Patent ID: 9383381
Filing Date: 2016-07-05
CPC Classification: G01C,G01P

Claim Text:
1. An airspeed calculation system for determining the airspeed of an aircraft, comprising: a static pressure device configured to determine a static pressure acting on the aircraft; a global positioning system device configured to determine an inertial position of the aircraft; an inertial measurement unit device configured to determine inertial measurements of the aircraft; an angle of attack device configured to determine an angle of attack of the aircraft; a total pressure sensor configured to determine a total pressure that the aircraft experiences while the aircraft is moving; a total air temperature sensor configured to determine a total air temperature that the aircraft experiences while the aircraft is moving; at least one processor in electronic communication with the static pressure device, the global positioning system device, the inertial measurement unit device, the angle of attack device, the total pressure sensor, and the total air temperature sensor; and a memory in electronic communication with the at least one processor, wherein the memory comprises programming code for execution by the at least one processor, and the programming code is configured to: