Optical system for detecting and displaying aircraft position and environment during landing and takeoff
First Claim
1. A method for detecting a position of an aircraft comprising:
- transmitting light beams;
receiving reflected or backscattered light beams resulting from the transmitting;
measuring differences between the transmitted and received light beams; and
determining parameters based on the measuring to determine the position of the aircraft;
wherein at least one of the transmitted or received light beams, or both, travel through one or more optical fibers.
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Accused Products
Abstract
A system and method uses light signals to detect and display the position of an airborne vehicle, such as a helicopter, during takeoff or landing or low speed, low altitude operation. A transmitter on the vehicle emits light signals while an optical receiver retrieves reflected light signals. Using light detection and ranging techniques, various parameters, such as altitude, ground speed and relative wind, are calculated based on the Doppler shift within the reflected light signals. The signals are transmitted in three different directions to facilitate the measurements of different Doppler shifts. The parameters are also displayed on a screen or other visual device within the vehicle.
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Citations
22 Claims
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1. A method for detecting a position of an aircraft comprising:
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transmitting light beams; receiving reflected or backscattered light beams resulting from the transmitting; measuring differences between the transmitted and received light beams; and determining parameters based on the measuring to determine the position of the aircraft; wherein at least one of the transmitted or received light beams, or both, travel through one or more optical fibers. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A method comprising:
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receiving at an aircraft reflected or backscattered light beams based on light beams transmitted from the aircraft, such that at least one of the transmitted or received light beams, or both, travel through one or more optical fibers; measuring differences between the transmitted and received light beams; determining parameters relating to a position of the aircraft according to the measured differences; and displaying the parameters in the aircraft. - View Dependent Claims (12, 13, 14, 15, 16)
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17. A system for detecting position of an aircraft comprising:
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a transmitter configured to transmit a light beam from the aircraft; an optical receiver configured to receive reflected or backscattered light beams; and a measuring device configured to compare the transmitted and received beams and to calculate parameters with respect to the position of the object, wherein at least one of the transmitter and the optical receiver comprises an optical fiber configured to guide the transmitted or received light beams, or both. - View Dependent Claims (18, 19, 20, 21, 22)
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Specification