| 摘要 |
FIELD: aircraft engineering.SUBSTANCE: three-point registration methods are selected, directing paths are straightened and rocket guidance proportional convergence is performed. Rocket guidance processes are ranked by descending priority. Generated and compared are predicted and threshold magnitudes of target elevation at rocket launching moment, rocket launching angle in vertical plane, rocket flight range, rocket flight speed, rocket bearing, rocket available overload and angle of rendezvous of rocket with target. Rocket destruction area boundaries are defined and selected guidance method is set. Target coordinates are tracked and measured and conditions of rendezvous of rocket with target are predicted. Rocker guidance method is selected and defined are methods of rocket launching and angles of rocket launching. Rocket is launched and guided to target.EFFECT: higher efficiency of guidance.3 cl, 1 dwg |
