LEADER 04189nam  22006975  450 
001 9910254194903321
005 20250609111427.0
010   $a3-319-25540-1
024 7 $a10.1007/978-3-319-25540-8
035   $a(CKB)3710000000498795
035   $a(EBL)4068165
035   $a(SSID)ssj0001584621
035   $a(PQKBManifestationID)16263932
035   $a(PQKBTitleCode)TC0001584621
035   $a(PQKBWorkID)14864616
035   $a(PQKB)10340208
035   $a(DE-He213)978-3-319-25540-8
035   $a(MiAaPQ)EBC4068165
035   $a(PPN)190536543
035   $a(MiAaPQ)EBC6234128
035   $a(EXLCZ)993710000000498795
100   $a20151027d2016      u|         0
101 0 $aeng
135   $aur|n|---|||||
181   $ctxt
182   $cc
183   $acr
200 10$aFlexible Spacecraft Dynamics, Control and Guidance $eTechnologies by Giovanni Campolo /$fby Leonardo Mazzini
205   $a1st ed. 2016.
210  1$aCham :$cSpringer International Publishing :$cImprint: Springer,$d2016.
215   $a1 online resource (372 p.)
225 1 $aSpringer Aerospace Technology,$x1869-1730
300   $aDescription based upon print version of record.
311 08$a3-319-25538-X 
320   $aIncludes bibliographical references at the end of each chapters and index.
327   $aIntroduction -- The Kinematic of the flexible satellite -- The Satellite Attitude Control System -- The Dynamic of the flexible body -- The Dynamic in the Gravitational Field -- The Optimal Control Theory -- Attitude Control Methods -- Orbital Dynamic and Control -- Spacecraft Propulsion -- Sensors and Actuators technologies -- Complements to Body Kinematic -- Elements of Estimation Theory -- Basics of Lagrangian Equations -- The J2 perturbation solution -- Complements to Optimal Orbital Transfer -- Elements of Plasma physics.
330   $aThis book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers. After an introduction on the kinematics of the flexible and agile space vehicles, the modern architecture and functions of an AOC system are described and the main AOC modes reviewed with possible design solutions and examples. The dynamics of the flexible body in space are then considered using an original Lagrangian approach suitable for the control applications of large space flexible structures. Subsequent chapters address optimal control theory, attitude control methods, and orbit control applications, including the optimal orbital transfer with finite and infinite thrust. The theory is integrated with a description of current propulsion systems, with the focus especially on the new electric propulsion systems and state of the art sensors and actuators.
410  0$aSpringer Aerospace Technology,$x1869-1730
606   $aAerospace engineering
606   $aAstronautics
606   $aAutomatic control
606   $aSpace sciences
606   $aAerospace Technology and Astronautics$3https://scigraph.springernature.com/ontologies/product-market-codes/T17050
606   $aControl and Systems Theory$3https://scigraph.springernature.com/ontologies/product-market-codes/T19010
606   $aSpace Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics)$3https://scigraph.springernature.com/ontologies/product-market-codes/P22030
615  0$aAerospace engineering.
615  0$aAstronautics.
615  0$aAutomatic control.
615  0$aSpace sciences.
615 14$aAerospace Technology and Astronautics.
615 24$aControl and Systems Theory.
615 24$aSpace Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics).
676   $a629.41
700   $aMazzini$b Leonardo$4aut$4http://id.loc.gov/vocabulary/relators/aut$0762226
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910254194903321
996   $aFlexible Spacecraft Dynamics, Control and Guidance$91545018
997   $aUNINA