Abstract: A system and method for a hybrid development platform for project development that integrates local and continuous integration (CI)-based building and testing. The system and method can make use of a build cluster, that executes individual commands within build targets; a build cache that stores partial results of previous executions; an artifact and image storage system, that stores and updates artifacts and container images; and a secrets repository that manages local and global project secrets. The system and method function as an automated build platform that enables an execution environment agnostic build platform for development over local development and extended network computing environments.

Abstract: An aircraft cargo locating system determines the location and weight of aircraft cargo placed in unit loading devices. A wireless tag, such as an Radio Frequency Identification (RFID) tag is affixed to each of the loading devices. The system receives information from the tags, and from the information calculates the location of the loading devices and the weight of the loading devices. The system is able to calculate weight and balance parameters to assist in the loading process.

Abstract: A cargo loading logistics system for verifying cargo loaded on an aircraft receives a desired restraint configuration from a database and determines an actual restraint configuration on the aircraft by receiving data from a plurality of machine readable identifiers corresponding to a plurality of install points and data from a plurality of machine readable identifiers corresponding to a plurality of restraints. The cargo loading logistics system then compares the desired restraint configuration with the actual restraint configuration and determines if the aircraft is properly configured to be loaded for an upcoming flight.

Abstract: A cargo loading logistics system for verifying cargo loaded on an aircraft receives a desired restraint configuration from a database and determines an actual restraint configuration on the aircraft by receiving data from a plurality of machine readable identifiers corresponding to a plurality of install points and data from a plurality of machine readable identifiers corresponding to a plurality of restraints. The cargo loading logistics system then compares the desired restraint configuration with the actual restraint configuration and determines if the aircraft is properly configured to be loaded for an upcoming flight.

Abstract: A test device to determine the operational behavior of a memory module socket may include a connector configured to mate with a memory module socket, a signal detection circuit to detect a power characteristic of a first signal, and an edge detection circuit to detect a transition of a second signal. The test device may provide continuity verification for signals passing through the memory module socket. In another implementation, the test device may include a connector, a signal capture circuit to detect and digitally sample a signal, and a memory to store a value representative of the sampled signal. This device may use a digital signal processor (as the signal capture circuit) to analyze the sampled signal. Test devices may also include an indicator circuit to indicate operation of the signal detection, edge detection, or signal capture circuits.