Abstract: Systems for exchanging information between a cargo handling system of an aircraft and a Power Drive Unit (PDU) are described herein. The systems include a power source provided within the aircraft and a first PDU provided within the aircraft. The power source is capable of providing DC power to the at least one PDU via an electrical power line. The power source further including a first Power Line Communication (PLC) node and the PDU further including a second Power Line Communication (PLC) node. The first PLC node being capable of communicating with the second PLC node via the electrical power line.

Abstract: Methods of determining fluid density within a tank, such as an aircraft tank are include installing one or more clusters of sensors each cluster comprising a plurality of sensors including at least one pressure sensor. A minimum of two pressure measurements are required for density estimation. The fluid density between different clusters may be determined from pressure measurements obtained by each cluster and the distance between the clusters. Furthermore, the distribution of density throughout the tank may be determined by employing clusters including two or more pressure sensors.

Abstract: Systems for exchanging information between a cargo handling system of an aircraft and a Power Drive Unit (PDU) are described herein. The systems include a power source provided within the aircraft and a first PDU provided within the aircraft. The power source is capable of providing DC power to the at least one PDU via an electrical power line. The power source further including a first Power Line Communication (PLC) node and the PDU further including a second Power Line Communication (PLC) node. The first PLC node being capable of communicating with the second PLC node via the electrical power line.