초록 ▼

The aircraft is provided with an infrared sensor which is adjustable by means of feedback control so that its line of sight (image center) is and remains in line with the middle one of three infrared fires at and near the end of the runway. The craft is now maneuvered in such a way that its longitud

The aircraft is provided with an infrared sensor which is adjustable by means of feedback control so that its line of sight (image center) is and remains in line with the middle one of three infrared fires at and near the end of the runway. The craft is now maneuvered in such a way that its longitudinal axis is aligned with the horizontal component of the line of sight. After a particular distance has been reached, the aircraft descends while the image of the middle fire remains centered. The system uses existing equipment and is further supplemented to correct an initial gross deviation from the desired approach path.

대표청구항 ▼

1. Method of automatically landing an aircraft, comprising the steps of providing a plurality of infrared fires at a particular distance from each other, one fire being centrally located at the end of a runway; detecting, on board of the aircraft, images of the fires, under utilization of an inf

1. Method of automatically landing an aircraft, comprising the steps of providing a plurality of infrared fires at a particular distance from each other, one fire being centrally located at the end of a runway; detecting, on board of the aircraft, images of the fires, under utilization of an infrared sensor; reorienting the detecting sensor by means of automatic tracking so that an image of the centrally located fires has a central disposition with respect to and in an image frame; automatically determining angular deviation of the reoriented sensor from the direction of flight of the aircraft in a horizontal plane; and automatically maneuvering the aircraft on the basis of said determining step so that the aircraft approaches the said centrally located fire while maintaining the sensor oriented as having resulted from the reorienting step. 2. Method as in claim 1, the detecting step including, orienting the infrared sensor at a particular angle and in a particular direction; and searching for absence or presence of said images in its field of view. 3. Method as in claim 1 or 2, including the step of selecting a particular intensity level and/or a particular distance value in the images of the fires as a criterion for identifying them as images of said fires. 4. Method as in claim 1 and including the step of initiating descent after said aircraft has been maneuvered toward said centrally located fire. 5. Method as in claim 1, wherein said fires are turned on when the aircraft has a particular distance from them. 6. Apparatus for automatically landing an unmanned aircraft, comprising: an infrared image sensor, adjustably disposed in said aircraft; first loop means including the sensor for orienting the sensor and stabilizing its orientation to point toward a particular ground target point; second loop means being slaved to said first loop means for maneuvering the aircraft toward said target point; and means for causing said aircraft to descend toward said target point. 7. A system for automatically landing an unmanned aircraft, comprising: a plurality of infrared fires disposed on the ground in particular relation to a runway; an infrared sensor in the aircraft and being disposed for adjustable orientation; means connected to said sensor for being responsive to images of said fires and further connected to adjust said sensor so that its line of sight is particularly oriented to said fires, resulting in a possible angular deviation of a horizontal component of said line of sight to a longitudinal axis of the aircraft; and means for controlling the aircraft so that said angular deviation is reduced to zero, said means connected to the sensor maintaining said line of sight particularly oriented to said fires as the aircraft is controlled toward said zero deviation.