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008			220112s2021 si | s |||| 0|eng d
020			_a9789811596315
024	7		_a10.1007/978-981-15-9631-5 _2doi
040			_aES-MaUEC _bspa _cES-MaUEC _dES-MaUEC
050		4	_aTL795.4 _b2021 EB
100	1		_aMathavaraj, S. _eautor _9680516
245	1	0	_aSatellite Formation Flying : _bHigh Precision Guidance using Optimal and Adaptive Control Techniques _cby S. Mathavaraj, Radhakant Padhi
250			_aFirst edition 2021
264		1	_aSingapore _bSpringer International Publishing _c2021
300			_a1 recurso en línea (XXI, 154 páginas) _b 96 ilustraciones, 88 ilustraciones a color
336			_2rdacontent _aTexto _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
347			_aarchivo de texto _bPDF
490	0		_aEngineering (SpringerNature-11647)
490	0		_aEngineering (R0) (SpringerNature-43712)
505	0		_aChapter 1: Introduction and Motivation -- Chapter 2: Satellite Orbital Dynamics -- Chapter 3: Infinite-time LQR and SDRE for Satellite Formation Flying -- Chapter4: Adaptive LQR for Satellite Formation Flying -- Chapter 5: Adaptive Dynamic Inversion for Satellite Formation Flying -- Chapter 6: Finite-time LQR and SDRE for Satellite Formation Flying -- Chapter 7: Model Predictive Static Programming -- Chapter 8: Performance Comparison.
520	3		_aSmall satellite technology is opening up a new era in space exploration offering reduced cost of launch and maintenance, operational flexibility with on-orbit reconfiguration, redundancy etc. The true power of such missions can be harnessed only from close and precise formation flying of satellites. Formation flying missions support diverse application areas such as reconnaissance, remote sensing, solar observatory, deep space observatories, etc. A key component involved in formation flying is the guidance algorithm that should account for system nonlinearities and unknown disturbances. The main focus of this book is to present various nonlinear optimal control and adaptive guidance ideas to ensure precise close formation flying in presence of such difficulties. In addition to in-depth discussion of the relevant topics, MATLAB program files for the results included are also provided for the benefit of the readers. Since this book has concise information about the various guidance techniques, it will be useful reference for researchers and practising engineers in the space field.
988			_aSpringer_Engineering_2021
650		7	_2embne _9139695 _aSatélites artificiales
650		7	_2embne _9139696 _aVehículos espaciales
700	1		_aPadhi, Radhakant _eautor _9680517
776	0	8	_iPrinted edition: _z9789811596308
776	0	8	_iPrinted edition: _z9789811596322
776	0	8	_iPrinted edition: _z9789811596339
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-981-15-9631-5 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_b01/2022 _dz _eIG _zSI