High-precision distributed temperature measurement system

Abstract

The invention discloses a high-precision distributed temperature measurement system, which comprises a temperature sensor assembly, a temperature acquisition assembly and a thermal control lower computer, wherein the temperature sensor assembly comprises a platinum resistor, a precision resistor, a signal conditioning circuit and a packaging shell body; the platinum resistor and the precision resistor are connected in series and installed in the packaging shell body; the platinum resistor and the precision resistor are temperature quantity signal input sources, and the conditioning circuit conditions a temperature measured signal into a voltage signal to be acquired by the temperature acquisition assembly; the temperature sensor assembly and the temperature acquisition assembly are arranged at temperature control objects, the number of the temperature acquisition assemblies is one, and one temperature acquisition assembly corresponds to 1-4 temperature sensor assemblies; and a multi-way switch is used for switching different temperature acquisition assemblies, the potential difference between the platinum resistor and the precision resistor is acquired, the potential difference isamplified and converted into a digital signal, the digital signal is transmitted to the thermal control lower computer, and the measured temperature is obtained through calculation by means of the thermal control lower computer. According to the high-precision distributed temperature measurement system, the temperature measurement precision and stability are effectively improved.

Description

technical field [0001] The invention relates to the technical field of spacecraft temperature measurement and control, in particular to a high-precision distributed temperature measurement system. Background technique [0002] Electric heating active thermal control devices generally include heaters, controllers and temperature sensors, forming a closed-loop control loop, such as figure 1 shown. The temperature sensor is used to obtain the temperature signal T of the controlled object m ; The heater provides heat as a control actuator. The controller will obtain the temperature signal with the set value T d Compare, so as to obtain the error signal e(k)=T d -T m , and combined with the temperature control algorithm, generate the control output u to control the working state of the heater. [0003] The controller is the temperature controller, which is mainly responsible for temperature acquisition and control. The spacecraft temperature controller adopting the centrali...

AI Technical Summary

Problems solved by technology

[0006] (1) The temperature controller used in aerospace is arranged in the cabin, and its operating temperature is relatively wide, generally -15°C to +50°C, resulting in a large temperature drift of the system, which is mainly reflected in the reference resistor, amplifier, reference voltage source, constant Temperature drift of current source, AD and other devices

[0007] (2) The temperature sensor is far away from the temperature acquisition circuit located inside the temperature controller, which may require cable transfer, and there is contact resistance

[0008] (3) Long-distance transmission of weak measurement signals (microvolt-level voltage signals), susceptible to electromagnetic interference from the surrounding environment inside and outside the satellite ca

Images