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Titlebook: Autonomous Trajectory Planning and Guidance Control for Launch Vehicles; Zhengyu Song,Dangjun Zhao,Stephan Theil Book‘‘‘‘‘‘‘‘ 2023 The Edi

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發(fā)表于 2025-3-21 18:12:51 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
期刊全稱Autonomous Trajectory Planning and Guidance Control for Launch Vehicles
影響因子2023Zhengyu Song,Dangjun Zhao,Stephan Theil
視頻videohttp://file.papertrans.cn/167/166798/166798.mp4
發(fā)行地址Presents a series of advanced studies on autonomous trajectory planning and guidance control for launchers.Discusses technical challenges from a Chief Designer‘s perspective.Summarizes advances in fau
學(xué)科分類Springer Series in Astrophysics and Cosmology
圖書封面Titlebook: Autonomous Trajectory Planning and Guidance Control for Launch Vehicles;  Zhengyu Song,Dangjun Zhao,Stephan Theil Book‘‘‘‘‘‘‘‘ 2023 The Edi
影響因子.This open access book highlights the autonomous and intelligent flight control of future launch vehicles for improving flight autonomy to plan ascent and descent trajectories onboard, and autonomously handle unexpected events or failures during the flight...?..Since the beginning of the twenty-first century, space launch activities worldwide have grown vigorously. Meanwhile, commercial launches also account for the booming trend. Unfortunately, the risk of space launches still exists and is gradually increasing in line with the rapidly rising launch activities and commercial rockets. In the history of space launches, propulsion and control systems are the two main contributors to launch failures. With the development of information technologies, the increase of the functional density of hardware products, the application of redundant or fault-tolerant solutions, and the improvement of the testability of avionics, the launch losses caused by control systems exhibita downward trend, and the failures induced by propulsion systems become the focus of attention. Under these failures, the autonomous planning and guidance control may save the missions...?.This book focuses on the latest
Pindex Book‘‘‘‘‘‘‘‘ 2023
The information of publication is updating

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Spezielles Kapitel: Datenschutz, promotion, providing increasingly valuable high-tech services for society. Currently, the development of launch vehicle is progressing with respect to stronger capabilities, higher reliability, lowering costs, flexibility, and user convenience. Retrospectively, the global development history of the
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Hansjoachim Walther,Günter N?glere called orbital elements (OEs), which include the semi-major axis ., the eccentricity ., the argument of perigee ., the inclination angle ., and the longitude of ascending node (LAN) or the right ascension of ascending node (RAAN) ., where . and . can be converted to the perigee height . and the ap
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https://doi.org/10.1007/978-3-031-57575-4The powered descent phase is the terminal phase of the planetary descent and landing mission, where the required direction and magnitude of the thrust engine are determined to steer the spacecraft to meet the pre-determined targeting condition at the end, such as touchdown at the designated landing site with the required velocity [.].
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