Aviation Communication & Surveillance Systems LLC Patent applications |
Patent application number | Title | Published |
20160133138 | SYSTEMS AND METHODS FOR HELICOPTER SITUATIONAL AWARENESS AND LANDING ASSISTANCE - Systems and methods are delineated for use by a helicopter and helicopter landing stations to facilitate helicopter situational awareness and landing assistance. In accordance an exemplary embodiment, a system for use with a helicopter is delineated wherein the system comprises a ground transmitter with a GPS receiver, said ground transmitter being located in proximity to a landing pad for the helicopter; a receiver on the helicopter to receive transmissions from the ground transmitter; a display on the helicopter to depict position of the landing pad; a GPS receiver on the helicopter to provide position of the helicopter; and a database including identification information for the landing pad. | 05-12-2016 |
20150338503 | Systems and Methods for Providing ADS-B Mode Control Through Data Overlay - Embodiments of the present invention disclose systems and methods for providing enhanced features using an ATC Overlay data link. Further, there are provided systems and methods for ADS-B Mode Control that enable a transponder to selectively transmit data on a desired link, such as the ADS-B or ATC Overlay link, based on the control inputs such as current active ADS-B applications, thus reducing RF interference while maximizing the amount of pertinent data being transmitted. In various embodiments, ADS-B Mode Control also offers a mechanism to include pilot-entered data onto the ADS-B or ATC Overlay link, thereby producing flexibility for future ADS-B In applications. | 11-26-2015 |
20150248838 | INTEGRATED AVIONICS SYSTEM - There is provided an avionics system that provides several avionics functions within a single LRU. In one embodiment, the system comprises a software-configurable RF assembly, one or more processor assemblies that are configured to provide multiple TAWS/TCAS/Mode S/ADS-B/ATC functions, interfaces to allow connections to aircraft electronics and data loaders, and multipurpose antennas. In one embodiment, a common processor architecture allows generic avionics processors to be configured to operate a number of TAWS/TCAS/Mode S/ADS-B/ATC functions without the need for multiple LRUs, and software-defined RF functions allow RF circuitry that interfaces to the processors to handle current and future communication needs. | 09-03-2015 |
20150236409 | SCANNING META-MATERIAL ANTENNA AND METHOD OF SCANNING WITH A META- MATERIAL ANTENNA - Various antennas and systems of antennas can benefit from meta-material construction. For example, avionics antennas including weather antennas may benefit from being constructed of meta-materials. A method can include, for example, electronically scanning, by an antenna of an aircraft, an environment of the aircraft. The electronically scanning can include transmitting or receiving an electrical frequency over the antenna. The antenna can include a negative index of refraction meta-material. The electronically scanning can also include applying an electric field to control a dielectric constant of the antenna. | 08-20-2015 |
20140320332 | Interval Management Using Data Overlay - Computer assistance in interval management may be beneficial in a number of ways. For example, digital communication of interval management instructions or information related to interval management may beneficially be communicated to aircraft with respect to other aircraft. This information may be communicated overlaid on air traffic control (ATC) communications, or otherwise. A method can include, for example, obtaining a spacing goal for an aircraft relative to a target aircraft. The method can also include determining clearance instructions for the aircraft, wherein the speed guidance is based on the spacing goal. The method can further include transmitting the clearance instructions in a computer-readable format to the aircraft. The instructions can be provided by an overlay-modulated signal of a provided modulated ATC signal. The instructions can be configured to enable control of the aircraft to achieve the spacing goal. | 10-30-2014 |