Identifikatsiya Modeley Samoletov V Usloviyakh Strukturnoy Nepolnoty
| AUTHOR | Grebnev Oleg; Korsun Oleg |
| PUBLISHER | LAP Lambert Academic Publishing (07/04/2012) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
Monografiya posvyashchena probleme povysheniya tochnosti parametricheskoy identifikatsii matematicheskikh modeley samoletov po dannym letnogo eksperimenta v usloviyakh strukturnoy nepolnoty, to est' pri strukturnykh otlichiyakh prinyatoy modeli ot real'nogo ob"ekta.Opredeleny osnovnye strukturnye istochniki pogreshnostey identifikatsii aerodinamicheskikh koeffitsientov i polucheny kolichestvennye otsenki etikh pogreshnostey. Minimizatsiyu pogreshnostey identifikatsii predlagaetsya osushchestvlyat' na osnove sinteza spetsial'no podobrannykh testovykh signalov. Pri etom ispol'zuetsya dopushchenie, chto velichina strukturnoy pogreshnosti neizvestna, no imeetsya informatsiya o ee tipe. V ramkakh provedennykh issledovaniy razrabotan metod sinteza upravlyayushchego signala, obespechivayushchego zhelaemyy vykhodnoy signal. Razrabotana metodika nakhozhdeniya oblasti znacheniy parametrov upravlyayushchego signala, minimiziruyushchego pogreshnost' identifikatsii. Provedena aprobatsiya razrabotannykh metodov i otsenivanie ikh svoystv metodami matematicheskogo modelirovaniya.
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Product Format
Product Details
ISBN-13:
9783659158223
ISBN-10:
3659158224
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
Russian
More Product Details
Page Count:
144
Carton Quantity:
56
Product Dimensions:
6.00 x 0.34 x 9.00 inches
Weight:
0.49 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Technology & Engineering | Aeronautics & Astronautics
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publisher marketing
Monografiya posvyashchena probleme povysheniya tochnosti parametricheskoy identifikatsii matematicheskikh modeley samoletov po dannym letnogo eksperimenta v usloviyakh strukturnoy nepolnoty, to est' pri strukturnykh otlichiyakh prinyatoy modeli ot real'nogo ob"ekta.Opredeleny osnovnye strukturnye istochniki pogreshnostey identifikatsii aerodinamicheskikh koeffitsientov i polucheny kolichestvennye otsenki etikh pogreshnostey. Minimizatsiyu pogreshnostey identifikatsii predlagaetsya osushchestvlyat' na osnove sinteza spetsial'no podobrannykh testovykh signalov. Pri etom ispol'zuetsya dopushchenie, chto velichina strukturnoy pogreshnosti neizvestna, no imeetsya informatsiya o ee tipe. V ramkakh provedennykh issledovaniy razrabotan metod sinteza upravlyayushchego signala, obespechivayushchego zhelaemyy vykhodnoy signal. Razrabotana metodika nakhozhdeniya oblasti znacheniy parametrov upravlyayushchego signala, minimiziruyushchego pogreshnost' identifikatsii. Provedena aprobatsiya razrabotannykh metodov i otsenivanie ikh svoystv metodami matematicheskogo modelirovaniya.
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