Abstract: Example implementations associated with the aspects of the present invention include a low altitude aircraft identification system composed by three components: a small aircraft electronic identification box with an embedded logger, a ground identification equipment to automatically identify the aircraft just pointing at it, and an identification code database. The identification code can be transmitted by a visible light color sequence or by a radio frequency signal. The ground identification device is capable of recognizing both kinds of code.
Type:
Grant
Filed:
December 10, 2018
Date of Patent:
July 14, 2020
Assignee:
Airspace Systems, Inc.
Inventors:
Aislan Gomide Foina, Guy Bar-Nahum, Jasminder Singh Banga
Abstract: A system for arresting and capturing airborne targets comprising: a projectile comprising an airframe which houses a means for entanglement, a means for propulsion, and a means for producing drag, wherein the means for entanglement is tethered to the airframe, a launcher capable of launching the projectile to within a close distance of an airborne target, wherein as the projectile approaches the airborne target the projectile is first slowed down by the means for producing drag, and second, as the projectile slows down the means for propulsion causes the means for entanglement to be projected towards the airborne target, wherein the means for entanglement arrests and captures the airborne target, thus tethering it to the projectile, and wherein the means for producing drag slows down the speed at which the projectile and tethered airborne target descend to the ground.
Type:
Grant
Filed:
August 29, 2016
Date of Patent:
May 26, 2020
Assignee:
Airspace Systems, Inc.
Inventors:
Jasminder S. Banga, Earl R. Stirling, Noah U. Moore
Abstract: A flight control operation of a reference aerial vehicle is performed. For example, an image captured by an image sensor of the reference aerial vehicle is received. A target is detected in the image. A three-dimensional relative location of the target with respect to the reference aerial vehicle is determined based on the image. The flight control operation is performed based on the three-dimensional relative location of the target with respect to the reference aerial vehicle.
Type:
Grant
Filed:
September 26, 2018
Date of Patent:
December 24, 2019
Assignee:
Airspace Systems, Inc.
Inventors:
Guy Bar-Nahum, Hong-Bin Yoon, Karthik Govindaswamy, Hoang Anh Nguyen
Abstract: A spatio-temporal awareness engine combines a low-resolution tracking process and high resolution tracking process to employ an array of imaging sensors to track an object within the visual field. The system utilizes a low-resolution conversion through noise filtering and feature consolidation to load-balance the more computationally-intensive aspects of object tracking, allowing for a more robust system, while utilizing less computer resources. A process for target recovery and object path prediction in a robotic drone may include tracking targets using a combination of visual and acoustic multimodal sensors, operating a camera as a main tracking sensor of the multimodal sensors and feeding output of the camera to a spatiotemoral engine, complementing the main tracking sensor with non-visual, fast secondary sensors to assign rough directionality to a target tracking signal, and applying the rough directionality to prioritize visual scanning by the main tracking sensor.
Type:
Grant
Filed:
October 10, 2017
Date of Patent:
June 18, 2019
Assignee:
Airspace Systems, Inc.
Inventors:
Guy Bar-Nahum, Hoang Anh Nguyen, Jasminder S. Banga
Abstract: An aerial system discrimination system includes an aerial system disruption system, an aerial system identification system, and a permissions module. The discrimination system can additionally include or use an identifier transmission system configured to mount to the aerial system. The discrimination system functions to determine whether an aerial system is authorized or unauthorized to be in the airspace. The discrimination system can additionally function to prevent, disrupt, remove, or otherwise interact with an unauthorized aerial system within the airspace.
Abstract: Example implementations associated with the aspects of the present invention include a low altitude aircraft identification system composed by three components: a small aircraft electronic identification box with an embedded logger, a ground identification equipment to automatically identify the aircraft just pointing at it, and an identification code database. The identification code can be transmitted by a visible light color sequence or by a radio frequency signal. The ground identification device is capable of recognizing both kinds of code.
Inventors:
Earl R. Stirling, Jasminder S. Banga, Noah U. Moore, Tyler T. Valiquette, Peter Scheidl, David Adams, Christopher Liu, Kevin La, Robert Martin Johnston, Cameron Teranchi