FIELD: flying vehicle control and stabilization systems; guided missiles. SUBSTANCE: in guidance on target, phase shift introduced by on-board actuators at rocket rotational frequency are measured and input signal vector is turned through angle opposite to that being measured. Two-axis self-adaptive autopilot includes gyro position indicator and two actuator units; it is additionally provided with phase shifter, integrator, four ripple filters of second order, cosine non-linear converter, adder, two standard signal production units and four amplitude limiters. EFFECT: enhanced stabilization of rocket in the course of guidance. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SELF-OSCILLATING CONTROL ACTUATOR OF SPIN-STABILIZED GUIDED MISSILE | 2000 |
|
RU2184926C2 |
| SELF-EXCITED ACTUATOR OF GUIDED MISSILE ROTATING IN ROLL | 2003 |
|
RU2236669C1 |
| INTERRUPTED PNEUMATIC ACTUATOR OF CONTROL SYSTEM OF SPIN-STABILIZED MISSILES AND METHOD FOR MONITORING OF ITS DYNAMICS | 2000 |
|
RU2184340C2 |
| SPIN-STABILIZED MISSILE GUIDANCE SYSTEM | 2002 |
|
RU2234671C1 |
| SELF-OSCILLATING CONTROL ACTUATOR OF ROLL-STABILIZED GUIDED MISSILE | 2005 |
|
RU2288441C1 |
| MISSILE CONTROL SYSTEM | 2002 |
|
RU2218540C2 |
| METHOD FOR CONTROL OF MISSILE CONTROL ACTUATOR ELECTRO-PNEUMATIC DRIVE AND DEVICE FOR ITS REALIZATION | 2001 |
|
RU2206861C2 |
| METHOD FOR CONTROLLING TWO-CHANNEL ROTARY ROCKET AND CONTROL SYSTEM FOR ITS REALIZATION | 2006 |
|
RU2309446C1 |
| DEVICE FOR FORMATION OF COMMANDS TO CONTROL A ROCKET ROTATING AROUND ITS LONGITUDINAL AXIS | 2002 |
|
RU2235969C1 |
| METHOD TO GENERATE CONTROL INSTRUCTION FOR SPINNING TWO-CHANNEL ROCKET AND DEVICE TO THIS END | 2008 |
|
RU2373479C1 |
