000 | 04164cam a2200673Mu 4500 | ||
---|---|---|---|
001 | on1170936170 | ||
003 | OCoLC | ||
005 | 20220908100219.0 | ||
006 | m d | ||
007 | cr |n||||||||| | ||
008 | 160321s2014 nju o ||| 0 eng d | ||
040 |
_aLUN _beng _cLUN _dIEEEE _dOCLCO _dIDEBK _dYDXCP _dEBLCP _dREB _dWYU _dAU@ _dSNU _dOCLCF _dOCLCQ _dOCLCO |
||
019 |
_a885020083 _a1058593797 _a1170529976 _a1170702326 |
||
020 | _a1400855985 | ||
020 | _a9781400855988 | ||
020 |
_a1306990629 _q(ebk) |
||
020 |
_a9781306990622 _q(ebk) |
||
020 | _a1680158988 | ||
020 | _a9781680158984 | ||
035 |
_a(OCoLC)1170936170 _z(OCoLC)885020083 _z(OCoLC)1058593797 _z(OCoLC)1170529976 _z(OCoLC)1170702326 |
||
037 |
_a9453331 _bIEEE |
||
050 | 4 | _aTL676 ǂb .M32 1973eb | |
082 | 0 | 4 | _a629.134/33 |
049 | _aMAIN | ||
100 | 1 |
_aMcRuer, Duane T. _965642 |
|
245 | 1 | 0 |
_aAircraft Dynamics and Automatic Control _h[electronic resource]. |
260 |
_aPrinceton : _bPrinceton University Press, _c2014. |
||
300 | _a1 online resource (0 p.). | ||
336 |
_atext _btxt _2rdacontent |
||
337 |
_acomputer _bc _2rdamedia |
||
338 |
_aonline resource _bcr _2rdacarrier |
||
490 | 1 | _aPrinceton Legacy Library | |
500 | _aDescription based upon print version of record. | ||
500 | _aCover. | ||
520 | _aAeronautical engineers concerned with the analysis of aircraft dynamics and the synthesis of aircraft flight control systems will find an indispensable tool in this analytical treatment of the subject. Approaching these two fields with the conviction that an understanding of either one can illuminate the other, the authors have summarized selected, interconnected techniques that facilitate a high level of insight into the essence of complex systems problems. These techniques are suitable for establishing nominal system designs, for forecasting off-nominal problems, and for diagnosing the root causes of problems that almost inevitably occur in the design process. A complete and self-contained work, the text discusses the early history of aircraft dynamics and control, mathematical models of linear system elements, feedback system analysis, vehicle equations of motion, longitudinal and lateral dynamics, and elementary longitudinal and lateral feedback control. The discussion concludes with such topics as the system design process, inputs and system performance assessment, and multi-loop flight control systems. Originally published in 1974. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905. | ||
546 | _aEnglish. | ||
590 |
_aIEEE _bIEEE Xplore Princeton University Press eBooks Library |
||
650 | 0 |
_aAirplanes _xControl systems. _964422 |
|
650 | 0 |
_aFeedback control systems. _93888 |
|
650 | 4 |
_aAirplanes -- Control systems. _965643 |
|
650 | 4 |
_aFeedback control systems. _93888 |
|
650 | 6 |
_aAvions _xSyst�emes de commande. _964424 |
|
650 | 6 |
_aSyst�emes �a r�eaction. _965644 |
|
650 | 7 |
_aAirplanes _xControl systems. _2fast _0(OCoLC)fst00803111 _964422 |
|
650 | 7 |
_aFeedback control systems. _2fast _0(OCoLC)fst00922447 _93888 |
|
655 | 0 |
_aElectronic books. _93294 |
|
655 | 4 |
_aElectronic books. _93294 |
|
700 | 1 |
_aGraham, Dunstan. _965645 |
|
700 | 1 |
_aAshkenas, Irving. _965646 |
|
776 | 0 | 8 |
_iPrint version: _z0691024405 |
776 | 0 | 8 |
_iPrint version: _z0691600384 |
830 | 0 |
_aPrinceton legacy library. _963802 |
|
856 | 4 | 0 | _uhttps://ieeexplore.ieee.org/servlet/opac?bknumber=9453331 |
938 |
_aProQuest Ebook Central _bEBLB _nEBL3030518 |
||
938 |
_aProQuest MyiLibrary Digital eBook Collection _bIDEB _ncis28704733 |
||
938 |
_aYBP Library Services _bYANK _n11997048 |
||
942 | _cEBK | ||
994 |
_a92 _bINTKS |
||
999 |
_c81489 _d81489 |