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001435353 001__ 1435353
001435353 003__ OCoLC
001435353 005__ 20230309003850.0
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001435353 008__ 210315s2021\\\\si\a\\\\o\\\\\000\0\eng\d
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001435353 020__ $$a9789811596315$$q(electronic bk.)
001435353 020__ $$a981159631X$$q(electronic bk.)
001435353 020__ $$z9811596301
001435353 020__ $$z9789811596308
001435353 0247_ $$a10.1007/978-981-15-9631-5$$2doi
001435353 035__ $$aSP(OCoLC)1244125593
001435353 040__ $$aDCT$$beng$$epn$$cDCT$$dOCLCO$$dEBLCP$$dGW5XE$$dOCLCO$$dYDX$$dOCLCF$$dUKAHL$$dOCLCQ$$dOCLCO$$dCOM$$dN$T$$dOCLCQ
001435353 049__ $$aISEA
001435353 050_4 $$aTL795.4
001435353 08204 $$a629.46$$223
001435353 08204 $$a629.1$$223
001435353 1001_ $$aMathavaraj, S.,$$eauthor.
001435353 24510 $$aSatellite formation flying :$$bhigh precision guidance using optimal and adaptive control techniques /$$cS. Mathavaraj, Radhakant Padhi.
001435353 264_1 $$aSingapore :$$bSpringer,$$c2021.
001435353 300__ $$a1 online resource (xxi, 154 pages) :$$billustrations (some color)
001435353 336__ $$atext$$btxt$$2rdacontent
001435353 337__ $$acomputer$$bc$$2rdamedia
001435353 338__ $$aonline resource$$bcr$$2rdacarrier
001435353 347__ $$atext file
001435353 347__ $$bPDF
001435353 5050_ $$aChapter 1: Introduction and Motivation -- Chapter 2: Satellite Orbital Dynamics -- Chapter 3: Infinite-time LQR and SDRE for Satellite Formation Flying -- Chapter4: Adaptive LQR for Satellite Formation Flying -- Chapter 5: Adaptive Dynamic Inversion for Satellite Formation Flying -- Chapter 6: Finite-time LQR and SDRE for Satellite Formation Flying -- Chapter 7: Model Predictive Static Programming -- Chapter 8: Performance Comparison.
001435353 506__ $$aAccess limited to authorized users.
001435353 520__ $$aSmall satellite technology is opening up a new era in space exploration offering reduced cost of launch and maintenance, operational flexibility with on-orbit reconfiguration, redundancy etc. The true power of such missions can be harnessed only from close and precise formation flying of satellites. Formation flying missions support diverse application areas such as reconnaissance, remote sensing, solar observatory, deep space observatories, etc. A key component involved in formation flying is the guidance algorithm that should account for system nonlinearities and unknown disturbances. The main focus of this book is to present various nonlinear optimal control and adaptive guidance ideas to ensure precise close formation flying in presence of such difficulties. In addition to in-depth discussion of the relevant topics, MATLAB program files for the results included are also provided for the benefit of the readers. Since this book has concise information about the various guidance techniques, it will be useful reference for researchers and practising engineers in the space field.
001435353 650_0 $$aMicrospacecraft$$xAutomatic control.
001435353 650_0 $$aAerospace engineering.
001435353 650_0 $$aAstronautics.
001435353 650_0 $$aVibration.
001435353 650_0 $$aDynamics.
001435353 650_0 $$aMathematical optimization.
001435353 650_6 $$aPetits véhicules spatiaux$$xCommande automatique.
001435353 650_6 $$aAérospatiale (Ingénierie)
001435353 650_6 $$aAstronautique.
001435353 650_6 $$aVibration.
001435353 650_6 $$aDynamique.
001435353 650_6 $$aOptimisation mathématique.
001435353 655_0 $$aElectronic books.
001435353 7001_ $$aPadhi, Radhakant,$$eauthor.
001435353 77608 $$iPrint version:$$z9789811596308
001435353 77608 $$iPrint version:$$z9789811596322
001435353 77608 $$iPrint version:$$z9789811596339
001435353 852__ $$bebk
001435353 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-981-15-9631-5$$zOnline Access$$91397441.1
001435353 909CO $$ooai:library.usi.edu:1435353$$pGLOBAL_SET
001435353 980__ $$aBIB
001435353 980__ $$aEBOOK
001435353 982__ $$aEbook
001435353 983__ $$aOnline
001435353 994__ $$a92$$bISE