Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle, Li

Автор: Chai Runqi, Savvaris Al, Tsourdos Antonios
Название: Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems
ISBN: 981139847X ISBN-13(EAN): 9789811398476
Издательство: Springer
Рейтинг:
Цена: 149060.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: The comprehensive and systematic treatment of practical issues in spacecraft trajectory optimization is one of the book`s major features, making it particularly suited for readers who are seeking practical solutions in spacecraft trajectory optimization.

Автор: Runqi Chai, Al Savvaris, Antonios Tsourdos, Senchu
Название: Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems
ISBN: 9811398445 ISBN-13(EAN): 9789811398445
Издательство: Springer
Рейтинг:
Цена: 149060.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: The comprehensive and systematic treatment of practical issues in spacecraft trajectory optimization is one of the book`s major features, making it particularly suited for readers who are seeking practical solutions in spacecraft trajectory optimization.

Автор: Song
Название: Autonomous Trajectory Planning and Guidance Control for Launch Vehicles
ISBN: 9819906156 ISBN-13(EAN): 9789819906154
Издательство: Springer
Рейтинг:
Цена: 37260.00 T
Наличие на складе: Нет в наличии.
Описание: 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 exhibit a 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 progress of relevant projects and academic studies of autonomous guidance, especially on some advanced methods which can be potentially real-time implemented in the future control system of launch vehicles. In Chapter 1, the prospect and technical challenges are summarized by reviewing the development of launch vehicles. Chapters 2 to 4 mainly focus on the flight in the ascent phase, in which the autonomous guidance is mainly reflected in the online planning. Chapters 5 and 6 mainly discuss the powered descent guidance technologies. Finally, since aerodynamic uncertainties exert a significant impact on the performance of the ascent / landing guidance control systems, the estimation of aerodynamic parameters, which are helpful to improve flight autonomy, is discussed in Chapter 7. The book serves as a valuable reference for researchers and engineers working on launch vehicles. It is also a timely source of information for graduate students interested in the subject.

Автор: Song
Название: Autonomous Trajectory Planning and Guidance Control for Launch Vehicles
ISBN: 9819906121 ISBN-13(EAN): 9789819906123
Издательство: Springer
Рейтинг:
Цена: 37260.00 T
Наличие на складе: Нет в наличии.
Описание: 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 exhibit a 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 progress of relevant projects and academic studies of autonomous guidance, especially on some advanced methods which can be potentially real-time implemented in the future control system of launch vehicles. In Chapter 1, the prospect and technical challenges are summarized by reviewing the development of launch vehicles. Chapters 2 to 4 mainly focus on the flight in the ascent phase, in which the autonomous guidance is mainly reflected in the online planning. Chapters 5 and 6 mainly discuss the powered descent guidance technologies. Finally, since aerodynamic uncertainties exert a significant impact on the performance of the ascent / landing guidance control systems, the estimation of aerodynamic parameters, which are helpful to improve flight autonomy, is discussed in Chapter 7. The book serves as a valuable reference for researchers and engineers working on launch vehicles. It is also a timely source of information for graduate students interested in the subject.