APPARATUS AND METHOD FOR ADJUSTING SET CLEARANCE ALTITUDE IN A TERRAIN FOLLOWING RADAR SYSTEM

Abstract

An apparatus and method for adjusting set clearance altitude of an aircraft to control the aircraft to fly along a predetermined path relative to the terrain below. A terrain following radar system and a stored terrain elevation data base are used to determine the respective positions and elevations of selected portions of the terrain downrange from the aircraft. This information is used along with pre-stored information relating to the ability of a ground threat to detect the aircraft and the roughness of the terrain to compute three different altitudes. The first altitude (Ia) represents the maximum height at which the aircraft can fly without being detected by the ground threat. The second altitude (Da) represents the maximum desired altitude of the aircraft at any time during a flight. The third altitude (Ra) represents the minimum altitude at which the aircraft is allowed to fly. The set clearance altitude is determined for each of the selected positions on the terrain by first comparing Ia and Da and taking the lesser altitude as between the two. The lesser altitude is then compared with Ra and the greater of those two values is selected as the set clearance altitude. Set clearance altitude is one of the variables used to determine the desired vertical flight vector angle of the aircraft to control the aircraft to fly along a path corresponding to the respective set clearance altitudes above the terrain.

Source: Google Patents

35 USC §181 Secrecy Order

Inventor

• 1GEORGE M. BARNEY

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