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B.$3VANV200911 801 $aIT$bSOL$c20240614$gRICA 856 4 $uhttps://link.springer.com/openurl?genre=book&isbn=978-981-15-2097-6$zE-book - Accesso al full-text attraverso riconoscimento IP di Ateneo, proxy e/o Shibboleth 899 $aBIBLIOTECA DEL DIPARTIMENTO DI SCIENZE E TECNOLOGIE AMBIENTALI BIOLOGICHE E FARMACEUTICHE$1IT-CE0101$2VAN17 912 $fN 912 $aVAN0238815 950 $aBIBLIOTECA DEL DIPARTIMENTO DI SCIENZE E TECNOLOGIE AMBIENTALI BIOLOGICHE E FARMACEUTICHE$d17CONS e-book 2223 $e17BIB2223/398 398 20220201 996 $aGeoecology of Landscape Dynamics$91963827 997 $aUNICAMPANIA LEADER 03742nam 22006975 450 001 9910403766303321 005 20251113194430.0 010 $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. 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