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Spacecraft Dynamics and Control

Inglese · Tascabile

Spedizione di solito entro 3 a 5 settimane

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Informationen zum Autor 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. Carlo Novara received his MSc degree in Physics from the University of Turin in 1996 and his PhD degree in Computer and System Engineering from Politecnico di Torino in 2002. He held a visiting researcher position at University of California at Berkeley in 2001 and 2004 and is currently a Full Professor at Politecnico di Torino. He is a really prolific author of peer-reviewed scientific publications in international journals and conference proceedings. He has been involved in several national and international projects and in several research contracts in collaboration with Italian and European companies. He is the co-author of several patents in the automotive field. He is a member of the IEEE Technical Committee on System Identification and Adaptive Control, of the IFAC Technical Committee on Modelling, Identification and Signal Processing, of the IFAC Technical Committee on Modelling and Control of Environmental Systems, and a founding member of the IEEE-CSS Technical Committee on Medical and Healthcare Systems. His research interests include nonlinear and linear parameter-varying system identification, filtering/estimation, time series prediction, nonlinear control, predictive control, data-driven methods, set membership methods, sparse methods, nonlinear optimization, and aerospace, automotive, biomedical, and energy applications. Donato Carlucci is an Associate Professor at Politecnico di Torino. He is the author or co-author of scientific publications on applied nonlinear systems control. He has been involved in national and international projects in collaboration with Italian and European industries. He has worked for more than 40 years in the fields of nonlinear system control including aerospace systems. His current research interests include satellite attitude control. He is teaching courses on Automation and Production Systems at Politecnico di Torino Carlos Perez-Montenegro received his MSc degree in Electronic Engineering from Pontificia Universidad Javeriana in 2007, followed in 2014 by a PhD in Computer and Control Engineering from the Department of Control and Computer Engineering of Politecnico di Torino. His research interests span the fields of guidance, navigation, and control (GNC), with a focus on applications to planetary landing systems and unmanned aerial systems. Currently, he is designing and implementing control and estimation systems for service instruments of the automotive industry. Luca Massotti received his MSc and PhD degrees in Aerospace Engineering from Politecnico di Torino in 2000 and 2004 respectively. In 2001-2002, he was a visiting researcher at West Virginia University to study aircraft modelling and neural network controllers. In 2004, he joined Thales Alenia Space in Turin as an engineering consultant for metrology and AOCS. From 2005 to 2007, he was a post-doctoral researcher within the Earth Observation Programs of the European Space Agency at the ESTEC facility in the Netherlands, where he currently works as a system engineer for the Future Missions and Instruments division. He is actively involved in th...

Dettagli sul prodotto

Autori Enrico Canuto, Novara Carlo, Carlos Perez Montenegro, Luca Massotti, Carlos Perez-Montenegro, Donato Carlucci
Editore Butterworth Scientific Elsevier
 
Contenuto Libro
Forma del prodotto Tascabile
Data pubblicazione 10.03.2018
Categoria Libri scolastici > Didattica > Formazione professionale
Scienze naturali, medicina, informatica, tecnica > Tecnica > Meccanica, tecnica di produzione
 
EAN 9780081007006
ISBN 978-0-08-100700-6
 
Serie Aerospace Engineering
Categorie Audience, Authorship, TECHNOLOGY & ENGINEERING / Mechanical, hybridization, Quest, TECHNOLOGY & ENGINEERING / Engineering (General), SCIENCE / Mechanics / General, random processes, astronautics, Stability, Linear Algebra, Mechanical Engineering, Topics, Automatic control engineering, Aerodynamics, Dynamic systems, Controllability, Propulsion Systems, Electromagnetic Radiation, Lyapunov stability, Kalman Filter, Parametric Uncertainty, Reaction Wheels, Observability, Orbital dynamics, Hierarchical control, Euler Angles, two-body problem, Stochastic model, abbreviations, Kepler's equation, gyroscope, Accelerometer, Rotation matrix, Quaternion, Notations, Space environment, orbital stability, Halo orbit, closed-loop stability, control modes, triad, magnetometers, attitude determination, spacecraft attitude control, Control moment gyros, Thrusters, restricted three-body problem, Orbit transfer and hyperbolic flyby, spacecraft sensors, Active nutation damping, ESOQ, State predictor, Attitude dynamics and control with reaction wheels, Torque-free rigid body attitude, periodic systems, attitude dynamics, Separation theorem, Causal uncertainty, Angular rate determination, Reference orbit quaternion, Sensor modeling, Attitude requirements, Exchange momentum actuators, Sun and Earth sensors, Gravity gradient torques, Euler angle kinematics, Perturbing forces and torques, Error quaternion kinematics, Book objectives, Internal forces/torques, Neglected dynamics, gravity gradient stabilization, GOCE mission, Drag-free control, Star tracker, Magnetic torquers, Force actuators, Attitude representations, Torque actuators, Quaternion kinematics, Control law, Lagrangian equilibrium points, Static determination, Attitude accuracy, Space and time coordinates, Aerodynamic stability, Embedded model control, Attitude matrix kinematics, Attitude state predictor, Perturbed orbits, Attitude sensors, Hill�Clohessy�Wiltshire equations and control, Magnetic torques, Gauss planetary equations, Quaternion predictor, Lissajous orbit, Euler's equation of rotation, Error equation linearization, Spacecraft detumbling, Problem of Wahba, Lagrange planetary equations, Orbit propagation, Gravity forces, state feedback, Conversions between representations
 

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