Several boost-derived topologies are analyzed and compared for an aerospace application that uses a 100 V voltage bus. All these topologies have been designed and optimized considering the electrical requirements and the reduced number of space-qualified components. The comparison evaluates the power losses, mass, and dynamic response. Special attention has been paid to those topologies that may cancel the inherent right half plane zero (RHP) zero of the boost topology. Experimental results of the less common topologies are presented.
Comparison of Boost-Based MPPT Topologies for Space Applications
IEEE Transactions on Aerospace and Electronic Systems ; 49 , 2 ; 1091-1107
2013-04-01
11594477 byte
Article (Journal)
Electronic Resource
English
Boost-Based MPPT Converter Topology Trade-Off for Space Applications
British Library Conference Proceedings | 2008
|Boost-Based MPPT for the MTM PCDU of the BepiColombo Mission
British Library Conference Proceedings | 2008
|