G01S13/882

METHOD AND APPARATUS FOR IMPROVING CO-CHANNEL OPERATION OF INDEPENDENT RADIO SYSTEMS

A method, apparatus and system for improving co-channel operation of simultaneously operating, independent radio signals. The method, apparatus and system receive at least two co-channel RF signals, perform motion compensated correlation upon at least one of the at least two co-channel RF signals, and determine the direction of arrival of the at least one of the at least two co-channel RF signals. In response to the direction of arrival determined for the at least one of the at least two co-channel RF signals, an action to perform to improve co-channel operation of the at least two co-channel RF signals at a subject receiver is determined.

ALTIMETER WITH HIGH-RESOLUTION RADAR
20210048522 · 2021-02-18 ·

In some examples, a system is configured to be mounted on a vehicle, the system including one or more phased-array radar devices configured to transmit first radar signals, receive first returned radar signals, transmit second radar signals, and receive second returned radar signals. In some examples, the system also includes processing circuitry configured to detect an object based on the first returned radar signals and determine an estimated altitude of the vehicle above a ground surface based on the second returned radar signals.

METHODS, APPARATUSES AND SYSTEMS FOR PREDICTING RADIO ALTIMETER FAILURE

Methods, apparatuses, and systems for predicting radio altimeter failures are provided. An example method may include determining a first plurality of altitude values associated with a first radio altimeter, determining a second plurality of altitude values associated with a second radio altimeter, calculating a first level feature based at least in part on the first plurality of altitude values and the second plurality of altitude values, and determining a radio altimeter failure indicator based at least in part on the first level feature.

Dual band radar altimeter system and method

An altimeter apparatus for an aircraft includes an altimeter circuit and can use a method of determining altitude. The method includes receiving a first signal in a first band via a first receive antenna, and receiving a second signal in a second band via a second receive antenna. The first band is a C-Band and the second band is at least one of a W-Band, Ku-Band, Ka-Band, V-band, or K-Band. The method also includes providing an altitude in response to the first signal or the second signal.

Frequency modulated continuous wave radio altimeter spectral monitoring

In one embodiment, a radio altimeter tracking filter is provided. The filter comprises: a wireless radio interface; a processor coupled to the wireless radio interface; a memory coupled to the wireless radio interface; wherein the wireless radio interface is configured to wirelessly receive a radio altimeter signal and convert the radio altimeter signal to a baseband frequency signal, wherein the a radio altimeter signal sweeps across a first frequency spectrum between a first frequency and a second frequency; wherein the processor is configured to pass the baseband frequency signal through a filter executed by the processor, the filter comprising a passband having a first bandwidth, and wherein the filter outputs a plurality of spectral chirps in response to the baseband frequency signal passing through the first bandwidth; wherein the processor is configured to process the plurality of spectral chirps to output characteristic parameters that characterize the radio altimeter signal.

SURVEY-AUGMENTED NAVIGATION SYSTEM FOR AN AIRCRAFT

A system having components coupled to an aircraft and components remote from the aircraft processes radar-augmented data, transmits information between aircraft system components and/or remote system components, and dynamically determines locations and states of the aircraft, while the aircraft is in flight. Based on the locations and states of the aircraft, the system generates instructions for flight control of the aircraft toward a flight path appropriate to the locations of the aircraft, and can update flight control instructions as new data is received and processed.

SYSTEM FOR DESIGNATING A BOUNDARY OR AREA FOR A PET TECHNICAL FIELD
20210000078 · 2021-01-07 ·

An apparatus, system, and method for designating a boundary for a pet is usable both outdoors and indoors. A collar device communicates with satellites or indoor location devices to define a boundary for containment of an animal or pet. The device also includes an altimeter for detecting an altitude of the pet, for example, when a pet may jump up onto a table, counter or bed, or when a pet may travel to a different floor of a home, building or other structure.

System for designating a boundary or area for a pet technical field
10863718 · 2020-12-15 ·

An apparatus, system, and method for designating a boundary for a pet is usable both outdoors and indoors. A collar device communicates with satellites or indoor location devices to define a boundary for containment of an animal or pet. The device also includes an altimeter for detecting an altitude of the pet, for example, when a pet may jump up onto a table, counter or bed, or when a pet may travel to a different floor of a home, building or other structure.

Distance sensor test system

A distance sensor and a measured object are positioned at a known distance from each other. A measured distance between the distance sensor and the measured object is obtained from the distance sensor, where the distance sensor uses a plurality of signals at a plurality of angles to generate the measured distance. The known distance and the measured distance are compared in order to test the distance sensor and produce a test result.

Survey-augmented navigation system for an aircraft

A system having components coupled to an aircraft and components remote from the aircraft processes radar-augmented data, transmits information between aircraft system components and/or remote system components, and dynamically determines locations and states of the aircraft, while the aircraft is in flight. Based on the locations and states of the aircraft, the system generates instructions for flight control of the aircraft toward a flight path appropriate to the locations of the aircraft, and can update flight control instructions as new data is received and processed.