Real-time aircraft status detection system and method

A low power method for determining whether a cargo destined for air transport is in a flying state having the steps of: providing a housing for attachment to a cargo the housing having: an accelerometer for detecting a linear acceleration, a gyroscope for detecting an angular rate, a controller measuring a linear acceleration with the accelerometer, measuring an angular rate with the gyroscope, providing the measured linear acceleration and angular rate to the controller, and generating a flight status output signal indicating whether the housing is in a flying state as a function of the linear acceleration signal and angular rate signal.