Principles of Spacecraft Control: Concepts and Theory for Practical Applications

This textbook provides mathematical models and algorithms for developing a thorough understanding of control system functions of a rigid body spacecraft. It covers topics such as attitude control, agile rotation maneuvers, precise pointing control, and control systems with accelerometers and free-flying test masses. The aim is to provide an understanding of the principles in an engineering context and to offer concise explanations.

Format: Paperback / softback
Length: 193 pages
Publication date: 02 September 2022
Publisher: Springer International Publishing AG

The aim of this comprehensive textbook is to equip readers with the mathematical models and algorithms essential for developing a thorough understanding of all control system functions in a rigid body spacecraft. While the concepts presented may be relatively straightforward, they are highly practical and applicable in real-world scenarios. Instead of focusing on recent advancements, we have chosen to present straightforward yet effective algorithms that can be readily implemented. Our goal is to avoid delving into detailed and specialized topics that may not be crucial for a fundamental grasp of the subject matter. Furthermore, we will not address control problems that can be formulated using standard methodologies and solved using existing techniques. Instead, our focus will be on imparting an understanding of the principles, placing them within an engineering context, and providing concise explanations wherever possible.

In addition to conventional three-axis attitude control systems, this book delves into various other topics of significance for designing future spacecraft control systems. These include:

• Control of agile rotation maneuvers using control moment gyros: This topic discusses the use of control moment gyros to achieve precise rotational control in spacecraft. By applying torques to the gyros, it is possible to execute rapid and accurate rotation maneuvers, which are essential for tasks such as satellite deployment and orbit adjustments.

• Precise pointing control with error classes for pointing instruments: Pointing instruments, such as telescopes and cameras, play a crucial role in scientific and Earth observation missions. This topic explores the design of control systems that ensure accurate pointing of these instruments, taking into account factors such as instrument errors, environmental disturbances, and mission objectives.

• Control systems with accelerometers and free-flying test masses: In certain applications, such as space exploration and satellite imaging, it is desirable to have control systems that provide low-disturbance or disturbance-free environments. This topic discusses the use of accelerometers and free-flying test masses to measure and compensate for disturbances, enabling more precise and stable control of spacecraft.

We believe that these topics are of paramount importance for the future of spacecraft control systems, particularly in the fields of science and Earth observation missions. By providing readers with a comprehensive understanding of these subjects, we aim to empower them to contribute to the development of innovative and efficient control systems that will enable us to explore and understand our universe in greater detail.

Weight: 449g
Dimension: 240 x 168 (mm)
ISBN-13: 9783031047794
Edition number: 1st ed. 2023