Patent ID: 11867529
Assignee: RUMFERT, LLC
Field: Measurement (Instruments)
Classification: CPC G  B | IPC B  G

Claim 16:
17. The processor module computer instruction code implemented system of claim 16 wherein the first computer instruction code set when executed by the AWSS first processor module initializing the AWSS further implementing the steps of determining a pressure altitude correction factor from the initialization parameters and an initial reading of raw UAS pressure altitude while the UAS is on the ground and wherein the UAS corrected pressure altitude is determined based on application of the pressure altitude correction factor to the raw sensed pressure altitude and further wherein the AWSS comprises a secondary (monitor) sources and wherein the step of monitoring the UAS primary sensor pressure altitude to determine the need for a reset, includes the step of validating changes in UAS corrected pressure altitude with corresponding changes in the secondary (monitor) source.