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
| Title | Year | Author | Number |
|---|---|---|---|
| MISSILE GUIDANCE METHOD | 2009 |
|
RU2426969C2 |
| METHOD AND SYSTEM FOR DETERMINING MOST FAVOURABLE FOR ATTACK AERIAL TARGETS IN MULTI-PURPOSE TRACKING MODE | 2020 |
|
RU2743479C1 |
| METHOD FOR LAUNCHING A SURFACE-TO-AIR MISSILE AND SURFACE-TO-AIR MISSILE LAUNCH SYSTEM | 2021 |
|
RU2790339C1 |
| REMOTELY CONTROLLED MISSILE GUIDANCE METHOD | 2016 |
|
RU2645850C1 |
| METHOD FOR INTERCEPTING THE PRIORITY TARGETS WITH DISRUPTING THE GUIDANCE OF ACCOMPANYING FIGHTERS | 2020 |
|
RU2742737C1 |
| METHOD OF LONG-RANGE TARGET CAPTURE OF ZONE MISSILE HOMING HEAD AND LONG MISSILE GUIDANCE SYSTEM | 2015 |
|
RU2583347C1 |
| METHOD OF GUIDANCE OF TELECONTROLLED MISSILE AND GUIDANCE SYSTEM FOR ITS REALIZATION | 1996 |
|
RU2106597C1 |
| ROTATING SELF-GUIDED ROCKET | 2002 |
|
RU2216707C1 |
| METHOD FOR COMMAND TELECONTROL OF MISSILE | 2000 |
|
RU2188381C2 |
| METHOD FOR EXPELLING MISSILE TO TRACK INITIATION AREA WITH TARGET SEEKING HEAD, AND SYSTEM FOR ITS IMPLEMENTATION (VERSIONS) | 2013 |
|
RU2542691C1 |
