A method of correcting the aircraft vertically integrated standby instrument system

摘要

A method for correcting vertical aircraft defined integrated standby instrument system, which includes angular velocity sensors, accelerometers, the sensor is full air pressure, comprising using information from the accelerometers and angular rate sensors, characterized in that the correction of the vertical performed not on the apparent vertical, indications determined by the accelerometers, and by means of information processing using a Kalman filter of the true air speed of an aircraft arat determined by indications of full air pressure sensor and the speed determined by the accelerometers readings.