| タイトル | Investigation of the Multiple Method Adaptive Control (MMAC) method for flight control systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790014928 |
| 著者（英） | Green, C. S.; Dunn, K. P.; Athans, M.; Baram, Y.; Lee, W. H.; Castanon, D.; Willsky, A. S.; Sandell, N. R., Jr. |
| 著者所属（英） | Massachusetts Inst. of Tech. |
| 発行日 | 1979-05-01 |
| 言語 | eng |
| 内容記述 | The stochastic adaptive control of the NASA F-8C digital-fly-by-wire aircraft using the multiple model adaptive control (MMAC) method is presented. The selection of the performance criteria for the lateral and the longitudinal dynamics, the design of the Kalman filters for different operating conditions, the identification algorithm associated with the MMAC method, the control system design, and simulation results obtained using the real time simulator of the F-8 aircraft at the NASA Langley Research Center are discussed. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 79N23099
NASA-CR-3089 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/175657 |
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