000			03126nam a22004935i 4500
001			978-3-642-36841-7
003			DE-He213
005			20200421111839.0
007			cr nn 008mamaa
008			130607s2013 gw | s |||| 0|eng d
020			_a9783642368417 _9978-3-642-36841-7
024	7		_a10.1007/978-3-642-36841-7 _2doi
050		4	_aTJ212-225
072		7	_aTJFM _2bicssc
072		7	_aTEC004000 _2bisacsh
082	0	4	_a629.8 _223
100	1		_aXia, Yuanqing. _eauthor.
245	1	0	_aCompound Control Methodology for Flight Vehicles _h[electronic resource] / _cby Yuanqing Xia, Mengyin Fu.
264		1	_aBerlin, Heidelberg : _bSpringer Berlin Heidelberg : _bImprint: Springer, _c2013.
300			_aXVIII, 260 p. 125 illus. _bonline resource.
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
347			_atext file _bPDF _2rda
490	1		_aLecture Notes in Control and Information Sciences, _x0170-8643 ; _v438
505	0		_aOverview of Sliding Mode Control -- Overview of Active Disturbance Rejection Control -- Overview of Flight Vehicle Control -- The Descriptions of Flight Vehicle -- SMC for Missile Systems Based on Back-Stepping and ESO Techniques -- Adaptive SMC for Attitude Stabilization in Presence of Actuator Saturation -- Adaptive Nonsingular Terminal Sliding Mode Control for Rigid Spacecraft -- Attitude Tracking of Rigid Spacecraft with Uncertainties and Disturbances -- SMC for Attitude Tracking of Rigid Spacecraft with Disturbances -- Missile Guidance Law Based on ESO Techniques -- Missile Guidance Laws Based on SMC and FTC Techniques -- Cooperative Attack of Multiple Missiles Based on Optimal Guidance Law.
520			_a"Compound Control Methodology for Flight Vehicles" focuses on new control methods for flight vehicles. In this monograph the concept of compound control is introduced. It is demonstrated that both Sliding Mode Control (SMC) and Active Disturbance Rejection Control (ADRC) have their own advantages and limitations, i.e., chattering of SMC and the observability of extended state observer (ESO), respectively. It is shown that compound control combines their advantages and improves the performance of the closed-loop systems. The book is self-contained, providing sufficient mathematical foundations for understanding the contents of each chapter. It will be of significant interest to scientists and engineers engaged in the field of flight vehicle control.
650		0	_aEngineering.
650		0	_aAerospace engineering.
650		0	_aAstronautics.
650		0	_aControl engineering.
650	1	4	_aEngineering.
650	2	4	_aControl.
650	2	4	_aAerospace Technology and Astronautics.
700	1		_aFu, Mengyin. _eauthor.
710	2		_aSpringerLink (Online service)
773	0		_tSpringer eBooks
776	0	8	_iPrinted edition: _z9783642368400
830		0	_aLecture Notes in Control and Information Sciences, _x0170-8643 ; _v438
856	4	0	_uhttp://dx.doi.org/10.1007/978-3-642-36841-7
912			_aZDB-2-ENG
942			_cEBK
999			_c55475 _d55475