A study is presented on the design and testing of spacecraft power systems using the virtual test bed (VTB). The interdisciplinary components such as solar array and battery systems were first modeled in native VTB format and validated by experiment data. The shunt regulator and battery charge controller were designed in Simulink according to the system requirements and imported to VTB. Two spacecraft power systems were then designed and tested together with the control systems.
Design and testing of spacecraft power systems using VTB
IEEE Transactions on Aerospace and Electronic Systems ; 39 , 3 ; 976-989
2003-07-01
2032132 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Design and Testing of Spacecraft Power Systems Using VTB
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