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High-integration high-precision servo control device for control moment gyros

A technology for controlling torque gyroscopes and servo control devices, applied in program control, computer control, general control systems, etc., can solve the problems of low integration, increased power consumption, volume, quality and cost of control torque gyroscope servo systems

Inactive Publication Date: 2014-09-17
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The servo control of the control torque gyro is usually divided into the servo control of the frame motor and the flywheel motor, that is, the frame motor and the flywheel motor are servo-controlled based on their respective circuit systems, which will increase the power consumption, volume, quality and cost, the system integration is low

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Embodiment

[0032] The present invention can simultaneously perform high-precision servo control on two sets of control torque gyroscopes. The main controller DSP8 receives the control torque gyroscope group servo instructions through the CAN bus interface 7, including frame motor I14, flywheel motor I20, frame motor II17 and flywheel motor II24 servo command, and trigger the servo program that controls the torque gyroscope group.

[0033] Taking the control torque gyro servo control of a single set as an example, use the U / V phase current acquisition circuit I15 to obtain the U phase and V phase currents of the frame motor I14 in real time, and obtain the d / q axis current value i after coordinate transformation q1 i d1 , utilize the frame I position acquisition circuit 11 to acquire the frame I position θ of the frame motor I14 in real time 1 , further calculate the angular velocity Gω m1 , the main controller DSP8 according to the expected speed of the frame motor I14 and the feedba...

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Abstract

The invention discloses a high-integration high-precision servo control device for a control moment gyros, and is applied to the satellite attitude control executing mechanism. A slave controller FPGA acquires frame angular position signals of two frame motors through two frame position acquisition circuits respectively in real time, and acquires angular velocity signals of two flywheel motors through two hall signal acquisition circuits respectively in real time, and the signals are sent to a master controller DSP through an address / data / control bus to serve as respective velocity feedback values; the master controller DSP respectively acquires current values of the two frame motors and the two flywheel motors through two U / V phase current acquisition circuits and two busbar current acquisition circuits to serve as respective current feedback values; the master controller DSP carries out double closed-loop control over the velocity and current of the four sets of motors by combining with a corresponding servo control algorithm according to respective velocity and current feedback values, to produce a PWM instruction, the slave controller FPGA produces PWM according to the instruction, and high-precision servo control over the four sets of motors is realized.

Description

technical field [0001] The invention relates to a highly integrated and high-precision control torque gyroscope group servo control device, which is used for the servo control of two sets of control torque gyroscopes, and is suitable for high-integration, high-precision small and medium-sized agile satellite attitude control actuators. Background technique [0002] As a small and medium-sized agile satellite attitude control actuator, the control moment gyroscope can output dozens of times the torque of the traditional flywheel under the same power consumption, volume and mass by using its "torque amplification" feature, which greatly shortens the satellite maneuvering time. Realize multiple push-broom and splicing imaging of wide-format targets within a single track. The control moment gyro has been successfully applied in the WorldView-1 / 2 and Pleiades satellites, which greatly enhanced the maneuverability of the satellites and improved the agility of the satellites. [0...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/28G05B19/042
CPCB64G1/28
Inventor 金光陈茂胜穆欣戴路徐振陶淑苹
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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