Collision-avoidance system for ground crew using sensors
First Claim
1. A ground obstacle collision-avoidance system comprising:
- a plurality of radar sensor modules each located at a selected different location on an exterior of an installation aircraft, wherein each radar sensor module comprises;
a radar emitter configured to emit a radar signal; and
a radar detector configured to receive a radar return signal associated with reflections of the emitted radar signal that are reflected from the ground obstacle,wherein the radar sensor module is configured to communicate radar information corresponding to the detected radar return signal;
a processing system configured to determine a distance from the installation aircraft to a detected ground obstacle that has been detected by at least one of the plurality of radar sensor modules, determine a type of the detected ground obstacle, and generate a plan view indicating at least one aircraft icon, a graphical ground obstacle icon that is associated with the detected ground obstacle, and text indicating the distance from the installation aircraft to the detected ground obstacle; and
a display configured to present the plan view,wherein a presentation location of the aircraft icon on the plan view provides a relative reference point for the installation aircraft,wherein a presentation location of the graphical ground obstacle icon relative to the at least one aircraft icon indicates a location of the detected ground obstacle relative to the installation aircraft, andwherein a shape of the graphical ground obstacle icon indicates the type of the detected ground obstacle.
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Accused Products
Abstract
A ground obstacle collision-avoidance system includes a plurality of radar sensor modules that each receive at a radar detector radar return signals corresponding to reflections of the emitted signal from a ground obstacle, and transmits radar information associated with the received radar signal reflections reflected from the ground obstacle, wherein each of the plurality of radar sensor modules are uniquely located on a surface of an aircraft that is at risk for collision with a ground obstacle if the aircraft is moving; a gateway unit that receives the radar information transmitted from the radar sensor module and transmits information associated with the received radar information; a processing system configured to determine a distance from the installation aircraft to a detected ground object detected; and a display configured to present a plan view indicating an aircraft icon and a graphical ground obstacle icon that is associated with the detected ground obstacle.
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Citations
20 Claims
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1. A ground obstacle collision-avoidance system comprising:
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a plurality of radar sensor modules each located at a selected different location on an exterior of an installation aircraft, wherein each radar sensor module comprises; a radar emitter configured to emit a radar signal; and a radar detector configured to receive a radar return signal associated with reflections of the emitted radar signal that are reflected from the ground obstacle, wherein the radar sensor module is configured to communicate radar information corresponding to the detected radar return signal; a processing system configured to determine a distance from the installation aircraft to a detected ground obstacle that has been detected by at least one of the plurality of radar sensor modules, determine a type of the detected ground obstacle, and generate a plan view indicating at least one aircraft icon, a graphical ground obstacle icon that is associated with the detected ground obstacle, and text indicating the distance from the installation aircraft to the detected ground obstacle; and a display configured to present the plan view, wherein a presentation location of the aircraft icon on the plan view provides a relative reference point for the installation aircraft, wherein a presentation location of the graphical ground obstacle icon relative to the at least one aircraft icon indicates a location of the detected ground obstacle relative to the installation aircraft, and wherein a shape of the graphical ground obstacle icon indicates the type of the detected ground obstacle. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 16, 19)
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13. A method comprising:
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at each of a plurality of radar sensor modules, emitting, from a radar emitter, a radar signal; receiving, at a radar detector, radar return signals corresponding to reflections of the emitted radar signal from a ground obstacle; and transmitting radar information associated with the received radar return signal reflections reflected from the ground obstacle, wherein each of the plurality of radar sensor modules are uniquely located on a surface of an aircraft that is at risk for collision with the ground obstacle while the aircraft is being towed; at a gateway unit, receiving the radar information transmitted from the radar sensor module; and transmitting information associated with the received radar information, and at a processing system, determining a distance from the installation aircraft to a detected ground obstacle detected by at least one of the plurality of radar sensor modules; and determining a type of the detected ground obstacle; on a display, presenting a plan view indicating at least one aircraft icon, a graphical ground obstacle icon that is associated with the detected ground obstacle, and text indicating the distance from the installation aircraft to the detected ground obstacle, wherein a presentation location of the aircraft icon on the plan view provides a relative reference point for the installation aircraft, wherein a presentation location of the graphical ground obstacle icon relative to the at least one aircraft icon indicates a location of the detected ground obstacle relative to the installation aircraft, and wherein a shape of the graphical ground obstacle icon indicates the type of the detected ground obstacle. - View Dependent Claims (14, 15, 17, 20)
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18. A ground obstacle collision-avoidance system comprising:
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a plurality of radar sensor modules each located at a selected different location on an exterior of an installation aircraft, wherein each radar sensor module comprises; a radar emitter configured to emit a radar signal; and a radar detector configured to receive a radar return signal associated with reflections of the emitted radar signal that are reflected from the ground obstacle, wherein the radar sensor module is configured to communicate radar information corresponding to the detected radar return signal; a processing system configured to determine a first distance from the installation aircraft to a detected ground obstacle that has been detected by at least one of the plurality of radar sensor modules, the first distance being a distance that the detected ground obstacle is behind the installation aircraft, determine a second distance from the installation aircraft to the detected obstacle, the second distance being a distance of the detected ground obstacle to a side of the installation aircraft, and generate a plan view indicating at least one aircraft icon, a graphical ground obstacle icon that is associated with the detected ground obstacle, first text indicating the first distance, and second text indicating the second distance; and a display configured to present the plan view, wherein a presentation location of the aircraft icon on the plan view provides a relative reference point for the installation aircraft, and wherein a presentation location of the graphical ground obstacle icon relative to the at least one aircraft icon indicates a location of the detected ground obstacle relative to the installation aircraft.
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Specification