Laser beacon and optical detector system for aircraft collision hazard determination

• US 4,277,170 A
• Filed: 11/01/1979
• Issued: 07/07/1981
• Est. Priority Date: 11/01/1979
• Status: Expired due to Term

• Current Assignee: Richard B. Miles
• Original Assignee: Richard B. Miles
• Inventors: Miles, Richard B.
• Primary Examiner(s): Buczinski, S. C.
• Application Number:
  US06/090,497
• Time in Patent Office: 614 Days
• Field of Search: 356/1, 356/4, 356/152, 343/100 PE, 343/106 R, 343/112 CA, 340/25, 340/27 NA, 350/96.25, 350/96.18
• US Class Current: 356/141.3
• CPC Class Codes: G01S 3/782 Systems for determining direction or deviation from predetermined direction

Abstract

A laser beacon mounted on a first aircraft emits a beam which is sensed by an optical detector on a second aircraft in such a manner that a collision proximity warning device is triggered and/or collision avoidance maneuvers are initiated. The system is intended to prevent aircraft collisions which occur under visual flight regulation (VFR) conditions and which constitute in excess of 90% of civil aircraft mid-air accidents. In the preferred embodiment a horizontally collimated, vertically diverging laser beam is made to rotate 360° in polarization while simultaneously rotating 360° in azimuth with respect to the first aircraft. The optical detector mounted on the second aircraft preferably comprises a pair of horizontally offset light collectors which include narrow spectral width filters respectively and various other components which collectively determine the bearing, range and relative heading of the first aircraft. The information is stored so that subsequent signals arising from the first aircraft may be compared to determine trajectories and range rates. Collision warning and/or collision avoidance actions may then be started if the information indicates a high probability of collision. Alternative embodiments of the optical detector apparatus can be constructed with varying complexities to meet the needs of aircraft operating at different speeds or in different flight environments.

Claims

1. An aircraft collision hazard determination system comprising:

laser beacon means mountable on a first aircraft including a laser light source which emits a polarized beam of light, expanding means for optically expanding said beam into a vertically diverging and horizontally collimated fan-shaped beam, means for sweeping said fan-shaped beam 360°

in azimuth while simultaneously rotating said beam 360°

in polarization; and

,

a pair of optical detection means mountable on a second aircraft for detecting light from said laser beacon means including means for detecting different polarized components of the light and converting said components into electronic signals proportional thereto, means for electronically processing said polarized components to produce a signal indicative of the polarization of the light, and means for comparing the detected polarization from each of said optical detection means to verify the consistency of the polarization of the light thereby reducing false signals.

2. An aircraft collision hazard determination system comprising:

laser beacon means mountable on a first aircraft including a laser light source, a laser beam expander and collimator means for producing a beam which diverges vertically but remains horizontally collimated with substantially no divergence over the range of the system, and means for sweeping said vertically diverging and horizontally collimated beam 360°

in azimuth; and

an optical detection means mountable on a second aircraft including light sensitive detector means for converting the light from said beacon means into an electronic signal, electronic means for measuring the pulse shape characteristic as a function of time of said electronic signal, and logic means for converting said pulse shape characteristic as a function of time into a signal indicative of the distance of said laser beacon means from said optical detection means.

3. The system of claim 2 wherein said optical detection means further includes a narrow width spectral filter means actively locked to the frequency of said laser beacon means.

4. An aircraft collision hazard determination system comprising:

optical beacon means mountable on a first aircraft including a light source which emits a polarized beam of light, expanding means for optically expanding said beam into a vertically diverging and horizontally collimated fan-shaped beam, means for sweeping said fan-shaped beam 360°

in azimuth while simultaneously rotating said fan-shaped beam 360°

in polarization; and

,

optical detection means mountable on a second aircraft for detecting light from said optical beacon means including means for detecting different polarized components of said light and converting them into electronic signals, means for electronically processing the electronic signals indicative of said polarized components to produce a signal indicative of the polarization of said light, and logic means for converting the signal indicative of the polarization into information indicative of the bearing of said second aircraft from said first aircraft.

5. A method for detecting range comprising the steps of:

producing a laser beam;

expanding said laser beam into a beam which remains horizontally collimated with substantially no divergence over its desired range;

producing a beacon by sweeping said beam 360°

in azimuth;

collecting the observed pulse of light from said beacon;

converting the light pulse into an electronic signal;

determining the pulse shape characteristic as a function of time of said electronic signal; and

,

converting said pulse shape characteristic as a function of time into a range measurement.

6. A method for detecting bearing from a beacon comprising the steps of:

producing a polarized light beam;

producing a beacon by sweeping said light beam 360°

in azimuth while simultaneously rotating it 360°

in polarization;

collecting the observed pulse of light from said beacon;

detecting at least two different polarization components of the light; and

,

converting the polarization components into a signal indicative of the bearing from said beacon.

7. An optical beacon and detection system comprising:

laser beacon means including a laser light source for producing a laser beam, means for expanding and collimating the laser beam emitted from said laser light source such that said beam remains collimated with substantially no divergence over the range of the system, and means for sweeping said collimated beam 360°

in azimuth; and

,

optical detection means for observing light from said laser beacon means including light sensitive detector means for converting the observed pulse of light from said beacon means into an electronic signal;

electronic means for measuring the pulse shape characteristic as a function of time of said electronic signal, and logic means for converting said pulse shape characteristic as a function of time into a signal indicative of the distance of said laser beacon means from said optical detection means.

8. An optical beacon and detection system comprising:

beacon means including a light source which emits a polarized beam of light, means for sweeping said beam 360°

in azimuth while simultaneously rotating said beam 360°

in polarization; and

optical detection means including means for detecting at least two different polarized components of the light from said beam, means for electronically processing the detected polarized components to produce polarization information indicative of the polarization of the detected light, and means for converting said polarization information into a signal indicative of the bearing of said optical detection means from said beacon means.