航空機の進入経路に関する一考察
1992 年 40 巻 467 号 p. 674-681
詳細
1992 年 40 巻 467 号 p. 674-681
Approach paths of a single aircraft coming into a terminal area were solved numerically. The problem of calculating approach paths was formulated in terms of the optimal control problem. And then, inequality constraints of a state variable and control variables were taken into account so that numerical results might be consistent with approach paths of an actual aircraft. It was shown how the approach paths of a single aircraft depended upon functionals, inital conditions and terminal conditions.
