IP Library Granted Patent US 12,228,724
Granted Patent B2
US 12,228,724 · App. 17/368,928 · Granted Feb 18, 2025

Modular reconfigurable optical systems for supporting multiple modalities

Inventors: John Anthony Tejada (Londonderry, NH); William Jeff McKinley (Westford, MA)
Assignee: Goodrich Corporation
G02B23/04G02B17/0636G02B27/1006G02B27/1013
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,228,724
App. No.
17/368,928
Granted
Feb 18, 2025
Kind
B2
Abstract

An optical system comprising includes an off-axis folded three mirror anastigmat (TMA) telescope including a primary mirror for receiving energy from a scene. A secondary mirror is aligned to receive reflected energy from the primary mirror. A fold mirror is aligned to receive reflected energy from the secondary mirror. A tertiary mirror is aligned to receive reflected energy from the fold mirror and to direct energy between the secondary mirror and the fold mirror. A beam splitter is aligned to receive energy reflected from the tertiary mirror, to reflect a portion of that energy to a first imaging sensor, and to pass a second portion of that energy to a second imaging sensor.

Claims (52)

1. An optical system comprising:

an off-axis folded three mirror anastigmat (TMA) telescope including a primary mirror configured to receive scene energy, a secondary mirror configured to receive reflected energy from the primary mirror, a fold mirror configured to receive reflected energy from the secondary mirror, and a tertiary mirror configured to receive reflected energy from the fold mirror and to direct energy between the secondary mirror and the fold mirror; and

an interchangeable module configured to be removably connected to the TMA telescope, the interchangeable module comprising:

a first imaging sensor that is sensitive to a first modality of wavelengths;

a second imaging sensor that is sensitive to a second modality of wavelengths; and

a removable beam splitter configured to receive energy reflected from the tertiary mirror, to reflect a portion of that energy to the first imaging sensor, and to pass a second portion of that energy to the second imaging sensor, wherein the removable beam splitter includes a coating configured to accommodate wavelength sensitivities of the first imaging sensor and the second imaging sensor;

wherein the interchangeable module is removable and replaceable with a second interchangeable module comprising:

a third imaging sensor that is sensitive to a third modality of wavelengths; and

a fourth imaging sensor that is sensitive to a fourth modality of wavelengths.

2. The system as recited in claim 1 , wherein each of the first modality of wavelengths and the second modality of wavelengths includes at least one of: hyperspectral, multispectral, FMV (full motion video), MWIR (midwave infrared), LWIR (long wave infrared), SWIR (short wave infrared), or LIDAR (light detection and ranging) wavelengths.

3. The system as recited in claim 1 , wherein the primary mirror and the secondary mirror are aligned and configured to form an intermediate image between the fold mirror and the tertiary mirror.

4. The system as recited in claim 1 , wherein the primary mirror, secondary mirror, fold mirror, and tertiary mirror are configured to form an exit pupil further from an optical axis of the primary mirror than the secondary mirror and the fold mirror.

5. The system as recited in claim 1 , further comprising:

a by-pass mirror configured to move relative to the primary mirror between a first position and a second position;

wherein, in the first position, the by-pass mirror is configured to by-pass the primary mirror and direct rays directly to the beam splitter for wide field of view (WFOV) imaging; and

wherein, in the second position, the by-pass mirror is stowed from reflecting rays in the TMA telescope.

6. The system as recited in claim 1 , wherein at least one of the primary mirror, secondary mirror, fold mirror, or tertiary mirror is of single point diamond turning (SPDT) aluminum construction.

7. The system as recited in claim 1 , wherein the TMA telescope has an afocal interface between the TMA telescope and the first and second imaging sensors.

8. The system as recited in claim 7 , wherein the TMA telescope has an interface that is sensitive to tilt and rotation to facilitate changing the first imaging sensor and the second imaging sensor.

9. The system as recited in claim 7 , wherein the TMA telescope and the interchangeable module are housed within a single pod or ball, and wherein the single pod or ball has a single window configured to allow the scene energy into the pod or ball.

10. A method comprising:

obtaining an off-axis folded three mirror anastigmat (TMA) telescope including a primary mirror configured to receive scene energy, a secondary mirror configured to receive reflected energy from the primary mirror, a fold mirror configured to receive reflected energy from the secondary mirror, and a tertiary mirror configured to receive reflected energy from the fold mirror and to direct energy between the secondary mirror and the fold mirror; and

changing both of a first imaging sensor and a second imaging sensor out of the TMA telescope that forms an image on each of the first and second imaging sensors, wherein an interchangeable module is configured to be removably connected to the TMA telescope, the interchangeable module comprising:

the first imaging sensor, which is sensitive to a first modality of wavelengths;

the second imaging sensor, which is sensitive to a second modality of wavelengths; and

a removable beam splitter configured to receive energy reflected from the tertiary mirror, to reflect a portion of that energy to the first imaging sensor, and to pass a second portion of that energy to the second imaging sensor, wherein the removable beam splitter includes a coating configured to accommodate wavelength sensitivities of the first imaging sensor and the second imaging sensor;

wherein changing both of the first imaging sensor and the second imaging sensor comprises replacing the interchangeable module with a second interchangeable module, the second interchangeable module comprising:

a third imaging sensor that is sensitive to a third modality of wavelengths; and

a fourth imaging sensor that is sensitive to a fourth modality of wavelengths; and

wherein replacing the interchangeable module with the second interchangeable module includes not changing front end optics including the TMA telescope.

11. The method as recited in claim 10 , wherein replacing the interchangeable module with the second interchangeable module comprises at least one of:

replacing the first imaging sensor having one of a daytime or nighttime modality with the third imaging sensor having another of the daytime or nighttime modality; or

replacing the second imaging sensor having one of the daytime or nighttime modality with the fourth imaging sensor having another of the daytime or nighttime modality.

12. The method as recited in claim 10 , wherein replacing the interchangeable module with the second interchangeable module comprises at least one of:

replacing the first imaging sensor with the third imaging sensor, replacing the second imaging sensor with the fourth imaging sensor, and bore sighting the third and fourth imaging sensors to each other with a collimator in the field or in flight; or

bore sighting the third imaging sensor with the fourth imaging sensor with a bench collimator not in the field and then replacing the first and second imaging sensors with the third and fourth imaging sensors.

13. An optical system comprising:

an off-axis folded three mirror anastigmat (TMA) telescope including a primary mirror configured to receive scene energy, a secondary mirror configured to receive reflected energy from the primary mirror, a fold mirror configured to receive reflected energy from the secondary mirror, and a tertiary mirror configured to receive reflected energy from the fold mirror and to direct energy between the secondary mirror and the fold mirror;

a first interchangeable module configured to be removably connected to the TMA telescope, the first interchangeable module comprising a first imaging sensor sensitive to at least a first plurality of wavelengths and a second imaging sensor sensitive to at least a second plurality of wavelengths, wherein the first interchangeable module is removable and replaceable with a second interchangeable module comprising a third imaging sensor sensitive to at least a third plurality of wavelengths and a fourth imaging sensor sensitive to at least a fourth plurality of wavelengths;

a pod configured to house the TMA telescope and the first interchangeable module within the pod; and

a single window configured to allow scene energy into the pod to the TMA telescope.

14. The system as recited in claim 13 , wherein the primary mirror and the secondary mirror are aligned and configured to form an intermediate image between the fold mirror and the tertiary mirror.

15. The system as recited in claim 13 , wherein the primary mirror, secondary mirror, fold mirror, and tertiary mirror are configured to form an exit pupil further from an optical axis of the primary mirror than the secondary mirror and the fold mirror.

16. The system as recited in claim 13 , wherein the TMA telescope has an afocal interface between the TMA telescope and first and second imaging sensors of the first interchangeable module.

17. The system as recited in claim 13 , wherein the TMA telescope has an interface that is sensitive to tilt and rotation to facilitate changing the first interchangeable module.

18. The system as recited in claim 13 , further comprising:

an interchangeable beam splitter configured to receive energy reflected from the tertiary mirror, reflect a portion of that energy to the first imaging sensor, and pass a second portion of that energy to the second imaging sensor;

wherein the interchangeable beam splitter includes a coating configured to accommodate wavelength sensitivities of the first imaging sensor and the second imaging sensor; and

wherein the interchangeable beam splitter is removable and replaceable with a second interchangeable beam splitter including a second coating configured to accommodate the wavelength sensitivities of the third imaging sensor and the fourth imaging sensor.

19. The system as recited in claim 13 , wherein:

the first imaging sensor is configured for daytime imaging; and

the second imaging sensor is configured for nighttime imaging.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 25, 2021
From: TEJADA, JOHN ANTHONY; MCKINLEY, WILLIAM JEFF
To: GOODRICH CORPORATION
Reel/Frame 057282/0947 →
Continuity (2)
Provisional Application 63050259 · Jul 10, 2020
Related Publication 20220011564A1 · Jan 13, 2022
References Cited (17)
US 5309276A · Rodgers · 1994 [cited by applicant]
US 5763882A · Klapper et al. · 1998 [cited by applicant]
US 5831762A · Baker et al. · 1998 [cited by applicant]
US 6400501B2 · Tsuchiya · 2002 [cited by examiner]
US 6414805B1 · Reichman · 2002 [cited by examiner]
US 8284382B2 · Krasutsky · 2012 [cited by applicant]
US 10191275B1 · Murray et al. · 2019 [cited by applicant]
US 20100020307A1 · Kunick · 2010 [cited by applicant]
US 20150028194A1 · Cook · 2015 [cited by applicant]
US 20180210166A1 · Cannon · 2018 [cited by examiner]
US 20190179130A1 · Miller et al. · 2019 [cited by applicant]
WO WO2006002271A1 · 2006 [cited by examiner]
Petrushevsky, Vladimer et al., “Common Aperture Multispectral Spotter Camera: Spectro XR”, Proceedings of SPIE, vol. 10433, Oct. 6, 2017, 7 pages. [cited by applicant]
Deepak, Sampath et al., “The WISE Telescope and Scanner: Design Choices and Hardware Results”, An Optical Believe it or Not: Key Lessons Learned II, Oct. 7, 2010, pp. 1-11. [cited by applicant]
Bongiovi R. P., et al., “Airborne LWIR Hyperspectral Measurements of Military Vehicles”, Aerospace Applications Conference, 1996, Proceedings., vol. 3, Feb. 3, 1996, pp. 121-135. [cited by applicant]
Extended European Search Report dated Dec. 9, 2021, issued during the proseuction of European Patent Application No. EP 21185055.7. 11 pages. [cited by applicant]
EP Communicaton Pursuant to Art. 94(3) EPC, dated Dec. 4, 2023, issued during the prosecution of European Patent Application No. EP 21185055.7. [cited by applicant]