دانلود کتاب اصول کنترل فضاپیما

The design of spacecraft control systems is, first of all, a system engineering task. This concerns not only the control system itself (sensors, actuators, computers, and software) but also the mission objectives and interfaces to other subsystems. With increasingly demanding mission and system requirements, the interconnection between spacecraft control system, instrument payload, and platform becomes even more distinct. Therefore, a thorough understanding of the functional principles of a spacecraft control system as well as its limitations is required for efficient system engineering. This book is written as a textbook. The objective is to provide the mathematical models and algorithms needed to develop a thorough understanding of all control system functions of a rigid-body spacecraft. Relatively simple but practically applicable algorithms are presented rather than recent advances.We try to avoid detailed and specialized issues that are of less importance for the fundamental understanding, such as detailed environment models. Furthermore, control problems that can be cast in standard formulations and solved with existing methods are not treated here. Instead, we intend to provide an understanding of the principles, put them in an engineering context, and try to give all explanations as concise as possible.