The temperature control system is an indispensable key system for the thermal vacuum test. It is used to simulate the infrared heat flow environment of the spacecraft in orbit. In order to improve the stability and reliability of temperature control, this paper designs and develops a thermal vacuum test temperature control system based on the Modbus RTU serial communication protocol on the LabVIEW platform. The system combines the flexibility of software development on LabVIEW platform and combines the stability of serial communication with controller. This temperature control system has been used in thermal vacuum test, the control effect of overshooting within 1°C and temperature control accuracy within ±0.2°C. The system has high stabili...
In 2014 KTH Royal Institute of Technology initiated a space technology and research center, KTH Spac...
AbstractThermal vacuum test is widely used for the ground validation of spacecraft thermal control s...
A satellite is being integrated and tested by BISEE (Beijing Institute of Spacecraft Environment Eng...
The temperature control system is an indispensable key system for the thermal vacuum test. It is use...
Temperature measurement is a very important measurement project in spacecraft vacuum thermal test, a...
A universal software platform is developed for improving the defects in the practical one. This soft...
During the development of spacecraft, it is mandatory that they have to pass a number of important t...
The heat sink temperature is often set in a semi-empirical way based on steady-state temperatures . ...
A thermal vacuum facility for testing launch vehicle thermal protection systems by subjecting them t...
An advanced thermal control system for the Burst Alert Telescope on the Swift satellite has been des...
The Apollo Telescope Mount's thermal systems unit was utilized to conduct a full-scale thermal vacuu...
The purpose of this project is to develop a low-cost test set-up with the instruments used in therm...
The paper describes the specific temperature stability and control requirements for the thermal vacu...
At present, the spacecraft thermal test temperature measurement system has not been designed effecti...
Robotic and mechatronic systems are particularly sensitive regarding their thermal environment. The ...
In 2014 KTH Royal Institute of Technology initiated a space technology and research center, KTH Spac...
AbstractThermal vacuum test is widely used for the ground validation of spacecraft thermal control s...
A satellite is being integrated and tested by BISEE (Beijing Institute of Spacecraft Environment Eng...
The temperature control system is an indispensable key system for the thermal vacuum test. It is use...
Temperature measurement is a very important measurement project in spacecraft vacuum thermal test, a...
A universal software platform is developed for improving the defects in the practical one. This soft...
During the development of spacecraft, it is mandatory that they have to pass a number of important t...
The heat sink temperature is often set in a semi-empirical way based on steady-state temperatures . ...
A thermal vacuum facility for testing launch vehicle thermal protection systems by subjecting them t...
An advanced thermal control system for the Burst Alert Telescope on the Swift satellite has been des...
The Apollo Telescope Mount's thermal systems unit was utilized to conduct a full-scale thermal vacuu...
The purpose of this project is to develop a low-cost test set-up with the instruments used in therm...
The paper describes the specific temperature stability and control requirements for the thermal vacu...
At present, the spacecraft thermal test temperature measurement system has not been designed effecti...
Robotic and mechatronic systems are particularly sensitive regarding their thermal environment. The ...
In 2014 KTH Royal Institute of Technology initiated a space technology and research center, KTH Spac...
AbstractThermal vacuum test is widely used for the ground validation of spacecraft thermal control s...
A satellite is being integrated and tested by BISEE (Beijing Institute of Spacecraft Environment Eng...