| 000 | 03138cam a2200337Ia 4500 | ||
|---|---|---|---|
| 001 | CRC00E83139PDF | ||
| 003 | FlBoTFG | ||
| 005 | 20230510164702.0 | ||
| 006 | m o d | ||
| 007 | cr cn | ||
| 008 | 121126s2013 fluad ob 001 0 eng d | ||
| 020 | _a9780429141232 | ||
| 035 | _a(OCoLC)811060637 | ||
| 040 |
_aFlBoTFG _cFlBoTFG |
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| 082 |
_a623.4519 _bA244 |
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| 090 |
_aUG1310 _b.A38 2013 |
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| 100 | _aBalakrishnan, S. N., Tsourdos, A. and White, B. A. | ||
| 245 | 0 | 0 | _aAdvances in Missile Guidance, Control, and Estimation |
| 260 |
_aBoca Raton : _bCRC Press, _cc2012. |
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| 300 | _a720 p. : | ||
| 490 | 0 | _aAutomation and control series | |
| 505 | 0 | _a1. Robust autopilot design for quasilinear parameter-varying missile model / Antonios Tsourdos and Brian A. White -- 2. Polynomial approach for design and robust analysis of lateral missile control / Antonios Tsourdos, Brian A. White, and L. Bruyere -- 3. Control design and gain scheduling using observer-based structures / Daniel Alazard -- 4. Adaptive neural network-based autopilot design / Karthikeyan Rajagopal and S.N. Balakrishnan -- 5. Integrated guidance and control for missiles / Nathan Harl ... [et al.] -- 6. Higher-order sliding modes for missile guidance and control / Yuri B. Shtessel and Christian H. Tournes -- 7. Neoclassical missile guidance / Pini Gurfil -- 8. Differential geometry applied to missile guidance / Brian A. White and Antonios Tsourdos -- 9. Differential game-based interceptor missile guidance / Josef Shinar and Tal Shima -- 10. Optimal guidance laws with impact angle control / Chang-Kyung Ryoo, Min-Jea Tahk, and Hangju Cho -- 11. Integrated design of estimator and guidance law / Josef Shinar and Tal Shima -- 12. Introduction to particle filters for tracking and guidance / David Salmond -- 13. Practical techniques for the design of multirate digital guidance laws and autopilots / C.A. Rabbath, N. L�echevin, and M. Lauzon -- 14. Design of CLOS guidance system / G. Hexner and H. Weiss -- 15. Practical considerations in robust control of missiles / Kevin A. Wise. | |
| 520 |
_aThis volume considers the modern tactical missile, which has become a highly integrated package made up of many electronic, mechanical, electromechanical and pyrotechnic sub-systems. In addition to hardware, it also covers the guidance algorithm and workings of the missile autopilot. It demonstrates how all of the elements are integrated to function together in high-performance mode while maintaining cost effectiveness. This text offers unique coverage of the three major missile control components: guidance, control, and estimation. It includes contributed chapters from leading experts from six nations. Nonlinear control techniques and implementation issues are covered in detail-- _cProvided by publisher. |
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| 530 | _aAlso available in print edition. | ||
| 538 | _aMode of access: World Wide Web. | ||
| 650 | 0 |
_aGuided missiles _xGuidance systems. |
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| 655 | 7 |
_aElectronic books. _2lcsh |
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| 776 | 1 | _z9781420083132 (hardback) | |
| 856 | 4 | 0 |
_uhttp://marc.crcnetbase.com/isbn/9781420083149 _qebook |
| 942 |
_2ddc _cEBK |
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| 999 |
_c1003 _d1003 |
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