Radar-based system, module, and method for presenting steering symbology on an aircraft display unit
AssigneeRockwell Collins, Inc.
InventorGeorge R. Kanellis
Life of this patent
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Abstract
A novel and non-trivial radar-based system, module, and method for presenting steering symbology on an aircraft display unit are disclosed. Hazard information acquired from a forward-looking aircraft radar system may be presented as hazard data to a symbology generating processor. A plurality of minimum turn angles may be determined based upon the boundary tangents of the hazard data. Data representative of steering symbology corresponding to a one or more minimum turn angles may be generated, where the symbology may take the form of textual symbology and/or non-textual symbology. Then, the steering symbology data may be provided to a presentation system for depiction of steering symbology on a tactical display unit and/or strategic display unit.
Claims20
An airborne radar-based system for presenting steering symbology on an aircraft display unit, said system comprising:
- a forward-looking aircraft radar system;
- a symbology generating processor configured to
- receive hazard data from the forward-looking aircraft radar system configured to acquire hazard data, where
- the hazard data is representative of hazard and wind correction information,
- determine a plurality of minimum turn angles based upon boundary tangents of the hazard and wind correction information, where
- such plurality includes a minimum left turn angle and a minimum right turn angle,
- generate first steering symbology data, where
- such first steering symbology data is representative of first steering symbology corresponding to a first minimum turn angle and comprised of a first non-textual, hazard avoidance steering cue presented in a tactical display image, where
- the tactical display image is comprised of at least
- an airspeed indicator,
- an altitude indicator,
- a heading indicator, and
- an attitude indicator comprised of at least pitch and roll indications, and
- provide the first steering symbology data to a presentation system;
- and
- the presentation system configured to
- receive the first steering symbology data, whereby
- the first non-textual, hazard avoidance steering cue of the first steering symbology data is superimposed against the heading indicator depicted on a tactical display unit.
An airborne radar-based module for presenting steering symbology on an aircraft display unit, said module comprising:
- an input communications interface to facilitate a providing of hazard data to a symbology generating processor;
- the symbology generating processor configured to
- receive hazard data from the forward-looking aircraft radar system configured to acquire hazard data, where
- the hazard data is representative of hazard and wind correction information,
- determine a plurality of minimum turn angles based upon boundary tangents of the hazard and wind correction information, where
- such plurality includes a minimum left turn angle and a minimum right turn angle,
- generate first steering symbology data, where
- such first steering symbology data is representative of first steering symbology corresponding to a first minimum turn angle and comprised of a first non-textual, hazard avoidance steering cue presented in a tactical display image, where
- the tactical display image is comprised of at least
- an airspeed indicator,
- an altitude indicator,
- a heading indicator, and
- an attitude indicator comprised of at least pitch and roll indications, and
- provide the first steering symbology data an output communications interface, whereby
- the first non-textual, hazard avoidance steering cue of the first steering symbology data is superimposed against the heading indicator depicted on a tactical display unit;
- and
- the output communications interface to facilitate a providing of the first steering symbology data from the symbology generating processor to a presentation system.
An airborne radar-based method for presenting steering symbology on an aircraft display unit, said method comprising:
- receiving hazard data from the forward-looking aircraft radar system configured to acquire hazard data, where
- the hazard data is representative of hazard and wind correction information;
- determining a plurality of minimum turn angles based upon boundary tangents of the hazard and wind correction information, where
- such plurality includes a minimum left turn angle and a minimum right turn angle;
- generating first steering symbology data, where
- such first steering symbology data is representative of first steering symbology corresponding to a first minimum turn angle and comprised of a first non-textual, hazard avoidance steering cue presented in a tactical display image, where
- the tactical display image is comprised of at least
- an airspeed indicator,
- an altitude indicator,
- a heading indicator, and
- an attitude indicator comprised of at least pitch and roll indications;
- and
- providing the first steering symbology data to a presentation system, whereby
- the first non-textual, hazard avoidance steering cue of the first steering symbology data is superimposed against the heading indicator depicted on a tactical display unit.
Dependencies are inferred from the claim text.