Spacecraft Dynamics and Control: The Embedded Model Control Approach provides a uniform way of approaching space engineering control problems from the standpoint of model-based control, using state equations as the key dynamic model for simulation, design and implementation. The book introduces model-based control design methodology for spacecraft attitude and orbit control. It then covers model-based estimation and control algorithm design, using spacecraft and environment dynamics as the core of the implemented control algorithms-referred to as the embedded (or internal) model. The book also presents two appendices, in which the state equation machinery is fully exploited and introduced.
Embedded model and noise estimators constitute a closed-loop state predictor to be stabilized by the estimator gains. Kalman filter optimization may be adopted under certain restricted assumptions. This book is indispensable for researchers and practitioners in the field of control engineering, aerospace engineering, mechanical engineering and applied mathematics.Die Inhaltsangabe kann sich auf eine andere Ausgabe dieses Titels beziehen.
Enrico Canuto taught Automatic Control for more than 40 years at Politecnico di Torino, Italy. He developed and applied the embedded model control methodology for the design and implementation of digital control systems. Over the course of his career, he has contributed to data reduction of the European astrometric mission Hipparcos, concluding with the publication of the Hipparcos star Catalogue of 120,000 stars; to the European GOCE mission and other forthcoming missions; to instruments for space qualification like the Nanobalance thrust-stand. In the last ten years, he has also collaborated with the Center for Gravity Experiments, Huazhong University of Science and Technology, Wuhan, and the Tianqin Centre, Sun-Yat-Sen University, Zhuhai, China, in the field of scientific space missions aimed at detecting gravitational waves.
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