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Method for measuring servo current in real time during moudling loading of electromechanical servo mechanism

A technology of electromechanical servo and servo current, applied in the field of simulation test of electromechanical servo mechanism model flight

Pending Publication Date: 2022-05-17
BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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Problems solved by technology

[0004] In the previous semi-physical simulation test of electromechanical servo system, the test was carried out after the servo power supply and the power supply were turned on, and the real-time observation test of the servo current was not carried out.

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  • Method for measuring servo current in real time during moudling loading of electromechanical servo mechanism
  • Method for measuring servo current in real time during moudling loading of electromechanical servo mechanism

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Embodiment Construction

[0036] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention.

[0037] refer to Figure 1-2 , a method for real-time measurement of servo current when an electromechanical servo mechanism is loaded, comprising the following steps:

[0038] S1: Prepare the measuring device and conduct self-inspection, in order to ensure that there will be no sudden failure during use;

[0039] Measuring devices include control cabin, simulation test platform and control combination, electromechanical servo, servo protection device, steel plate loading device, ground servo power supply, cable and current measuring device;

[0040] In this embodiment, the control cabin is used to provide a more realistic environment for the electromechanical servo ...

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Abstract

The invention belongs to the technical field of simulated flight simulation test of an electromechanical servo mechanism, and particularly relates to a method for measuring servo current in real time during simulated flight loading of the electromechanical servo mechanism, which comprises the following steps of: S1, preparing a measuring device and performing self-inspection; the measuring device comprises a control cabin section, a simulation test platform control combination, an electromechanical servo, a servo protection device, a steel plate loading device, a ground servo power supply, a cable and a current measuring device; S2, mounting and fixing the electromechanical servo; s3, switching on a power supply and external control; and S4, connecting the simulation test platform and the control combination, and completing the preparation of the simulation system. According to the invention, in the semi-physical simulation of various deviation ballists, the working current of the servo battery can be collected and recorded in real time, the abrupt change peak value change curve can be recorded, the current parameters of the servo mechanism under the simulated real flight working condition can be truly measured, the verification can be provided for the parameters of the corresponding missile-borne battery, and the method can be suitable for different electromechanical servo mechanisms.

Description

technical field [0001] The invention relates to the technical field of simulation test of electromechanical servo mechanism model flight, in particular to a method for real-time measurement of servo current when electromechanical servo mechanism model flight is loaded. Background technique [0002] In the hardware-in-the-loop simulation test of some control systems, the electromechanical servo system will participate in the test as an important single machine. Electromechanical servo includes servo control driver, servo power supply, servo mechanism and servo cable. [0003] The electromechanical servo mechanism model flight loading device is to simulate the load moment and the moment of inertia relative to the rudder shaft that the electromechanical servo will bear during real flight. According to the test requirements, the electromechanical servo should be installed in the real control cabin. [0004] In the past hardware-in-the-loop simulation test of electromechanical s...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02G01R31/00
CPCG05B17/02G01R31/008
Inventor 黎阳吴骁赵谦谭芸
Owner BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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