In space industry thermal models are an important tool to predict, analyze and understand the thermal behaviour of components, subsystems and whole spacecrafts. Most parameters of these models have a limited accuracy and consequently the models results are uncertain. In order to reduce this uncertainty to a required level the model parameters are adjusted (correlated) by fitting the model to test results obtained during thermo vacuum tests. This is often a difficult long lasting manual process. In order to perform these correlations automatically many different methods have been developed and analyzed. Two of these methods are analyzed regarding their requirements, efficiency and limitations. A genetic algorithm is compared to a method base...
The correlation of the Thermal Mathematical Models is often performed manually, and the results obta...
This paper presents a mathematically rigorous, subspace projection-based reduced order modeling (ROM...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010.Ca...
The design of the thermal control system of space vehicles, needed to maintain the equipment compone...
Genetic algorithms have been used for matching temperature values generated using thermal mathematic...
There are always differences between the computer predicted temperatures of a spacecraft thermal mod...
The correlation of the thermalmathematical models (TMMs) of spacecrafts with the results of the ther...
Temperatures predicted by the Thermal Mathematical Models (TMMs) used in the thermal control design ...
Model-to-test correlation is a frequent problem in spacecraft-thermal control design. The goal of co...
Thermal mathematical models are the main tool an engineer has to optimize the thermal design of a sp...
Model-to-test correlation is a frequent problem in spacecraft-thermal control design. The idea is to...
Spacecraft thermal model validation is normally performed by comparing model predictions with therma...
A software-based thermal modeling process was documented for generating the thermal panel settings n...
This thesis describes the development and correlation of a thermal model that forms the foundation ...
This thesis describes the development and correlation of a thermal model that forms the foundation o...
The correlation of the Thermal Mathematical Models is often performed manually, and the results obta...
This paper presents a mathematically rigorous, subspace projection-based reduced order modeling (ROM...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010.Ca...
The design of the thermal control system of space vehicles, needed to maintain the equipment compone...
Genetic algorithms have been used for matching temperature values generated using thermal mathematic...
There are always differences between the computer predicted temperatures of a spacecraft thermal mod...
The correlation of the thermalmathematical models (TMMs) of spacecrafts with the results of the ther...
Temperatures predicted by the Thermal Mathematical Models (TMMs) used in the thermal control design ...
Model-to-test correlation is a frequent problem in spacecraft-thermal control design. The goal of co...
Thermal mathematical models are the main tool an engineer has to optimize the thermal design of a sp...
Model-to-test correlation is a frequent problem in spacecraft-thermal control design. The idea is to...
Spacecraft thermal model validation is normally performed by comparing model predictions with therma...
A software-based thermal modeling process was documented for generating the thermal panel settings n...
This thesis describes the development and correlation of a thermal model that forms the foundation ...
This thesis describes the development and correlation of a thermal model that forms the foundation o...
The correlation of the Thermal Mathematical Models is often performed manually, and the results obta...
This paper presents a mathematically rigorous, subspace projection-based reduced order modeling (ROM...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010.Ca...