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Detection device of attitude control integrated controller

A technology of attitude control and detection device, which is applied in the general control system, control/regulation system, test/monitoring control system, etc., to achieve the effect of deducting the round-trip time delay, simplifying the installation work, and wide detection coverage

Active Publication Date: 2021-07-09
杭州航天电子技术有限公司
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  • Abstract
  • Description
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  • Application Information

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Problems solved by technology

[0003] The object to be achieved by the present invention is to provide a detection device for the integrated controller of attitude control, which can effectively solve the problems of coordination and controllability of the integrated controller of attitude control in the testing process

Method used

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  • Detection device of attitude control integrated controller
  • Detection device of attitude control integrated controller
  • Detection device of attitude control integrated controller

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Experimental program
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Embodiment Construction

[0019] Such as figure 1 , figure 2 , image 3 As shown, a detection device for an attitude control integrated controller includes a base plate 1, a host computer 2, an attitude signal generation unit 3, an attitude adjustment action unit 4, and a power detection unit 5. The host computer 2, the attitude signal generation unit The unit 3, the attitude adjustment action unit 4 and the power detection unit 5 are all arranged on the base plate 1, and the host computer 2 is respectively connected with the attitude signal generation unit 3, the attitude adjustment action unit 4 and the power detection unit 5. The bottom plate 1 is provided with a fixed structure 11 fixed to the measured attitude control integrated controller 8, and the attitude signal generating unit 3 and the attitude adjustment action unit 4 are provided with a first integrated controller connected to the measured attitude control. A communication cable 6 , the attitude signal generating unit 3 is provided with...

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Abstract

The invention relates to a detection device of an attitude control integrated controller, which comprises a bottom plate, an upper computer, an attitude signal generation unit, an attitude adjustment action unit and a power supply power detection unit, and is characterized in that the attitude signal generation unit and the attitude adjustment action unit are respectively provided with a first communication cable, and the attitude signal generation unit is provided with a second communication cable; the device has the advantages that the upper computer receives uploaded information of the attitude signal generation unit, the attitude adjustment action unit, the power supply power measurement unit and the tested attitude control integrated controller at the same time, the requirements of input of external attitude signals of the integrated controller, a connection object of signal output of the integrated controller and interfaces and cables for information transmission in the process are met, the requirements of a working power supply of the integrated controller and the requirement of metering the power consumption of the integrated controller are met, the requirements of test equipment are reduced, the cost of production equipment is greatly reduced, and the detection coverage is wider.

Description

technical field [0001] The invention relates to a detection device of an attitude control integrated controller. Background technique [0002] Micro-satellite precision attitude measurement and control system mainly includes: control computer, reaction flywheel (reaction torque), magnetic torque device (magnetic control torque), magnetometer (magnetic field measurement), inertial components (MEMS gyroscope and high-precision fiber optic gyroscope, attitude Angle and angular velocity measurement), star sensor (earth vector measurement), sun sensor (sun vector measurement) and GPS / BD receiver (orbit measurement) and other functional units. The above-mentioned systems generally adopt a conventional decentralized control strategy: that is, each flywheel and each magnetic torque device has its own controller and is a self-contained small system, which receives the telemetry and remote control of the attitude control computer through the digital communication interface, which has ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02
CPCG05B23/0221
Inventor 刘小旦丁强朱晓谷璐璐姚伟军
Owner 杭州航天电子技术有限公司