Real-time satellite imaging system
Methods and apparatus for Real-time Satellite Imaging System ( 10 ) are disclosed. More particularly, one embodiment of the present invention an imaging sensor ( 14 ) on a geostationary satellite having one or more co-collimated telescopes ( 18 ). The telescopes ( 18 ) illuminate focal planes ( 22 ) which are sparsely populated with focal plane arrays ( 24 ). The focal plane arrays ( 24 ) record the entire observable Earth hemisphere at one time, at least once every ten seconds, or more often.
1 . An apparatus comprising:
an image sensor;
said image sensor including a plurality of co-collimated telescopes; said co-collimated telescopes being configured to produce a plurality of images of the same field of view;
said image sensor being carried aboard a satellite in geostationary orbit;
said image sensor being configured to be pointed generally toward Earth;
said image sensor including a focal plane;
said focal plane including a plurality of focal plane arrays;
said focal plane arrays being configured to produce a plurality of data;
said focal plane arrays being sparsely populated upon said focal plane of each of said co-collimated telescopes;
said plurality of data including of a plurality of images of a generally entire visible hemisphere of the surface of the Earth;
said plurality of data providing persistent imaging of said generally entire visible hemisphere of the surface of the Earth;
said plurality of images each being captured as full images substantially simultaneously;
said plurality of images each having resolutions that correspond with an image at nadir having at least one hundred meter resolution.
2 . An apparatus as recited in claim 1 , in which said image sensor is a staring sensor.
3 . An apparatus as recited in claim 1 , in which each of said plurality of focal plane arrays is connected to a field programmable gate array.
4 . An apparatus as recited in claim 1 , in which
each of said plurality of focal plane arrays is connected to a sensor image control element; each of said sensor image control elements is configured to limit a light integration time of its associated focal plane array.
5 . An apparatus as recited in claim 1 , in which
each of said plurality of said sensor image control elements are configured to set the number of frames per second delivered in the plurality of data from the plurality of focal plane arrays from one-tenth of a frame per second to twenty frames per second.
6 . An apparatus as recited in claim 1 , further comprising:
a sensor image readout element;
said sensor image readout element being configured to readout in parallel said plurality of data from said plurality of focal plane arrays.
7 . An apparatus as recited in claim 1 , in which
said sensor image readout elements are configured to transmit a maximum light level of each of said plurality of focal plane arrays to said sensor image control element.
8 . An apparatus as recited in claim 1 , further comprising:
an image processing element;
said image processing element including a plurality of software controlled electronic processing elements; said software controlled electronic processing elements being configured to receive the raw levels of said plurality of data from said plurality of focal plane arrays.
9 . An apparatus as recited in claim 1 , further comprising:
an electrically reactive high index of refraction material plate;
a sensor image control element; said sensor image control element including a voltage control element;
said voltage control element being configured to apply a plurality of different voltages across said electrically reactive high index of refraction material plate;
said electrically reactive high index of refraction material plate altering the direction of a plurality of light rays illuminating each of said plurality of focal plane arrays.
10 . An apparatus as recited in claim 1 , in which said plurality of images being furnished for viewing at a remote location on Earth within not more than thirty seconds of the event being observed generally on the Earth.
11 . An apparatus comprising:
an image sensor;
said image sensor including a telescope; said telescope being configured to produce an image of the field of view;
said image sensor including an electrically reactive high index of refraction material plate;
said image sensor including a sensor image control element; said sensor image control element including a voltage control element;
said voltage control element being configured to apply a plurality of different voltages across said electrically reactive high index of refraction material plate;
said electrically reactive high index of refraction material plate altering the direction of a plurality of light rays illuminating each of said plurality of focal plane arrays;
said image sensor being carried aboard a satellite in geostationary orbit;
said image sensor being configured to be pointed generally toward Earth;
said image sensor including a focal plane;
said focal plane including a focal plane array;
said focal plane array being configured to produce a plurality of data;
said plurality of data providing persistent imaging of at least a portion of said generally visible hemisphere of the surface of the Earth;
said image being captured as a full image substantially simultaneously;
said plurality of images each having resolutions that correspond with an image at nadir having a resolution of at least hundred meters
12 . An apparatus as recited in claim 11 , in which said image sensor is a staring sensor.
13 . An apparatus as recited in claim 11 , in which each of said plurality of focal plane arrays is connected to a field programmable gate array.
14 . An apparatus as recited in claim 11 , in which
each of said plurality of focal plane arrays is connected to a sensor image control element; each of said sensor image control elements is configured to limit a light integration time of its associated focal plane array from one microsecond to ten seconds.
15 . An apparatus as recited in claim 11 , in which
each of said plurality of said sensor image control elements are configured to set the number of frames per second delivered in the plurality of data from the plurality of focal plane arrays from a frame every ten seconds to twenty frames per second.
16 . An apparatus as recited in claim 11 , further comprising:
a sensor image readout element;
said sensor image readout element being configured to readout in parallel said plurality of data from said plurality of focal plane arrays.
17 . An apparatus as recited in claim 11 , in which
said sensor image readout element is configured to transmit a maximum light level of said focal plane array to said sensor image control element.
18 . An apparatus as recited in claim 11 , further comprising:
an image processing element;
said image processing element including a software controlled electronic processing element;
said software controlled electronic processing element being configured to receive the raw levels of said plurality of data from said plurality of focal plane arrays.
19 . An apparatus as recited in claim 11 , in which said plurality of images being furnished for viewing at a remote location on Earth within not more than thirty seconds of the event being observed generally on the Earth.