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Lidar system producing multiple scan paths and method of making and using same

  • US 9,244,272 B2
  • Filed: 03/12/2013
  • Issued: 01/26/2016
  • Est. Priority Date: 03/12/2013
  • Status: Active Grant
First Claim
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1. A ranging system comprising:

  • an aircraft;

    a light detection and ranging (LiDAR) scanning system carried by the aircraft, comprising;

    a housing;

    a light source within the housing adapted to transmit light;

    a light deflection system within the housing comprising;

    a light deflection element rotatably supported within the housing and having a first end and a second end, the light deflection element rotatable and balanced about an axis extending from the first end to the second end, the light deflection element further having at least three sides extending between the first end and the second end, at least a first side of the at least three sides has a first reflective surface at a first angle in relation to the axis, and at least a second side of the at least three sides has a second reflective surface at a second angle in relation to the axis, with the first angle being different from the second angle, the light deflection element being rotatable about the axis such that light is deflectable from the first and second reflective surfaces of the first and second sides;

    wherein upon actuation of the light source and rotation of the light deflection element, the LiDAR scanning system forms at least a first scan path and a second scan path; and

    a receiver within the housing adapted to receive the light after reflection from the scan paths; and

    a computer having computer instructions adapted to determine and store distance from a calculated time of travel of the light from the light source to an object to be scanned in the scan paths and back to the receiver;

    wherein the first scan path is at a first angle in relation to the LiDAR scanning system and the second scan path is at a second angle in relation to the LiDAR scanning system, where the first angle is nadir relative to the aircraft and the second angle is oblique relative to the first angle.

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