000			03487nam a22005415i 4500
001			978-1-4939-0802-8
003			DE-He213
005			20200421111658.0
007			cr nn 008mamaa
008			140531s2014 xxu| s |||| 0|eng d
020			_a9781493908028 _9978-1-4939-0802-8
024	7		_a10.1007/978-1-4939-0802-8 _2doi
050		4	_aTL787-4050.22
072		7	_aTRP _2bicssc
072		7	_aTTDS _2bicssc
072		7	_aTEC002000 _2bisacsh
082	0	4	_a629.1 _223
100	1		_aMarkley, F. Landis. _eauthor.
245	1	0	_aFundamentals of Spacecraft Attitude Determination and Control _h[electronic resource] / _cby F. Landis Markley, John L. Crassidis.
264		1	_aNew York, NY : _bSpringer New York : _bImprint: Springer, _c2014.
300			_aXV, 486 p. 96 illus., 4 illus. in color. _bonline resource.
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
347			_atext file _bPDF _2rda
490	1		_aSpace Technology Library ; _v33
505	0		_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.
520			_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.
650		0	_aEngineering.
650		0	_aDynamics.
650		0	_aErgodic theory.
650		0	_aAerospace engineering.
650		0	_aAstronautics.
650		0	_aControl engineering.
650	1	4	_aEngineering.
650	2	4	_aAerospace Technology and Astronautics.
650	2	4	_aDynamical Systems and Ergodic Theory.
650	2	4	_aControl.
700	1		_aCrassidis, John L. _eauthor.
710	2		_aSpringerLink (Online service)
773	0		_tSpringer eBooks
776	0	8	_iPrinted edition: _z9781493908011
830		0	_aSpace Technology Library ; _v33
856	4	0	_uhttp://dx.doi.org/10.1007/978-1-4939-0802-8
912			_aZDB-2-ENG
942			_cEBK
999			_c54811 _d54811