FIELD: aviation. SUBSTANCE: flying vehicle has case, two outer wing panels, fin and two stabilizer panels. Fin, wing panels and stabilizer panels are mounted for rotation around respective lateral axes of body-axis coordinate system of flying vehicle. Rim is additionally mounted on case rotation around longitudinal axis of body-axis coordinate system of flying vehicle; wing panel axles are fitted in this rim. EFFECT: normal functioning of all systems of flying vehicle in forming rather high horizontal aerodynamic force. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FLYING VEHICLE AERODYNAMIC CONFIGURATION | 1993 |
|
RU2093417C1 |
| CONTROL ACTUATOR OF ALL-MOVING AERODYNAMIC SURFACE | 1994 |
|
RU2090446C1 |
| WAY OF REMOTE DETERMINATION OF COORDINATES OF POSITION OF GROUND OBJECT | 2000 |
|
RU2182713C2 |
| METHOD OF TURNING FLYING VEHICLE CONTROL AERODYNAMIC SURFACE | 2001 |
|
RU2193992C2 |
| CONTROL ACTUATOR OF ALL-MOVING AERODYNAMIC SURFACE | 1993 |
|
RU2072311C1 |
| METHOD FOR DETECTION OF AIRCRAFT POSITION | 1998 |
|
RU2148795C1 |
| METHOD OF ORIENTATION OF VISION FIELD OF SURVEILLANCE SYSTEM | 2000 |
|
RU2183023C2 |
| METHOD FOR DETERMINATION OF VALUES OF PARAMETERS OF BOMB TRAJECTORY | 2002 |
|
RU2212620C1 |
| PROCEDURE ESTABLISHING LIMITS OF RANGE OF POSSIBLE LAUNCH OF ROCKET | 2001 |
|
RU2206044C2 |
| AUTOMOBILE | 1995 |
|
RU2104895C1 |
