マイクロバーストに対する操縦に関する一覚書
1988 年 36 巻 418 号 p. 520-528
詳細
1988 年 36 巻 418 号 p. 520-528
Flights against microburst are analysed as optimal control problems. A typical microburst model is used with a Dryden gust model superimposed on it. Control laws are those of an optimal regulator with Kalman-filter for noisy measurements. The result shows the importance of the accurate measurements of ground and air velocity as well as climb rates. The result also shows a control law which is close to optimal and which is feasible for practical use.
