Spacecraft Dynamics and Control: The Embedded Model Control Approach provides a uniform and systematic way of approaching space engineering control problems from the standpoint of model-based control, using state-space equations as the key paradigm for simulation, design and implementation.
The book introduces the Embedded Model Control methodology for the design and implementation of attitude and orbit control systems. The logic architecture is organized around the embedded model of the spacecraft and its surrounding environment. The model is compelled to include disturbance dynamics as a repository of the uncertainty that the control law must reject to meet attitude and orbit requirements within the uncertainty class. The source of the real-time uncertainty estimation/prediction is the model error signal, as it encodes the residual discrepancies between spacecraft measurements and model output. The embedded model and the uncertainty estimation feedback (noise estimator in the book) constitute the state predictor feeding the control law. Asymptotic pole placement (exploiting the asymptotes of closed-loop transfer functions) is the way to design and tune feedback loops around the embedded model (state predictor, control law, reference generator). The design versus the uncertainty class is driven by analytic stability and performance inequalities. The method is applied to several attitude and orbit control problems.
- The book begins with an extensive introduction to attitude geometry and algebra and ends with the core themes: state-space dynamics and Embedded Model Control
- Fundamentals of orbit, attitude and environment dynamics are treated giving emphasis to state-space formulation, disturbance dynamics, state feedback and prediction, closed-loop stability
- Sensors and actuators are treated giving emphasis to their dynamics and modelling of measurement errors. Numerical tables are included and their data employed for numerical simulations
- Orbit and attitude control problems of the European GOCE mission are the inspiration of numerical exercises and simulations
- The suite of the attitude control modes of a GOCE-like mission is designed and simulated around the so-called mission state predictor
- Solved and unsolved exercises are included within the text - and not separated at the end of chapters - for better understanding, training and application
- Simulated results and their graphical plots are developed through MATLAB/Simulink code
Industry Reviews
"Spacecraft Dynamics and Control approaches the problem of controlling a spacecraft from a model-based control perspective. Both orbit and attitude control are dealt with, although more focus is given on the latter. In my opinion, there are two main strengths of this book. Being the result of authors' collaboration with ESA, the book presents the material with a focus on practical applications. The case studies and proposed and solved exercises are carefully designed and they are a critical support for reading comprehension and self-assessment. This book distinguishes itself by the focus on strong model-based control. As such I consider it useful for researchers and practitioners with classical control theory expertise to familiarise with astrodynamics problems and for those with a more physics-based background to get their hands on spacecraft control control problems. Undergraduate and graduate students will find this book useful to understand fundamentals concepts and to carry out individual or group projects. The notation used and terminology is sometimes non-standard, however this does not impair upon the reading much as consistency is preserved along the manuscript.
"In my opinion, there are two main strengths of this book. Being the result of authors' collaboration with ESA, the book presents the material with a focus on practical applications. The case studies and proposed and solved exercises are carefully designed and they are a critical support for reading comprehension and self-assessment. This book distinguishes itself by the focus on strong model-based control. As such I consider it useful for researchers and practitioners with classical control theory expertise to familiarise with astrodynamics problems and for those with a more physics-based background to get their hands on spacecraft control control problems. Undergraduate and graduate students will find this book useful to understand fundamentals concepts and to carry out individual or group projects. The notation used and terminology is sometimes non-standard, however this does not impair upon the reading much as consistency is preserved along the manuscript." --The Aeronautical Journal
