Coded aperture seeker for navigation
A guided munition system includes a munition body including at least one fluid dynamic control for changing course of the munition body in flight. A seeker onboard the munition body is operatively connected to control the at least one fluid dynamic control. The seeker includes a coded aperture imaging device facing outward from the munition body for image based control for guiding the munition body in flight.
1. A guided munition system comprising:
a munition body including at least one fluid dynamic control for changing course of the munition body in flight; and
a seeker onboard the munition body operatively connected to control the at least one fluid dynamic control, wherein the seeker includes a coded aperture imaging device facing outward from the munition body for image based control for guiding the munition body in flight,
wherein the coded aperture imaging device includes a sensor spaced apart from a coded aperture,
wherein the sensor includes a focal plane array (FPA),
wherein the FPA is sensitive to short-wave infrared (SWIR) wavelengths,
wherein the coded aperture includes a pattern of transparent and opaque or reflective areas defined in a mask on the substrate, and
wherein the coded aperture includes a spatial light modulator (SLM) configured to change the pattern in the mask for situational adaptability.
2. The system as recited in claim 1 , wherein the coded aperture imaging device faces forward on the munition body relative to a longitudinal axis of the munition body.
3. The system as recited in claim 1 , wherein the coded aperture imaging device faces laterally relative to a longitudinal axis of the munition body.
4. The system as recited in claim 1 , wherein the coded aperture imaging device is a laterally facing coded aperture imaging device, which faces laterally relative to a longitudinal axis of the munition body, wherein the laterally facing coded aperture imaging device is configured to provide images to the seeker for navigation as the munition body spins about the longitudinal axis.
5. The system as recited in claim 1 , wherein the coded aperture imaging device is a first laterally facing coded aperture imaging device, which faces laterally relative to a longitudinal axis of the munition body, and further comprising:
at least one additional laterally facing coded aperture imaging device operatively connected to the seeker, wherein the first laterally facing coded aperture imaging device and the at least one additional laterally facing coded aperture imaging device are configured to provide images to the seeker for navigation as the munition body is spin stabilized about the longitudinal axis.
6. The system as recited in claim 5 , wherein the seeker is configured to utilize images obtained of celestial bodies, horizon, and surface terrain from the at least one laterally facing coded aperture imaging device.
7. A guided munition system comprising:
a munition body including at least one fluid dynamic control for changing course of the munition body in flight; and
a seeker onboard the munition body operatively connected to control the at least one fluid dynamic control, wherein the seeker includes a coded aperture imaging device facing outward from the munition body for image based control for guiding the munition body in flight,
wherein the coded aperture imaging device includes a sensor spaced apart from a coded aperture,
wherein the sensor includes a focal plane array (FPA), wherein the FPA is sensitive to short-wave infrared (SWIR) wavelengths,
wherein the coded aperture includes a pattern of transparent and opaque or reflective areas defined in a mask on the substrate, and wherein the coded aperture includes a static coded pattern attached to actuators configured to move the static coded pattern relative to the sensor.
8. The system as recited in claim 1 , wherein the coded aperture imaging device is mounted on an outer skin of the munition body.
9. A method of guiding a munition comprising:
guiding a munition to a target using images obtained with a coded aperture imaging device onboard the guided munition wherein the coded aperture imaging device includes a spatial light modulator (SLM) configured to change the pattern in a mask for situational adaptability.
10. The method as recited in claim 9 , wherein using images obtained with a coded aperture imaging device includes collecting images while the coded aperture imaging device is directed to the sky and, digitally processing the images to locate celestial bodies within the images.
11. The method as recited in claim 9 , wherein using images obtained with a coded aperture imaging device includes collecting images of the ground and comparing the images to topology maps of a terrain path.
12. The method as recited in claim 9 , wherein guiding the munition includes finding direction and orientation of the munition by analyzing lines of data within an image from the coded aperture imaging device that includes the horizon.
13. The method as recited in claim 9 , wherein guiding the munition includes using direction intensity data of the atmosphere with sky in view in an image from the coded aperture imaging device.
14. The method as recited in claim 9 , further comprising upfinding for the munition, determining pitch of the munition, and determining roll of the munition using an image from the coded aperture imaging device.
15. The method as recited in claim 9 , further comprising determining yaw of the munition through determining rotational orientation of celestial bodies in a celestial view in an image from the coded aperture imaging device.
16. A method of guiding a munition comprising:
guiding a munition to a target using images obtained with a coded aperture imaging device onboard the guided munition, wherein the coded aperture imaging device includes a static coded pattern attached to actuators configured to move the static coded pattern relative to a sensor.