Line scanner

Claim 2

An improved line scanner for airborne radiation sensitive systems comprising: (a) means for focusing radiation having an optical axis; (b) a spin mirror included at about 45° to the optical axis; (c) a detector array comprising a plurality of radiation detector cells which provide a plurality of synchronously sampled signals representing the radiation impinging on the detector at any given time; (d) a multiplexer assembly having a plurality of multiplexer channels wherein each multiplexer channel is connected to one of the detector cells so as to receive the synchronously sampled signals; (e) means for converting the sampled signals into digital radiation signals; (f) a shaft encoder for providing positional data representing the spin mirror orientation at any given time; (g) means for providing velocity-to-height data; (h) memory means for storing the digital radiation signals together with synchronous positional data including array displacement coordinate information corresponding in time to each portion of the digital radiation signal and for storing the velocity-to-height data; (i) a frame buffer; and (j) address control means arranged to load data into the frame buffer for correction of time delays resulting from the apparent array rotation by compensating for the time delays through applying the displacement information to the corresponding sampled signal in accordance with the following equations sin θ=δx/(φ.sub.ALT /2), δx=(φ.sub.ALT /2) sin θ cos θ=y/(φ.sub.ALT /2), y=(φ.sub.ALT /2) cos θ δy=(φ.sub.ALT /2)-y=(φ.sub.ALT /2(1-cos θ) where θis the scan angle from nadir, φ ALT is the along track angular coverage per scan, y is the detector position referenced to the center of the array, δy is the along track displacement coordinate, and δx is the across track displacement coordinate.

Claim 3

The apparatus of claim 1 wherein each of the elements (a) through (j) are mounted in a cylindrical housing.

Claim 4

The apparatus of claim 1 wherein the means for focusing radiation comprises an infrared focusing lens assembly having an optical speed in the range of about F/1.0 to F/1.5.

Claim 5

The apparatus of claim 1 wherein the means for focusing radiation comprises a folded catadioptric telescope.

Claim 6

The apparatus of claim 1 wherein the means for focusing radiation comprises a folded all reflective telescope.

Claim 7

The apparatus of claim 1 wherein the detector array is structured and arranged to be a single linear array connected by TEL connections to the multiplexer assembly.

Claim 8

The apparatus of claim 6 wherein the single linear array comprises collinear detector cells and wherein the number of cells is in the range of about 100 to about 600 cells.

Claim 9

The apparatus of claim 6 wherein the detector array consists substantially of PV HgCdTe material.

Claim 10

The apparatus of claim 1 wherein the detector array is comprised of a staggered array having at least two staggered lines of detectors forming a focal plane array.

Claim 11

The apparatus of claim 9 wherein the focal plane array is bump bonded with bump interconnects to the multiplexer assembly.

Claim 12

An improved line scanner for airborne radiation sensitive systems for scanning a scene from left to right horizons including a plurality of single scene elements comprising: (a) means for focusing radiation having an optical axis; (b) a spin mirror included at about 45° to the optical axis; (c) a detector array comprising a plurality of radiation detector cells which provide a plurality of synchronously sampled signals representing the radiation impinging on the detector at any given time; (d) a multiplexer assembly having a plurality of multiplexer channels wherein each multiplexer channel is connected to one of the detector cells so as to receive the synchronously sampled signals; (e) means for converting the sampled signals into digital radiation signals; (f) a shaft encoder for providing positional data representing the spin mirror orientation at any given time; (g) means for accepting and conditioning a velocity-to-height signal from a system external to the invention; (h) memory means for storing the digital radiation signals together with synchronous positional data including array displacement coordinate information corresponding in time to each portion of the digital radiation signal and for storing the velocity-to-height data; (i) a frame buffer; and (j) address control means arranged to load data into the frame buffer for correction of time delays resulting from the apparent array rotation by compensating for the time delays through applying the displacement information to the corresponding sampled signal in accordance with the following equations sin θ=δx/(φ.sub.ALT /2), δx=(φ.sub.ALT /2) sin θ cos θ=y/(φ.sub.ALT /2), y=(φ.sub.ALT /2) cos θ δy=(φ.sub.ALT /2)-y=(φ.sub.ALT /2)(1-cos θ) where θis the scan angle from nadir, φ ALT is the along track angular coverage per scan, y is the detector position referenced to the center of the array, δy is the along track displacement coordinate, and δx is the across track displacement coordinate; (k) means for selecting detector signal channels; and (l) means for combining detector signals, said equations used in conjunction with detector signal channel selection and signal combination means so as to provide an approximately constant ground footprint of each scan swath throughout a scan from one horizon to the other and so as to provide enhanced signal-to-noise ratio for those portions of the scan between the left horizon and -60° scan angle and between +60° and the right horizon, said signal-to-noise ratio improvement being a factor of the square root of n at either horizon and less elsewhere, where n is the number of detector signals being combined to represent a single scene element.

Claim 13

An improved line scanner for airborne radiation sensitive systems for scanning a scene from left to right horizons including a plurality of single scene elements comprising: (a) means for focusing radiation having an optical axis; (b) a spin mirror included at about 45° to the optical axis; (c) a detector array comprising a plurality of radiation detector cells which provide a plurality of synchronously sampled signals representing the radiation impinging on the detector at any given time; (d) a multiplexer assembly having a plurality of multiplexer channels wherein each multiplexer channel is connected to one of the detector cells so as to receive the synchronously sampled signals; (e) means for converting the sampled signals into digital radiation signals; (f) a shaft encoder for providing positional data representing the spin mirror orientation at any given time; (g) means for accepting and conditioning a velocity-to-height signal from a system external to the invention; (h) memory means for storing the digital radiation signals together with synchronous positional data including array displacement coordinate information corresponding in time to each portion of the digital radiation signal and for storing the velocity-to-height data; (i) a frame buffer; and (j) address control means arranged to load data into the frame buffer for correction of time delays resulting from the apparent array rotation by compensating for the time delays through applying the displacement information to the corresponding sampled signal in accordance with the following equations sin θ=δx/(φ.sub.ALT /2), δx=(φ.sub.ALT /2) sin θ cos θ=y/(φ.sub.ALT /2), y=(φ.sub.ALT /2) cos θ δy=(φ.sub.ALT /2)-y=(φ.sub.ALT /2)(1-cos θ) where θis the scan angle from nadir, φ ALT is the along track angular coverage per scan, y is the detector position referenced to the center of the array, δy is the along track displacement coordinate, and δx is the across track displacement coordinate; (k) means for selecting detector signal channels; and (l) means for combining detector signals, said equations used in conjunction with detector signal channel selection and signal combination means so as to provide an approximately constant ground footprint of each scan swath throughout a scan from one horizon to the other and so as to provide enhanced signal-to-noise ratio for those portions of the scan between the left horizon and -60° scan angle and between +60° and the right horizon, said signal-to-noise ratio improvement being a factor of the square root of n at either horizon and less elsewhere, where n is the number of detector signals being combined to represent a single scene element.

Claim 14

The apparatus of claim 11 wherein each of the elements (a) through (l) are mounted in a cylindrical housing.

Claim 15

The apparatus of claim 11 wherein the means for focusing radiation comprises an infrared focusing lens assembly having an optical speed in the rang of about F/1.0 to F/1.5.

Claim 16

The apparatus of claim 11 wherein the means for focusing radiation comprises a folded catadioptric telescope.

Claim 17

The apparatus of claim 11 wherein the means for focusing radiation comprises a folded all reflective telescope.

Claim 18

The apparatus of claim 11 wherein the detector array is structured and arranged to be a single linear array connected by TEL connections to the multiplexer assembly.

Claim 19

The apparatus of claim 16 wherein the single linear array comprises collinear detector cells and wherein the number of cells is in the range of about 100 to about 600 cells.

Claim 20

The apparatus of claim 16 wherein the detector array consists substantially of PV HgCdTe material.

Claim 21

The apparatus of claim 11 wherein the detector array is comprised of a staggered array having at least two staggered lines of detectors forming a focal plane array.

Claim 22

The apparatus of claim 19 wherein the focal plane array is bump bonded with bump interconnects to the multiplexer assembly.