FIELD: automatic control systems; control systems for the position of inertial objects.
SUBSTANCE: invention can be used in control systems for pointing radars, actuators of mobile robotic systems, launchers, guns and turrets of self-propelled artillery vehicles designed to guide an inertial object to the required angular position. The essence of the claimed solution lies in the fact that in the inertial object guidance control system containing a serially connected master, a mismatch meter, the following devices connected in series: a switching unit, a power amplifier, an actuating element, the output of which is mechanically connected to the control object, a speed sensor, the input of which is mechanically connected to an actuating element, a position sensor, the input of which is mechanically connected to the control object, and the output is connected to the second input of the mismatch meter, the first null device, the input of which is connected to the output of the mismatch meter, the first threshold device, the OR element, a multiplication block is introduced, the first input of which is connected to the output of the mismatch meter, the second input is connected to the output of the speed sensor, and the output is connected to the input of the first threshold device, the second null device, the input of which is connected to the output of the mismatch meter, the second threshold device, the input of which is connected to the output of the speed sensor, the first AND element, the first input of which is connected to the output of the first null device, and the output is connected to the first input of the OR element, the second AND element, the first input of which is connected to the output of the second null device, and the output is connected to the second input of the OR element , the third AND element, the first input of which is connected to the output of the second threshold device, the second input is connected to the output of the first threshold device, the third input is connected to the output of the OR element, and the output is connected to the control input of the switching unit and to the second input of the first AND element, the NOT element , the input of which is connected to the output of the third element AND, and the output is connected to the second input of the second element AND, the first input of the switching unit is connected to the output of the mismatch meter.
EFFECT: increase in the speed of response.
1 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
INERTIAL OBJECT GUIDANCE CONTROL SYSTEM | 2014 |
|
RU2537256C1 |
TRACKING GUIDANCE SYSTEM | 2023 |
|
RU2815295C1 |
CONTROL SYSTEM FOR GUIDANCE OF INERTIAL OBJECT | 2002 |
|
RU2225633C1 |
GUIDANCE SYSTEM | 2023 |
|
RU2819712C1 |
GUIDANCE DRIVE | 2023 |
|
RU2817037C1 |
GUIDANCE SYSTEM | 2023 |
|
RU2805507C1 |
SERVO SYSTEM | 0 |
|
SU1081622A1 |
FOL-UP GUIDANCE SYSTEM | 2006 |
|
RU2347172C2 |
OBJECT BRIGHTENING SYSTEM | 1999 |
|
RU2163353C1 |
NONLINEAR CORRECTING DEVICE | 0 |
|
SU1536351A1 |
Authors
Dates
2023-05-12—Published
2022-05-11—Filed