000 | 03606nam a22004695i 4500 | ||
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001 | 978-1-84628-471-7 | ||
003 | DE-He213 | ||
005 | 20170628033856.0 | ||
007 | cr nn 008mamaa | ||
008 | 100301s2006 xxk| s |||| 0|eng d | ||
020 |
_a9781846284717 _9978-1-84628-471-7 |
||
024 | 7 |
_a10.1007/978-1-84628-471-7 _2doi |
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100 | 1 |
_aAlamir, Mazen. _eauthor. |
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245 | 1 | 0 |
_aStabilization of Nonlinear Systems Using Receding-horizon Control Schemes _h[electronic resource] : _bA Parametrized Approach for Fast Systems / _cby Mazen Alamir. |
264 | 1 |
_aLondon : _bSpringer London, _c2006. |
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300 |
_aXVII, 308 p. 102 illus. _bonline resource. |
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336 |
_atext _btxt _2rdacontent |
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337 |
_acomputer _bc _2rdamedia |
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338 |
_aonline resource _bcr _2rdacarrier |
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347 |
_atext file _bPDF _2rda |
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490 | 1 |
_aLecture Notes in Control and Information Sciences, _x0170-8643 ; _v339 |
|
505 | 0 | _aGeneric Framework -- Definitions and Notation -- The Receding-Horizon State Feedback -- Stabilizing Schemes with Final Equality Constraint on the State -- Stabilizing Formulations with Free Prediction Horizon and No Final Constraint on the State -- General Stabilizing Formulations for Trivial Parametrization -- Limit Cycles Stabilizing Receding-Horizon Formulation for a Class of Hybrid Nonlinear Systems -- Generic Design of Dynamic State Feedback Using Receding-Horizon Schemes -- Application Examples -- Swing-Up Mechanical Systems -- Minimum-Time Constrained Stabilization of Nonholonomic Systems -- Stabilization of a Rigid Satellite in Failure Mode -- Receding-Horizon Solution to the Minimum-Interception-Time Problem -- Constrained Stabilization of a PVTOL Aircraft -- Limit Cycle Stabilizing Receding-Horizon Controller for the Planar Biped Rabbit. | |
520 | _aWhile conceptually elegant, the generic formulations of nonlinear model predictive control are not ready to use for the stabilization of fast systems. Dr. Alamir presents a successful approach to this problem based on a co-operation between structural considerations and on-line optimization. The balance between structural and optimization aspects of the method is dependent on the system being considered so the many examples aim to transmit a mode of thought rather than a ready-to-use recipe; they include: - double inverted pendulum; - non-holonomic systems in chained form; - snake board; - missile in intercept mission; - polymerization reactor; - walking robot; - under-actuated satellite in failure mode. In addition, the basic stability results under receding horizon control schemes are revisited using a sampled-time, low-dimensional control parameterization that is mandatory for fast computation and some novel formulations are proposed which offer promising directions for future research. | ||
650 | 0 | _aEngineering. | |
650 | 0 | _aChemical engineering. | |
650 | 0 | _aSystems theory. | |
650 | 0 | _aMathematical optimization. | |
650 | 1 | 4 | _aEngineering. |
650 | 2 | 4 | _aControl Engineering. |
650 | 2 | 4 | _aAutomation and Robotics. |
650 | 2 | 4 | _aSystems Theory, Control. |
650 | 2 | 4 | _aCalculus of Variations and Optimal Control; Optimization. |
650 | 2 | 4 | _aAutomotive and Aerospace Engineering, Traffic. |
650 | 2 | 4 | _aIndustrial Chemistry/Chemical Engineering. |
710 | 2 | _aSpringerLink (Online service) | |
773 | 0 | _tSpringer eBooks | |
776 | 0 | 8 |
_iPrinted edition: _z9781846284700 |
830 | 0 |
_aLecture Notes in Control and Information Sciences, _x0170-8643 ; _v339 |
|
856 | 4 | 0 | _uhttp://dx.doi.org/10.1007/978-1-84628-471-7 |
912 | _aZDB-2-ENG | ||
999 |
_c17252 _d17252 |