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008 200513s2020 sz | s |||| 0|eng d
020 _a9783030473488
_9978-3-030-47348-8
024 7 _a10.1007/978-3-030-47348-8
_2doi
050 4 _aTL1-4050
072 7 _aTRP
_2bicssc
072 7 _aTTDS
_2bicssc
072 7 _aTEC002000
_2bisacsh
072 7 _aTRP
_2thema
072 7 _aTTDS
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082 0 4 _a629.1
_223
100 1 _aHe, Shaoming.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_943203
245 1 0 _aOptimal Guidance and Its Applications in Missiles and UAVs
_h[electronic resource] /
_cby Shaoming He, Chang-Hun Lee, Hyo-Sang Shin, Antonios Tsourdos.
250 _a1st ed. 2020.
264 1 _aCham :
_bSpringer International Publishing :
_bImprint: Springer,
_c2020.
300 _aXIII, 214 p. 49 illus., 47 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aSpringer Aerospace Technology,
_x1869-1749
505 0 _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.
520 _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.
650 0 _aAerospace engineering.
_96033
650 0 _aAstronautics.
_943204
650 0 _aControl engineering.
_931970
650 0 _aRobotics.
_92393
650 0 _aAutomation.
_92392
650 0 _aComputational intelligence.
_97716
650 1 4 _aAerospace Technology and Astronautics.
_943205
650 2 4 _aControl, Robotics, Automation.
_931971
650 2 4 _aComputational Intelligence.
_97716
700 1 _aLee, Chang-Hun.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_943206
700 1 _aShin, Hyo-Sang.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_943207
700 1 _aTsourdos, Antonios.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_943208
710 2 _aSpringerLink (Online service)
_943209
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9783030473471
776 0 8 _iPrinted edition:
_z9783030473495
776 0 8 _iPrinted edition:
_z9783030473501
830 0 _aSpringer Aerospace Technology,
_x1869-1749
_943210
856 4 0 _uhttps://doi.org/10.1007/978-3-030-47348-8
912 _aZDB-2-ENG
912 _aZDB-2-SXE
942 _cEBK
999 _c77273
_d77273