000 03684nam a22005895i 4500
001 978-981-15-9631-5
003 DE-He213
005 20220801214542.0
007 cr nn 008mamaa
008 210315s2021 si | s |||| 0|eng d
020 _a9789811596315
_9978-981-15-9631-5
024 7 _a10.1007/978-981-15-9631-5
_2doi
050 4 _aTL1-4050
072 7 _aTRP
_2bicssc
072 7 _aTTDS
_2bicssc
072 7 _aTEC002000
_2bisacsh
072 7 _aTRP
_2thema
072 7 _aTTDS
_2thema
082 0 4 _a629.1
_223
100 1 _aMathavaraj, S.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_939027
245 1 0 _aSatellite Formation Flying
_h[electronic resource] :
_bHigh Precision Guidance using Optimal and Adaptive Control Techniques /
_cby S. Mathavaraj, Radhakant Padhi.
250 _a1st ed. 2021.
264 1 _aSingapore :
_bSpringer Nature Singapore :
_bImprint: Springer,
_c2021.
300 _aXXI, 154 p. 96 illus., 88 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
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 _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.
650 0 _aAerospace engineering.
_96033
650 0 _aAstronautics.
_939028
650 0 _aMultibody systems.
_96018
650 0 _aVibration.
_96645
650 0 _aMechanics, Applied.
_93253
650 0 _aMathematical optimization.
_94112
650 1 4 _aAerospace Technology and Astronautics.
_939029
650 2 4 _aMultibody Systems and Mechanical Vibrations.
_932157
650 2 4 _aOptimization.
_939030
700 1 _aPadhi, Radhakant.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_939031
710 2 _aSpringerLink (Online service)
_939032
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9789811596308
776 0 8 _iPrinted edition:
_z9789811596322
776 0 8 _iPrinted edition:
_z9789811596339
856 4 0 _uhttps://doi.org/10.1007/978-981-15-9631-5
912 _aZDB-2-ENG
912 _aZDB-2-SXE
942 _cEBK
999 _c76474
_d76474