The structure of the on-board algorithm of executing the tactical turn-away defensive maneuver by an aircraft

被引：0

作者：

Demkin, M.A. ^{[1
]}

Novakov, D.V. ^{[1
]}

Fedunov, B.E. ^{[1
]}

机构：

[1] Moscow Inst. of Aviation, Volokolamskoe sh. 4, Moscow, 115409, Russia

来源：

Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya | 2002年 / 05期

关键词：

Aircraft - Algorithms - Maneuverability - Motion control - Trajectories;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

We consider the structure of the algorithms of the trajectory control of an aircraft that executes defensive maneuvers aimed at maximally fast braking of an attacking (from the forward hemisphere) guided missile of the air-to-air class. The algorithm uses the tables of parameters of an enemy's guided missile and the coefficients of polynomial approximation of the line of switching of the control of the evading aircraft.

引用

页码：162 / 174