| タイトル | Method of discrete modeling and its application to estimation of TF30 engine variables |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770004114 |
| 著者（英） | Arpasi, D. J.; Bruton, W. M. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1976-10-01 |
| 言語 | eng |
| 内容記述 | A method of discrete modeling is presented that effectively isolates steady state model accuracy from dynamic model accuracy. The steady state model may be generated from the engine design equations with any desired degree of accuracy. The dynamic model is generated by applying a step disturbance of a manipulated variable to an open loop engine simulation. The sampled response of the variable is combined with the steady state model's response to form a set of weighting factors. These weighting factors are then used to weight past values of the manipulated variable, thus forming the dynamic model. The method is used to estimate various TF30-P-3 engine variables. A dynamic trim function is developed to compensate for the dynamic nonlinearities of the variables as well as for inaccuracies in dynamic definition. The trim function is shown to be realted to the square root of the sum of the squares of the weighting factors obtained at various engine operating conditions. Finally, the estimation of variables without dynamic modeling is discussed. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 77N11057
NASA-TM-X-3443
E-8560 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/184076 |
