Flight vehicle system identification : a time-domain methodology
This book offers a systematic approach to flight vehicle system identification and covers the time-domain methodology. It addresses theoretical and practical aspects of parameter estimation methods, including those in the stochastic framework focusing on nonlinear models, cost function, optimization...
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Main Author: | |
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Format: | eBook |
Language: | English |
Published: |
Reston, VA :
American Institute of Aeronautics and Astronautics, Inc.,
[2015]
|
Edition: | Second edition. |
Series: | Progress in astronautics and aeronautics ;
v. 245. |
Subjects: | |
ISBN: | 9781523100804 152310080X 9781624102790 1624102794 9781624102783 1624102786 |
Physical Description: | 1 online resource (xviii, 627 pages) : illustrations |
LEADER | 03515cam a2200481 i 4500 | ||
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001 | kn-ocn940509423 | ||
003 | OCoLC | ||
005 | 20240717213016.0 | ||
006 | m o d | ||
007 | cr cn||||||||| | ||
008 | 160222s2015 vaua ob 001 0 eng d | ||
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020 | |a 9781523100804 |q (electronic bk.) | ||
020 | |a 152310080X |q (electronic bk.) | ||
020 | |a 9781624102790 | ||
020 | |a 1624102794 | ||
020 | |z 9781624102783 | ||
020 | |z 1624102786 | ||
035 | |a (OCoLC)940509423 |z (OCoLC)932003169 |z (OCoLC)1097131448 | ||
100 | 1 | |a Jategaonkar, Ravindra V., |e author. | |
245 | 1 | 0 | |a Flight vehicle system identification : |b a time-domain methodology / |c Ravindra V. Jategaonkar. |
250 | |a Second edition. | ||
264 | 1 | |a Reston, VA : |b American Institute of Aeronautics and Astronautics, Inc., |c [2015] | |
264 | 4 | |c ©2015 | |
300 | |a 1 online resource (xviii, 627 pages) : |b illustrations | ||
336 | |a text |b txt |2 rdacontent | ||
337 | |a computer |b c |2 rdamedia | ||
338 | |a online resource |b cr |2 rdacarrier | ||
490 | 1 | |a Progress in astronautics and aeronautics ; |v volume 245 | |
504 | |a Includes bibliographical references and index. | ||
505 | 0 | |a Introduction -- Data gathering -- Model postulates and simulation -- Output-error method -- Filter-error method -- Equation-error methods -- Recursive parameter estimation -- Artificial neural networks -- Unstable aircraft identification -- Data compatibility check -- Model validation -- Selected advanced examples. | |
506 | |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty | ||
520 | |a This book offers a systematic approach to flight vehicle system identification and covers the time-domain methodology. It addresses theoretical and practical aspects of parameter estimation methods, including those in the stochastic framework focusing on nonlinear models, cost function, optimization methods, and residual analysis. A pragmatic and balanced account of pros and cons in each case is provided. It presents data gathering and model validation, covering large-scale and high-fidelity modeling. Real-world problems dealing with a variety of flight vehicle applications are addressed, and solutions are provided. Examples include: estimation of aerodynamic stability and control derivatives from flight data; flight-path reconstruction; nonlinearities in control surface effectiveness; stall hysteresis; unstable aircraft; flexible aircraft model integrating rigid-body and structural dynamics; wake vortex encounters; and other critical considerations. -- |c Edited summary from book. | ||
590 | |a Knovel |b Knovel (All titles) | ||
650 | 0 | |a Aerodynamics |x Mathematical models. | |
650 | 0 | |a Aeronautics |x Mathematical models. | |
650 | 0 | |a System identification. | |
650 | 0 | |a Time-domain analysis. | |
655 | 7 | |a elektronické knihy |7 fd186907 |2 czenas | |
655 | 9 | |a electronic books |2 eczenas | |
776 | 0 | 8 | |i Print version: |a Jategaonkar, Ravindra V. |t Flight vehicle system identification. |b Second edition |z 9781624102783 |w (OCoLC)903532332 |
830 | 0 | |a Progress in astronautics and aeronautics ; |v v. 245. | |
856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpFVSIAT04/flight-vehicle-system?kpromoter=marc |y Full text |