001432798 000__ 04829cam\a2200745\i\4500
001432798 001__ 1432798
001432798 003__ OCoLC
001432798 005__ 20230309003534.0
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001432798 007__ cr\nn\nnnunnun
001432798 008__ 201107s2021\\\\si\a\\\\ob\\\\000\0\eng\d
001432798 019__ $$a1204317216$$a1206394788$$a1232855809
001432798 020__ $$a9789811589010
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001432798 020__ $$z9811589003
001432798 020__ $$z9789811589003
001432798 0247_ $$a10.1007/978-981-15-8901-0$$2doi
001432798 035__ $$aSP(OCoLC)1225562800
001432798 040__ $$aSFB$$beng$$erda$$epn$$cSFB$$dOCLCO$$dOCLCF$$dGW5XE$$dYDX$$dERF$$dEBLCP$$dOCLCO$$dOCL$$dOCLCQ$$dOCLCO$$dCOM$$dOCLCQ
001432798 049__ $$aISEA
001432798 050_4 $$aTL571.5
001432798 08204 $$a629.132/306$$223
001432798 1001_ $$aChen, Wanchun,$$eauthor.
001432798 24510 $$aSteady glide dynamics and guidance of hypersonic vehicle /$$cWanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang.
001432798 264_1 $$aSingapore :$$bSpringer,$$c2021.
001432798 300__ $$a1 online resource :$$billustrations (some color)
001432798 336__ $$atext$$btxt$$2rdacontent
001432798 337__ $$acomputer$$bc$$2rdamedia
001432798 338__ $$aonline resource$$bcr$$2rdacarrier
001432798 504__ $$aIncludes bibliographical references.
001432798 5050_ $$aIntroduction -- Mathematical Fundamentals -- The Mathematical Model for Hypersonic Entry Glide Vehicle -- Mathematical description of optimal control problem for entry gliding -- Indirect approch to the optimal glide trajectory problem -- Direct Method for Gliding Trajectory Optimization Problem -- The Concept of Steady Glide Reentry Trajectory and the Stability of its Regular Perturbation Solutions -- Analytical Solutions of Steady Glide Reentry Trajectory in Three Dimensions and their Application to Trajectory Planning -- Trajectory Damping Control Technique for Hypersonic Glide Reentry -- Steady Glide Dynamic Modeling and Trajectory Optimization for High Lift-to-Drag Ratio Reentry Vehicle -- Singular Perturbation Guidance of Hypersonic Glide Reentry -- 3-D Reentry Guidance with Real-Time Planning of Reference with New Analytical Solutions Based on Spectral Decomposition Method -- Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical glide Formulas with the Consideration of the effects of the Earth's rotation -- Analytical Entry Guidance based on Steady Glide -- Linear Pseudospectral General Nominal Effort Miss Distance Guidance Method -- Linear Pseudospectral Adaptive Flight Phase Segmentation General Nominal Effort Miss Distance Reentry Guidance -- Trajectory-Shaping Guidance with Final Speed and Load Factor Constraints.
001432798 506__ $$aAccess limited to authorized users.
001432798 520__ $$aThis book presents the latest researches on hypersonic steady glide dynamics and guidance, including the concept of steady glide reentry trajectory and the stability of its regular perturbation solutions, trajectory damping control technique for hypersonic glide reentry, singular perturbation guidance of hypersonic glide reentry, trajectory optimization based on steady glide, linear pseudospectral generalized nominal effort miss distance guidance, analytical entry guidance and trajectory-shaping guidance with final speed and load factor constraints. They can be used to solve many new difficult problems in entry guidance. And many practical engineering cases are provided for the readers for better understanding. Researchers and students in the fields of flight vehicle design or flight dynamics, guidance and control could use the book as valuable reference.
001432798 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed January 26, 2021).
001432798 650_0 $$aAerodynamics, Hypersonic$$xMathematical models.
001432798 650_0 $$aHigh-speed aeronautics$$xMathematical models.
001432798 650_0 $$aGliders (Aeronautics)$$xStability.
001432798 650_0 $$aAerospace engineering.
001432798 650_0 $$aAstronautics.
001432798 650_0 $$aAutomatic control.
001432798 650_0 $$aAstronomy.
001432798 650_0 $$aAstrophysics.
001432798 650_0 $$aMathematical optimization.
001432798 650_0 $$aSystem theory.
001432798 650_6 $$aAérodynamique hypersonique$$xModèles mathématiques.
001432798 650_6 $$aVol à grande vitesse$$xModèles mathématiques.
001432798 650_6 $$aPlaneurs (Aéronautique)$$xStabilité.
001432798 650_6 $$aAérospatiale (Ingénierie)
001432798 650_6 $$aAstronautique.
001432798 650_6 $$aCommande automatique.
001432798 650_6 $$aAstronomie.
001432798 650_6 $$aAstrophysique.
001432798 650_6 $$aOptimisation mathématique.
001432798 650_6 $$aThéorie des systèmes.
001432798 655_0 $$aElectronic books.
001432798 7001_ $$aZhou, Hao,$$eauthor.
001432798 7001_ $$aYu, Wenbin,$$eauthor.
001432798 7001_ $$aYang, Liang,$$eauthor.
001432798 77608 $$iPrint version:$$z9789811589003
001432798 852__ $$bebk
001432798 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-981-15-8901-0$$zOnline Access$$91397441.1
001432798 909CO $$ooai:library.usi.edu:1432798$$pGLOBAL_SET
001432798 980__ $$aBIB
001432798 980__ $$aEBOOK
001432798 982__ $$aEbook
001432798 983__ $$aOnline
001432798 994__ $$a92$$bISE