Spacecraft Momentum Control Systems, 1st ed. 2015 Space Technology Library Series, Vol. 34
Auteurs : Leve Frederick A., Hamilton Brian J., Peck Mason A.
Frederick A. Leve Research Aerospace Engineer at the Air Force Research Laboratory, Space Vehicles Directorate, received his Ph.D. in Aerospace Engineering from the University of Florida in 2010. While at the University of Florida, he received the IAF Silver Hermann Oberth Medal and the AIAA Abe Zarem Award for Astronautics. Currently, he is the technical advisor to the Guidance, Navigation, and Controls Group and has published many papers in the area of attitude dynamics and control, specifically with respect to momentum control systems and also performs research in under-actuated control, fault tolerant control, control allocation, analytical mechanics, and system identification. Dr. Leve is a recipient of the 2014 AFRL Early Career Award.
Brian J. Hamilton Engineering Fellow at Honeywell Aerospace, received a BSEE with Honors from the University of Illinois, 1976.Mr. Hamilton has nearly 40 years of experience at Honeywell (formerly, Sperry) and has participated in the development of CMG technology since its infancy. In recent years, his research focus has been on CMG array control and steering, and the general application of momentum systems to agile spacecraft attitude control. Other areas of specialty include nonlinear modeling, controls design, system optimization and active magnetic suspension. Mr. Hamilton holds 12 patents.
Mason A. Peck
Associate Professor at Cornell University in Mechanical and Aerospace Engineering, received his Ph.D. in Aerospace Engineering from the University of California, Los Angeles, in 2001. He has worked as an aerospace engineer since 1994 and has been on the faculty at Cornell since 2004. From late 2011 through early 2014 he was NASA’s Chief Technologist. In that role, he served as the agency’s chief strategist for technology investment and prioritization and advocate for innovation in aeronautics and space technology.His research lab focuses on fundamental resea
Offers a rigorous approach to spacecraft momentum control systems informed by in-depth practical experience in contemporary technology
Practically addresses the topic of singularity avoidance with a contemporary perspective
Includes information for all who are interested in the problem of pointing a spacecraft precisely and quickly, from commercial engineers to researchers and students
Includes supplementary material: sn.pub/extras
Date de parution : 08-2016
Ouvrage de 247 p.
15.5x23.5 cm
Disponible chez l'éditeur (délai d'approvisionnement : 15 jours).
Prix indicatif 94,94 €
Ajouter au panierDate de parution : 10-2015
Ouvrage de 247 p.
15.5x23.5 cm
Disponible chez l'éditeur (délai d'approvisionnement : 15 jours).
Prix indicatif 137,14 €
Ajouter au panierThème de Spacecraft Momentum Control Systems :
Mots-clés :
Algorithms for Spacecraft Steering; Attitude Control; Control Moment Gyroscopes; Gyroscopes in Spacecraft; High-agility Spacecraft Control; Reaction Wheels; Space Systems Engineering; Spacecraft Dynamics; Spacecraft Engineering; System-level Architecture of Spacecraft; Theoretical use of Actuators in Aerospace Engineering