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010   $a3-030-47348-1
024 7 $a10.1007/978-3-030-47348-8
035   $a(CKB)4100000011243426
035   $a(DE-He213)978-3-030-47348-8
035   $a(MiAaPQ)EBC6199441
035   $a(PPN)248395475
035   $a(MiAaPQ)EBC29092824
035   $a(EXLCZ)994100000011243426
100   $a20200513d2020      u|         0
101 0 $aeng
135   $aurnn#---mamaa
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aOptimal Guidance and Its Applications in Missiles and UAVs /$fby Shaoming He, Chang-Hun Lee, Hyo-Sang Shin, Antonios Tsourdos
205   $a1st ed. 2020.
210  1$aCham :$cSpringer International Publishing :$cImprint: Springer,$d2020.
215   $a1 online resource (XIII, 214 p.) $c49 illus., 47 illus. in color
225 1 $aSpringer Aerospace Technology,$x1869-1749
311 1 $a3-030-47347-3 
327   $aIntroduction of Optimal Guidance -- Optimality of Error Dynamics in Missile Guidance -- Three-Dimensional Optimal Impact-Time-Control Guidance Law -- Gravity-Turn Assisted Optimal Guidance Law -- Observability-Enhancement Optimal Guidance Law -- Optimal Proportional-Integral Guidance Law -- Energy-Optimal Waypoint-Following Guidance Law -- Conclusions.
330   $aThis book presents a comprehensive overview of the recent advances in the domain of optimal guidance, exploring the characteristics of various optimal guidance algorithms and their pros and cons. Optimal guidance is based on the concept of trajectory optimization, which minimizes the meaningful performance index while satisfying certain terminal constraints, and by properly designing the cost function the guidance command can serve as a desired pattern for a variety of mission objectives. The book allows readers to gain a deeper understanding of how optimal guidance law can be utilized to achieve different mission objectives for missiles and UAVs, and also explores the physical meaning and working principle of different new optimal guidance laws. In practice, this information is important in ensuring confidence in the performance and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority.
410  0$aSpringer Aerospace Technology,$x1869-1749
606   $aAerospace engineering
606   $aAstronautics
606   $aControl engineering
606   $aRobotics
606   $aAutomation
606   $aComputational intelligence
606   $aAerospace Technology and Astronautics
606   $aControl, Robotics, Automation
606   $aComputational Intelligence
615  0$aAerospace engineering.
615  0$aAstronautics.
615  0$aControl engineering.
615  0$aRobotics.
615  0$aAutomation.
615  0$aComputational intelligence.
615 14$aAerospace Technology and Astronautics.
615 24$aControl, Robotics, Automation.
615 24$aComputational Intelligence.
676   $a623.4519
676   $a623.4519
700   $aHe$b Shaoming$4aut$4http://id.loc.gov/vocabulary/relators/aut$01061895
702   $aLee$b Chang-Hun$4aut$4http://id.loc.gov/vocabulary/relators/aut
702   $aShin$b Hyo-Sang$4aut$4http://id.loc.gov/vocabulary/relators/aut
702   $aTsourdos$b Antonios$4aut$4http://id.loc.gov/vocabulary/relators/aut
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910403766303321
996   $aOptimal Guidance and Its Applications in Missiles and UAVs$92521307
997   $aUNINA