| 000 | 01324nam a2200217 a 4500 | ||
|---|---|---|---|
| 001 | ASIN1563472759 | ||
| 005 | 20190522114910.0 | ||
| 008 | 120319s1998 xxu eng d | ||
| 020 |
_a1563472759 (hardcover) _c$104.95 |
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| 020 | _a9781563472756 (hardcover) | ||
| 100 | 1 | _aBen-Asher, J. | |
| 245 | 1 | 0 |
_aAdvances in missile guidance theory / _cJ. Ben-Asher, I. Yaesh. |
| 250 | _aHar/Dskt ed. | ||
| 260 |
_a[S.l.] : _bAIAA, _c1998. |
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| 300 |
_a200 p. ; _c24 cm. |
||
| 490 | 1 | _aProgress in astronautics and aeronautics. | |
| 520 | _aThis work is about terminal guidance of intercepting missiles. It contains a variety of newly developed guidance methods based on linear quadratic optimization problems. This application-oriented book employs widely used and thoroughly developed theories such as LQ and H-infinity to the problem of missile guidance. Numerous examples help the reader to gain greater understanding of the relative merits and shortcomings to the various methods. Both the analytical derivations and the numerical computations of the examples are carried out by MAPLE and MATLAB subroutine. The codes are provided with the book. | ||
| 700 | 1 | _aYaesh, I. | |
| 830 | 0 | _aProgress in astronautics and aeronautics. | |
| 856 | 4 | 0 |
_3Amazon.com _uhttp://www.amazon.com/exec/obidos/ASIN/1563472759/chopaconline-20 |
| 999 |
_c2270 _d2270 |
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