Determination Method of the Aircrafts Flying Height Using Absolute Pressure Sensors

The method of measurement of height of the aircraft by means of several sensors of pressure is developed. Influence of arrangement of sensors on the aircraft on an error of measurements of height is established. The intelligent sensor of absolute pressure is developed. The method for compensation of the errors when determining height with absolute pressure sensor caused by various aerodynamic and atmospheric phenomena is offered. Experimental measurement of height of the aircraft by means of the developed methods and sensors in field conditions is taken. Measurement errors are defined.