000			03237cam a2200469M 4500
001			9781351248839
003			FlBoTFG
005			20220509193016.0
006			m o d
007			cr |n|||||||||
008			201126s2021 xx o 000 0 eng d
040			_aOCoLC-P _beng _cOCoLC-P
020			_a9781351248815 _q(electronic bk.)
020			_a1351248812 _q(electronic bk.)
020			_a9781351248839 _q(electronic bk.)
020			_a1351248839 _q(electronic bk.)
020			_a9781351248822 _q(electronic bk. : PDF)
020			_a1351248820 _q(electronic bk. : PDF)
020			_a9781351248808 _q(electronic bk. : Mobipocket)
020			_a1351248804 _q(electronic bk. : Mobipocket)
020			_z0815369816
020			_z9780815369813
035			_a(OCoLC)1224246880
035			_a(OCoLC-P)1224246880
050		4	_aTL795.4
072		7	_aTEC _x007000 _2bisacsh
072		7	_aTEC _x009070 _2bisacsh
072		7	_aTEC _x064000 _2bisacsh
072		7	_aTQ _2bicssc
082	0	4	_a629.46 _223
100	1		_aHajiyev, Chingiz.
245	1	0	_aFAULT TOLERANT ATTITUDE ESTIMATION FOR SMALL SATELLITES _h[electronic resource].
260			_a[S.l.] : _bCRC PRESS, _c2021.
300			_a1 online resource
520			_aSmall satellites use commercial off-the-shelf sensors and actuators for attitude determination and control (ADC) to reduce the cost. These sensors and actuators are usually not as robust as the available, more expensive, space-proven equipment. As a result, the ADC system of small satellites is more vulnerable to any fault compared to a system for larger competitors. This book aims to present useful solutions for fault tolerance in ADC systems of small satellites. The contents of the book can be divided into two categories: fault tolerant attitude filtering algorithms for small satellites and sensor calibration methods to compensate the sensor errors. MATLAB will be used to demonstrate simulations. Presents fault tolerant attitude estimation algorithms for small satellites with an emphasis on algorithms' practicability and applicability Incorporates fundamental knowledge about the attitude determination methods at large Discusses comprehensive information about attitude sensors for small satellites Reviews calibration algorithms for small satellite magnetometers with simulated examples Supports theory with MATLAB simulation results which can be easily understood by individuals without a comprehensive background in this field Covers up-to-date discussions for small satellite attitude systems design Dr. Chingiz Hajiyev is a professor at the Faculty of Aeronautics and Astronautics, Istanbul Technical University (Istanbul, Turkey). Dr. Halil Ersin Soken is an assistant professor at the Aerospace Engineering Department, Middle East Technical University (Ankara, Turkey).
588			_aOCLC-licensed vendor bibliographic record.
650		0	_aMicrospacecraft.
650		0	_aFault-tolerant computing.
650		7	_aTECHNOLOGY / Electricity _2bisacsh
650		7	_aTECHNOLOGY / Engineering / Mechanical _2bisacsh
856	4	0	_3Taylor & Francis _uhttps://www.taylorfrancis.com/books/9781351248839
856	4	2	_3OCLC metadata license agreement _uhttp://www.oclc.org/content/dam/oclc/forms/terms/vbrl-201703.pdf
999			_c128142 _d128142