000			03304cam a22003737i 4500
999			_c4421 _d4421
001			18101213
005			20200211072142.0
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
100	1		_aMarkley, F. Landis, _eauthor.
245	1	0	_aFundamentals of spacecraft attitude determination and control / _cF. Landis Markley, John L. Crassidis.
300			_axv, 486 pages : _billustrations, charts (graphs, tables) ; _c24 cm
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.
650		0	_aEngineering.
650		7	_aEngineering _2fast
650		7	_aSpace vehicles _xAttitude control systems. _2fast
700	1		_aCrassidis, John L., _eauthor.
830		0	_aSpace technology library ; _vv. 33.
856			_3Full-text online _uhttps://link.springer.com/book/10.1007/978-1-4939-0802-8
906			_a7 _bcbc _ccopycat _d2 _encip _f20 _gy-gencatlg
942			_2lcc _cBK