000 03520cam a22004337i 4500
001 18101213
005 20230324110355.0
008 140403t20142014gw ad b 001 0 eng d
010 _a 2014937452
020 _a1493908014
_q(cloth)
020 _a9781493908011
_q(cloth)
020 _z9781493908028
035 _a(OCoLC)ocn882605422
040 _aCDX
_beng
_erda
_cCDX
_dOCLCQ
_dYDXCP
_dOCLCO
_dWAU
_dBTCTA
_dOCLCQ
_dOCLCF
_dJID
_dCOH
_dOCL
_dDLC
042 _alccopycat
050 0 0 _aTL3260
_b.M37 2014
082 _a629.4742
_bMAR
100 1 _aMarkley, F. Landis,
_eauthor.
_9111353
245 1 0 _aFundamentals of spacecraft attitude determination and control /
_cF. Landis Markley, John L. Crassidis.
264 1 _aNew York :
_bSpringer,
_c[2014]
264 4 _c©2014
300 _axv, 486 pages :
_billustrations, charts (graphs, tables) ;
_c24 cm
336 _atext
_btxt
_2rdacontent
337 _aunmediated
_bn
_2rdamedia
338 _avolume
_bnc
_2rdacarrier
490 1 _aSpace technology library ;
_v33
504 _aIncludes bibliographical references (at the end of each chapter) and index.
505 0 _aIntroduction -- Matrices, vectors, frames, transforms -- Attitude kinematics and dynamics -- Sensors and actuators -- Static attitude determination methods -- Filtering for attitude estimation and calibration -- Attitude control -- Quaternion identities -- Euler angles -- Orbital dynamics -- Environment models -- Review of control and estimation theory -- Computer software.
520 _a"This 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 alsoprovides 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." --Publisher's Website.
650 0 _aSpace vehicles
_xAttitude control systems.
_9110660
650 0 _aEngineering.
650 7 _aEngineering
_2fast
_0(OCoLC)fst00910312
_9111354
650 7 _aSpace vehicles
_xAttitude control systems.
_2fast
_0(OCoLC)fst01127962
_9110660
700 1 _aCrassidis, John L.,
_eauthor.
_977889
830 0 _aSpace technology library ;
_vv. 33.
_9111355
906 _a7
_bcbc
_ccopycat
_d2
_encip
_f20
_gy-gencatlg
942 _2ddc
_cBK
955 _brm08 2017-02-18 z-processor
_irk06 2017-03-10 to Dewey
999 _c594242
_d594242