LEADER 04524nam 22007575 450 001 9910299748103321 005 20200705153921.0 010 $a1-4939-0802-2 024 7 $a10.1007/978-1-4939-0802-8 035 $a(CKB)3710000000119067 035 $a(DE-He213)978-1-4939-0802-8 035 $a(SSID)ssj0001239440 035 $a(PQKBManifestationID)11833558 035 $a(PQKBTitleCode)TC0001239440 035 $a(PQKBWorkID)11186535 035 $a(PQKB)10092217 035 $a(MiAaPQ)EBC6315038 035 $a(MiAaPQ)EBC1730916 035 $a(Au-PeEL)EBL1730916 035 $a(CaPaEBR)ebr10962533 035 $a(OCoLC)881223908 035 $a(PPN)178784427 035 $a(EXLCZ)993710000000119067 100 $a20140531d2014 u| 0 101 0 $aeng 135 $aurnn#008mamaa 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aFundamentals of Spacecraft Attitude Determination and Control$b[electronic resource] /$fby F. Landis Markley, John L. Crassidis 205 $a1st ed. 2014. 210 1$aNew York, NY :$cSpringer New York :$cImprint: Springer,$d2014. 215 $a1 online resource (XVI, 470 p. 96 illus., 4 illus. in color.) 225 1 $aSpace Technology Library ;$v33 300 $aBibliographic Level Mode of Issuance: Monograph 311 $a1-4939-0801-4 320 $aIncludes bibliographical references at the end of each chapter and index. 327 $aAttitude Determination and Estimation -- Matrices, Vectors, Frames, Transforms -- Rotational Kinematics and Dynamics -- Sensors and Actuators -- Static Attitude Determination Methods -- Filtering for Attitude Determination -- Attitude Control. 330 $aThis book explores topics that are central to the field of spacecraft attitude determination and control. The authors provide rigorous theoretical derivations of significant algorithms accompanied by a generous amount of qualitative discussions of the subject matter. The book documents the development of the important concepts and methods in a manner accessible to practicing engineers, graduate-level engineering students and applied mathematicians. It includes detailed examples from actual mission designs to help ease the transition from theory to practice, and also provides prototype algorithms that are readily available on the author?s website. Subject matter includes both theoretical derivations and practical implementation of spacecraft attitude determination and control systems. It provides detailed derivations for attitude kinematics and dynamics, and provides detailed description of the most widely used attitude parameterization, the quaternion. This title also provides a thorough treatise of attitude dynamics including Jacobian elliptical functions. It is the first known book to provide detailed derivations and explanations of state attitude determination, and gives readers real-world examples from actual working spacecraft missions. The subject matter is chosen to fill the void of existing textbooks and treatises, especially in state and dynamics attitude determination. MATLAB code of all examples will be provided through an external website. 410 0$aSpace Technology Library ;$v33 606 $aAerospace engineering 606 $aAstronautics 606 $aDynamics 606 $aErgodic theory 606 $aControl engineering 606 $aAerospace Technology and Astronautics$3https://scigraph.springernature.com/ontologies/product-market-codes/T17050 606 $aDynamical Systems and Ergodic Theory$3https://scigraph.springernature.com/ontologies/product-market-codes/M1204X 606 $aControl and Systems Theory$3https://scigraph.springernature.com/ontologies/product-market-codes/T19010 615 0$aAerospace engineering. 615 0$aAstronautics. 615 0$aDynamics. 615 0$aErgodic theory. 615 0$aControl engineering. 615 14$aAerospace Technology and Astronautics. 615 24$aDynamical Systems and Ergodic Theory. 615 24$aControl and Systems Theory. 676 $a629.4742 700 $aMarkley$b F. Landis$4aut$4http://id.loc.gov/vocabulary/relators/aut$0910917 702 $aCrassidis$b John L$4aut$4http://id.loc.gov/vocabulary/relators/aut 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910299748103321 996 $aFundamentals of Spacecraft Attitude Determination and Control$92039101 997 $aUNINA