Optimal Guidance and Its Applications in Missiles and UAVs (Record no. 77273)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 03806nam a22006375i 4500 |
| 001 - CONTROL NUMBER | |
| control field | 978-3-030-47348-8 |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20220801215237.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 200513s2020 sz | s |||| 0|eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| ISBN | 9783030473488 |
| -- | 978-3-030-47348-8 |
| 082 04 - CLASSIFICATION NUMBER | |
| Call Number | 629.1 |
| 100 1# - AUTHOR NAME | |
| Author | He, Shaoming. |
| 245 10 - TITLE STATEMENT | |
| Title | Optimal Guidance and Its Applications in Missiles and UAVs |
| 250 ## - EDITION STATEMENT | |
| Edition statement | 1st ed. 2020. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Number of Pages | XIII, 214 p. 49 illus., 47 illus. in color. |
| 490 1# - SERIES STATEMENT | |
| Series statement | Springer Aerospace Technology, |
| 505 0# - FORMATTED CONTENTS NOTE | |
| Remark 2 | Introduction 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 ## - SUMMARY, ETC. | |
| Summary, etc | This 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. |
| 700 1# - AUTHOR 2 | |
| Author 2 | Lee, Chang-Hun. |
| 700 1# - AUTHOR 2 | |
| Author 2 | Shin, Hyo-Sang. |
| 700 1# - AUTHOR 2 | |
| Author 2 | Tsourdos, Antonios. |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | https://doi.org/10.1007/978-3-030-47348-8 |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | eBooks |
| 264 #1 - | |
| -- | Cham : |
| -- | Springer International Publishing : |
| -- | Imprint: Springer, |
| -- | 2020. |
| 336 ## - | |
| -- | text |
| -- | txt |
| -- | rdacontent |
| 337 ## - | |
| -- | computer |
| -- | c |
| -- | rdamedia |
| 338 ## - | |
| -- | online resource |
| -- | cr |
| -- | rdacarrier |
| 347 ## - | |
| -- | text file |
| -- | |
| -- | rda |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Aerospace engineering. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Astronautics. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Control engineering. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Robotics. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Automation. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Computational intelligence. |
| 650 14 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Aerospace Technology and Astronautics. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Control, Robotics, Automation. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Computational Intelligence. |
| 830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE | |
| -- | 1869-1749 |
| 912 ## - | |
| -- | ZDB-2-ENG |
| 912 ## - | |
| -- | ZDB-2-SXE |
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