Microwave aircraft landing system using narrow bandwidth filtering

Claim 2

A locating system comprising: source means located on known features and radiating modulated microwave carrier signals having predetermined modulated frequencies selected so as to identify each of said known features; and camera means remote from said source means for sensing said microwave carrier signals within a field of view and providing a visual perspective image of said known features, said camera means including: an array of receivers arranged in a focal plane for sensing said microwave carrier signals from separate portions of said field of view; bandwidth filter means coupled to each of said array of receivers for identifying the modulated frequency associated with each received microwave carrier signal as one of the predetermined modulated frequencies and providing an output signal to identify each detected known feature; and a visual display for generating said visual perspective image of the detected known features in response to said output signals and which distinguishes between each of said detected known features, wherein said visual display includes a plurality of pixels, and each of said pixels receives output signals generated by one of said receivers and the bandwidth filter means coupled thereto.

Claim 3

The locating system as defined in claim 1 wherein said camera means further comprises: focusing means operatively coupled to said array of receivers and aligned with the focal plane for collectively focusing said microwave carrier signals from the field of view onto the array of receivers.

Claim 4

The locating system as defined in claim 2 wherein each of said array of receivers comprises: antenna means operatively coupled to said focusing means for receiving said radiating microwave carrier signals from said portion of the field of view.

Claim 5

The locating system as defined in claim 1 wherein said narrow bandwidth filter means comprises: at least one narrow passband filter; and means for sequentially selecting the passband frequency of said passband so as to continuously monitor a number of selected frequency bandwidths.

Claim 6

The locating system as defined in claim 1 wherein said narrow bandwidth filter means comprises a plurality of passband filters connected in parallel, each of said plurality of passband filters monitoring a selected narrow frequency bandwidth.

Claim 7

The locating system as defined in claim 1 further comprising: memory means for storing the output signals in a bit map.

Claim 8

The locating system as defined in claim 1 wherein said source means comprises: a plurality of modulated sources for radiating modulated microwave power signals; and wherein, each of said plurality of modulated sources are located on a selected known feature and has a predetermined amplitude modulated frequency which identifies said feature.

Claim 9

The system as defined in claim 1 wherein said source means are located relative to a runway and selected features associated therewith and said camera means are located on an aircraft so as to provide a visual aid for an aircraft landing system.

Claim 10

A visualization system for use on an aircraft to identify features associated with an aircraft runway, said system comprising: a plurality of signal sources located on selected known features associated with an aircraft runway and radiating modulated microwave carrier signals which have modulated frequencies selected so as to identify said known features; receiver means located on an aircraft and including an array of receiver elements arranged in a focal plane for sensing said microwave carrier signals within a selected field of view, each of said receiver elements receiving microwave carrier signals from separate portions of said field of view; filtering means coupled to each of said receiver elements for identifying the modulated frequency associated with each received microwave carrier signal as one of said predetermined modulated frequencies and providing an output signal to identify each detected known feature; and imaging means including a plurality of pixels operatively connected to said receiver means for creating a visual perspective image of the detected known features in response to the output signals and which identifies and distinguishes between said detected known features, wherein each of said pixels receives output signals generated by one of said receiver means and the filtering means coupled thereto.

Claim 11

A visualization system for use on an aircraft to identify features associated with an aircraft runway, said system comprising: a plurality of signal sources located on selected known features associated with an aircraft runway and radiating modulated microwave carrier signals which have modulated frequencies selected so as to identify said known features; receiver means located on an aircraft and including an array of receiver elements arranged in a focal plane for sensing said microwave carrier signals within a selected field of view, each of said receiver elements receiving microwave carrier signals from separate portions of said field of view; filtering means coupled to each of said receiver elements for identifying the modulated frequency associated with each received microwave carrier signal as one of said predetermined modulated frequencies and providing an output signal to identify each detected known feature; and imaging means including a plurality of pixels operatively connected to said receiver means for creating a visual perspective image of the detected known features in response to the output signals and which identifies and distinguishes between said detected known features, wherein each of said pixels receives output signals generated by one of said receiver means and the filtering means coupled thereto.

Claim 12

The visualization system as defined in claim 9 wherein said receiver means further comprises: focusing means including a microwave lens for receiving the microwave signals within said field of view and focusing said received signals onto the array of receiver elements.

Claim 13

The visualization system as defined in claim 9 wherein each of said receiver elements comprises: antenna means operatively coupled to said focusing means for receiving said radiating microwave carrier signals from said portion of said field of view.

Claim 14

The visualization system as defined in claim 9 wherein said filtering means comprises at least one narrow bandpass filter for sensing said modulated frequencies of said radiating signals within selected frequency bandwidths.

Claim 15

The visualization system as defined in claim 9 wherein said filtering means comprises: at lest one narrow bandpass filter; and means for sequentially selecting a plurality of frequency bandwidths for said passband filter so as to continually monitor a number of selected frequency bandwidths.

Claim 16

The visualization system as defined in claim 9 wherein said filtering means comprises a plurality of passband filters located in parallel, each of said plurality of passband filters monitoring a selected narrow bandwidth for detecting microwave signals having one of said modulated frequencies.

Claim 17

The visualization system as defined in claim 9 further comprising: memory means for storing the output signals in a bit map.

Claim 20

The method as defined in claim 16 wherein the step of filtering comprises comparing said sensed microwave signals with narrow bandwidth filters so as to identify said modulating frequencies as one of a plurality of selected frequencies.

Claim 21

The method as defined in claim 16 further comprising the steps of: storing the output signals in a bit map; and displaying the stored output signals in a visual display.

Claim 22

The method as defined in claim 16 wherein said step of sensing said microwave signals comprises: focusing microwave signals received from a field of view onto the array of receivers along a focal plane.