000			03349nam a22003735i 4500
001			290789
003			MX-SnUAN
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007			cr nn 008mamaa
008			150903s2009 xxk| o |||| 0|eng d
020			_a9781848825611 _99781848825611
024	7		_a10.1007/9781848825611 _2doi
035			_avtls000344476
039		9	_a201509030408 _bVLOAD _c201405050307 _dVLOAD _y201402061258 _zstaff
040			_aMX-SnUAN _bspa _cMX-SnUAN _erda
050		4	_aTL1-483
100	1		_aDucard, Guillaume J.J. _eautor _9321720
245	1	0	_aFault-tolerant Flight Control and Guidance Systems : _bPractical Methods for Small Unmanned Aerial Vehicles / _cby Guillaume J.J. Ducard.
264		1	_aLondon : _bSpringer London, _c2009.
300			_brecurso en línea.
336			_atexto _btxt _2rdacontent
337			_acomputadora _bc _2rdamedia
338			_arecurso en línea _bcr _2rdacarrier
347			_aarchivo de texto _bPDF _2rda
490	0		_aAdvances in Industrial Control, _x1430-9491
500			_aSpringer eBooks
505	0		_aReview -- Nonlinear Aircraft Model -- Nonlinear Fault Detection and Isolation System -- Control Allocation -- Nonlinear Control Design -- Autopilot for the Longitudinal Motion -- Autopilot for the Lateral Motion -- Reconfigurable Guidance System -- Evaluation of the Reduction in the Performance of a UAV -- Conclusions and Outlook.
520			_aUnmanned aerial vehicles (UAVs) offer an incomparable means of gathering intelligence and carrying out missions without needing an onboard human pilot. The benefits are considerable in terms of cost, efficiency, and reduced pilot risk. In order to complete a mission efficiently and with a high level of safety and security, the following key design points must be met: • the flight control system must be robust against the aircraft’s model uncertainties and external disturbances; • an efficient fault detection and isolation (FDI) system should be capable of monitoring the health of the aircraft; and • the flight control and guidance system should be reconfigurable depending on actuator fault occurrence or aircraft damage, and should be able to avoid obstacles. Fault-tolerant Flight Control and Guidance Systems addresses all of these aspects with a practical approach following three main requirements: being applicable in real-time; highly computationally efficient; and modular. The text provides: • an overview of fault-tolerant flight control techniques; • the necessary equations for the modeling of small UAVs; • a complete nonlinear FDI system based on extended Kalman filters; and • a nonlinear flight control and guidance system. The book is written in a didactic style with many figures and diagrams making it suitable not only for academic researchers and practicing engineers but also graduate students working in the fields of fault detection techniques and the automatic control of UAVs.
590			_aPara consulta fuera de la UANL se requiere clave de acceso remoto.
710	2		_aSpringerLink (Servicio en línea) _9299170
776	0	8	_iEdición impresa: _z9781848825604
856	4	0	_uhttp://remoto.dgb.uanl.mx/login?url=http://dx.doi.org/10.1007/978-1-84882-561-1 _zConectar a Springer E-Books (Para consulta externa se requiere previa autentificación en Biblioteca Digital UANL)
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999			_c290789 _d290789