Abstract:The number of spacecraft which implement feedback control systems to wrap up stringent thermal requirements is continuously growing. The GOCE and HERSCHEL scientific satellites and the GALILEO navigation satellite system are just some examples of this application. For the design and verification of the active thermal control systems (TCS), both thermal and control design software must be run and mathematical models need to be exchanged over these two domains. Both types of software are commercially available a… Show more
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