
视频video | http://file.papertrans.cn/342/341515/341515.mp4 |
概述 | Gives the reader a complete overview of fault-tolerant flight control techniques including modeling equations and extended Kalman filter implementation.Presents a complete nonlinear flight control sys |
丛书名称 | Advances in Industrial Control |
图书封面 |  |
描述 | .Unmanned aerial vehicles (UAVs) offer an incomparable means of gathering intelligence and carrying out missions without needing an onboard human pilot. The benefits are considerable in terms of cost, efficiency, and reduced pilot risk...In order to complete a mission efficiently and with a high level of safety and security, the following key design points must be met:..• the flight control system must be robust against the aircraft’s model uncertainties and external disturbances;..• an efficient fault detection and isolation (FDI) system should be capable of monitoring the health of the aircraft; and..• the flight control and guidance system should be reconfigurable depending on actuator fault occurrence or aircraft damage, and should be able to avoid obstacles...Fault-tolerant Flight Control and Guidance Systems. addresses all of these aspects with a practical approach following three main requirements: being applicable in real-time; highly computationally efficient; and modular. The text provides:..• an overview of fault-tolerant flight control techniques;..• the necessary equations for the modeling of small UAVs;..• a complete nonlinear FDI system based on extended Kalman filte |
出版日期 | Book 2009 |
关键词 | Autopilot; Kalman filter; Monitoring; UAV; actuator; aerospace engineering; automatic control; control; cont |
版次 | 1 |
doi | https://doi.org/10.1007/978-1-84882-561-1 |
isbn_softcover | 978-1-84996-850-8 |
isbn_ebook | 978-1-84882-561-1Series ISSN 1430-9491 Series E-ISSN 2193-1577 |
issn_series | 1430-9491 |
copyright | Springer-Verlag London 2009 |