| 000 | 01125nam a2200313 a 4500 | ||
|---|---|---|---|
| 005 | 20250914154325.0 | ||
| 008 | 060928s2005 vaua i 001 0 eng | ||
| 020 |
_a1563476959 _cRM330.12 |
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| 039 | 9 |
_a201310291704 _blan _c200611181619 _ddollah _c200611101054 _dfati _y09-28-2006 _zidah |
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| 040 | _dUKM | ||
| 090 | _aQA402.3.G884 | ||
| 090 |
_aQA402.3 _b.G884 |
||
| 100 | 1 | _aGutman, Shaul. | |
| 245 | 1 | 0 |
_aApplied min-max approach to missile guidance anda control / _cShaul Gutman. |
| 260 |
_aVirginia : _bAmerican Institute of Aeronautics and Astronautics, _c2005. |
||
| 300 |
_axvii, 298 p. : _bill. ; _c24 cm. |
||
| 440 | 0 |
_aProgress in astronautics and aeronautics ; _vvol. 209. |
|
| 504 | _aIncludes index. | ||
| 650 | 0 | _aControl theory. | |
| 650 | 0 |
_aGuided missiles _xControl systems _xMathematical models. |
|
| 650 | 0 |
_aFlight control _xMathematical models. |
|
| 907 |
_a.b13810248 _b2021-05-28 _c2019-11-12 |
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| 942 |
_c01 _n0 _kQA402.3.G884 |
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| 914 | _avtls003335914 | ||
| 990 | _afka | ||
| 991 | _aInstitut Sains Angkasa | ||
| 998 |
_at _b2006-02-09 _cm _da _feng _gvau _y0 _z.b13810248 |
||
| 999 |
_c378957 _d378957 |
||