Aerial system and vehicle for continuous operation
First Claim
1. An aerial vehicle having a vision-based navigation system for capturing an arresting cable situated at a landing site, the aerial vehicle comprising:
- a fuselage having a propulsion system;
an arresting device coupled to the fuselage, the arresting device to capture said arresting cable at the landing site;
a camera situated on the aerial vehicle;
an infrared illuminator situated on the aerial vehicle to illuminate the landing site, wherein said arresting cable has two infrared reflectors situated on said arresting cable; and
an onboard processor to (i) generate a plurality of coordinates representing features of the landing site using an image thresholding technique, (ii) eliminate one or more coordinates as outlier coordinates using linear correlation, (iii) identify two of the plurality of coordinates as associated with the two infrared reflectors using a Kalman filter, and (iv) navigate the aerial vehicle toward said two of the plurality of coordinates associated with the two infrared reflectors to enable the aerial vehicle to capture said arresting cable situated at the landing site.
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Accused Products
Abstract
An aerial vehicle having a vision based navigation system for capturing an arresting cable situated at a landing site may comprise a fuselage having a propulsion system; an arresting device coupled to the fuselage, the arresting device to capture the arresting cable at the landing site; a camera situated on the aerial vehicle; an infrared illuminator situated on the aerial vehicle to illuminate the landing site, wherein the arresting cable has two infrared reflectors situated thereon; and an onboard vision processor. The onboard vision processor may (i) generate a plurality of coordinates representing features of the landing site using an image thresholding technique, (ii) eliminate one or more coordinates as outlier coordinates using linear correlation, and (iii) identify two of the plurality of coordinates as the two infrared reflectors using a Kalman filter.
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Citations
20 Claims
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1. An aerial vehicle having a vision-based navigation system for capturing an arresting cable situated at a landing site, the aerial vehicle comprising:
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a fuselage having a propulsion system; an arresting device coupled to the fuselage, the arresting device to capture said arresting cable at the landing site; a camera situated on the aerial vehicle; an infrared illuminator situated on the aerial vehicle to illuminate the landing site, wherein said arresting cable has two infrared reflectors situated on said arresting cable; and an onboard processor to (i) generate a plurality of coordinates representing features of the landing site using an image thresholding technique, (ii) eliminate one or more coordinates as outlier coordinates using linear correlation, (iii) identify two of the plurality of coordinates as associated with the two infrared reflectors using a Kalman filter, and (iv) navigate the aerial vehicle toward said two of the plurality of coordinates associated with the two infrared reflectors to enable the aerial vehicle to capture said arresting cable situated at the landing site. - View Dependent Claims (2, 3)
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4. A vision-based navigation system for installation on an aerial vehicle, the vision-based navigation system comprising:
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a camera; an illuminator situated on the aerial vehicle to illuminate a landing site, wherein the landing site comprises an arresting cable with two reflectors situated on the arresting cable; an onboard processor to identify a perching point at the landing site, wherein the onboard processor identifies the perching point by (i) generating a plurality of coordinates representing features of the landing site using an image thresholding technique, (ii) identifying among said plurality of coordinates a coordinate associated with each of said two reflectors, and (iii) navigate the aerial vehicle toward the identified coordinates associated with each of said two infrared reflectors to enable the aerial vehicle to capture the arresting cable situated at the landing site. - View Dependent Claims (5, 6, 7, 8, 9, 10, 11)
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12. An aerial vehicle for autonomous landing, the aerial vehicle comprising:
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a fuselage; a camera; an illuminator situated on the aerial vehicle to illuminate two reflectors situated at a landing site; and an onboard processor to identify a perching point at the landing site, wherein the onboard processor identifies the perching point by (i) generating a plurality of coordinates representing features of the landing site using an image thresholding technique, (ii) identifying among said plurality of coordinates a coordinate associated with each of said two reflectors, and (iii) navigate the aerial vehicle toward the identified coordinates associated with each of said two infrared reflectors to enable the aerial vehicle to land at the perching point autonomously. - View Dependent Claims (13, 14, 15, 16, 17, 18, 19, 20)
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Specification