FIELD: tool-making industry, possible use in rocket control systems.
SUBSTANCE: to achieve the effect depending on banking angle between control channels since the moment of control beginning, rocket control command module is determined and coefficient of ratio of maximal angle of rocket rudder deviation to command module. If command module exceeds maximal rudder deviation value, then rocket control commands are reduced proportionally to α coefficient. In the system for controlling two-channel rotary rocket, between control channels, signal module computation device, signal divider and first and second limiters-amplifiers are introduced. First and second inputs of signal module computation device are connected to outputs of rocket control command generation block.
EFFECT: increased precision of control angle.
2 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF CONTROL SIGNAL FORMING FOR DOUBLE-CHANNEL ROCKET ROTATING AROUND LONGITUDINAL AXIS | 2012 |
|
RU2511610C1 |
| CONTROL OVER SPACESHIP ANGULAR MOTION | 2011 |
|
RU2475428C1 |
| DEVICE FOR FORMATION OF COMMANDS TO CONTROL A ROCKET ROTATING AROUND ITS LONGITUDINAL AXIS | 2002 |
|
RU2235969C1 |
| METHOD OF COMBINED GUIDANCE OF SMALL-SIZED MISSILE WITH SEPARABLE PROPULSION SYSTEM AND GUIDANCE SYSTEM FOR ITS IMPLEMENTATION | 2014 |
|
RU2569046C1 |
| DEVICE FOR GENERATION OF SINGLE-CHANNEL CONTROL SIGNAL FOR ROTATING MISSILE | 1995 |
|
RU2111522C1 |
| DEVICE FOR AUTOMATICALLY SHIFTING AIRCRAFT FROM STALL AND SPINNING CONDITIONS TO STANDARD MODE OF FLIGHT | 2005 |
|
RU2280591C1 |
| METHOD FOR CONTROL OF ROCKET WITH AERODYNAMIC CONTROL SURFACES | 2000 |
|
RU2182306C2 |
| GUIDED MISSILE IN TRANSPORTER-LAUNCHER CONTAINER | 2012 |
|
RU2518126C2 |
| GUIDANCE METHOD OF MISSILE ROTATING ALONG CENTRE MARK ANGLE, GUIDANCE SYSTEM AND POSITION SENSOR FOR ITS IMPLEMENTATION | 2008 |
|
RU2406962C2 |
| METHOD OF MISSILE REMOTE CONTROL | 2011 |
|
RU2465535C1 |
