Obstruction detection and warning system and method
An obstruction detection and warning system includes a plurality of edge light emitters, and a processing system. The edge light emitters are mounted on a structure that has a width and a height. Each edge light emitter is operable to emit a light beam at an angular rate, and that is encoded with data that indicates its position and its height. The processing system receives the light beam emitted from each edge light emitter and decodes the encoded data from the received light beam to determine the width and height of the structure, and to determine a distance from an aircraft to the structure. The processor also compares an active trajectory and current altitude of the aircraft to the width and height of the structure and the distance to the structure and, based on the comparison, generates and supplies situational cues to an operator of the aircraft.
1. An obstruction detection and warning system, comprising:
a plurality of edge light emitters mounted on a structure, the structure having a width and a height, each edge light emitter mounted on the structure at a position relative to a reference position and at a height above ground level, each edge light emitter operable to emit a light beam at an angular rate, the light beam encoded with data that indicates its position and its height;
a processing system for receiving the light beam emitted from each edge light emitter and operable, upon receipt of the light beam emitted from each edge light emitter, to:
decode the encoded data from the received light beam to determine the width and height of the structure, and to determine a distance from an aircraft to the structure,
compare an active trajectory and current altitude of the aircraft to the width and height of the structure and the distance to the structure, and
based on the comparison, generate and supply situational cues to an operator of the aircraft.
2. The system of claim 1 , wherein the processing system comprises:
a decoder operable to decode the encoded data from the received light beam; and
a receiver operable to receive the light beam emitted from each light emitter and supply the received light beam to the decoder.
3. The system of claim 1 , further comprising:
a display device in operable communication with the processing system and configured, in response to commands, to render one or more images,
wherein the processing system is further operable supply commands to the display device that cause the display device to render one or more images of the situational cues.
4. The system of claim 1 , wherein the processing system implements autocorrelation to determine the width and height of the structure and the distance to the structure.
5. The system of claim 1 , wherein at least a portion of the processing system is disposed in the aircraft.
6. The system of claim 1 , wherein at least a portion of the processing system is disposed remote from the aircraft.
7. The system of claim 1 , further comprising:
an avionics system in operable communication with the processing system and operable to supply the active trajectory and current altitude of the aircraft to the processing system.
8. The system of claim 7 , wherein the avionics system comprises a flight management system.
9. The system of claim 1 , wherein each edge light emitter comprises:
a plurality of light emitting diodes (LEDs); and
a microcontroller coupled to the LEDs and configured to drive each of the LEDs in a manner that causes the edge light emitter to emit the light beam.
10. A method of providing obstruction detection and warning, the method comprising the steps of:
emitting a light beam, at an angular rate, from each of a plurality of edge light emitters, each edge light emitter mounted on a structure that has a width and a height, each edge light emitter mounted on the structure at a position relative to a reference position and at a height above ground level, the light beam emitted from each edge light emitter encoded with data that indicates its position and its height;
receiving, in a processing system, the light beam emitted from each edge light emitter;
decoding, in the processing system, the encoded data from the received light beam to determine the width and height of the structure, and to determine a distance from an aircraft to the structure;
compare, in the processing system, an active trajectory and current altitude of the aircraft to the width and height of the structure and the distance to the structure; and
based on the comparison, generating and supplying, via the processing system, situational cues to an operator of the aircraft.
11. The method of claim 10 , wherein the step of decoding comprises using a decoder to decode the encoded data from the received light beam.
12. The method of claim 10 , further comprising:
commanding, using the processing system, a display device render one or more images of the situational cues.
13. The method of claim 10 , wherein the processing system implements autocorrelation to determine the width and height of the structure and the distance to the structure.
14. The method of claim 10 , wherein at least a portion of the processing system is disposed in the aircraft.
15. The method of claim 10 , wherein at least a portion of the processing system is disposed remote from the aircraft.
16. The method of claim 10 , further comprising:
using an avionics system to supply the active trajectory and current altitude of the aircraft to the processing system.
17. An obstruction detection and warning system, comprising:
a plurality of edge light emitters mounted on a structure, the structure having a width and a height, each edge light emitter mounted on the structure at a position relative to a reference position and at a height above ground level, each edge light emitter operable to emit a light beam at an angular rate, the light beam encoded with data that indicates its position and its height;
a display device responsive to commands to render one or more images; and
a processing system in operable communication with the display device and configured to receive the light beam emitted from each edge light emitter, the processing system operable, upon receipt of the light beam emitted from each edge light emitter, to:
decode the encoded data from the received light beam to determine the width and height of the structure, and to determine a distance from an aircraft to the structure,
compare an active trajectory and current altitude of the aircraft to the width and height of the structure and the distance to the structure,
based on the comparison, generate situational cues for use by an operator of the aircraft, and
supply commands to the display device that cause the display device to render one or more images of the situational cues.
18. The system of claim 17 , wherein the processing system comprises:
a decoder operable to decode the encoded data from the received light beam; and
a receiver operable to receive the light beam emitted from each light emitter and supply the received light beam to the decoder.
19. The system of claim 17 , wherein the processing system implements autocorrelation to determine the width and height of the structure and the distance to the structure.
20. The system of claim 17 , wherein each edge light emitter comprises:
a plurality of light emitting diodes (LEDs); and
a microcontroller coupled to the LEDs and configured to drive each of the LEDs in a manner that causes the edge light emitter to emit the light beam.