Passive altimeter system for a platform and method thereof

Patent metadata

Field	Value
Publication number	US-10989797-B2
Application number	US-201816325980-A
Country	US
Kind code	B2
Filing date	Apr 25, 2018
Priority date	Apr 25, 2018
Publication date	Apr 27, 2021
Grant date	Apr 27, 2021

Abstract

A passive altimeter system comprising an angle between a point and a central boresight that is determined from distortion parameters of a lens in an infrared sensor in a countermeasure system on a mobile platform wherein the infrared sensor captures a first image for determining a distance between the platform and one of (i) a ground surface and (ii) a target, and the passive altimeter system further comprising a dimensional distance between two points in the first image that is determined from a secondary source external to the countermeasure system, and a processor to triangulate the distance between the platform and one of (i) the ground surface and (ii) the target based on the dimensional distance and the angle.

First claim

What is claimed:

1. An altimeter system comprising:
a platform adapted to be positioned at a distance relative to one of (i) a ground surface and (ii) a target;
at least one sensor carried by the platform to capture a first image;
a second image having a known resolution;
at least one non-transitory computer readable storage medium having instructions encoded thereon that, when executed by a processor, perform operations to align the first image with the second image to triangulate the distance of the platform relative to the ground surface or the target, and the instructions including:
store, at least temporarily, the first and second images on the at least one non-transitory computer readable storage medium;
determine a dimensional distance in the first image based on corresponding similar features in the second image;
determine an angle between a boresight and an object in the first image based, at least in part, on distortion parameters of the at least one sensor; and
triangulate the distance from the platform to the one of (i) the ground surface and (ii) the target based, at least in part, on the dimensional distance in the first image and the angle.

2. The altimeter system of claim 1 , wherein the platform is a movable platform, and the distance between the movable platform and the ground surface is an altitude of the movable platform.

3. The altimeter system of claim 2 , wherein the movable platform is a helicopter.

4. The altimeter system of claim 1 , wherein the second image is generated from a source that is remote from the platform.

5. The altimeter system of claim 4 , wherein the instructions further include: determine the dimensional distance in the second image prior to associating the dimensional distance with the first image.

6. The altimeter system of claim 5 , wherein the source generating the second image is a secondary source providing the second image in a similar direction as the at least one sensor.

7. The altimeter system of claim 1 , further comprising:
a second sensor carried by the platform spaced from the at least one sensor;
a first wide angle field of view associated with the at least one sensor;
a second wide angle field of view associated with the second sensor;
wherein the ground surface or the target is located in an overlap region defined by the first wide angle field of view (FOV) overlapping the second wide angle FOV.

8. The altimeter system of claim 7 , further comprising a sloped ground surface in the overlap region and the target is an obstacle in the overlap region.

9. The altimeter system of claim 8 , wherein the instructions further include:
detect the sloped ground surface or the obstacle in the overlap region as the platform is descending towards the ground surface; and
warn an operator that the ground surface is sloped or of the obstacle below the platform.

10. The altimeter system of claim 8 , wherein the instructions further include:
display a surface contour map of the ground surface below the platform, as the platform is descending, to an operator.

11. The altimeter system of claim 1 , further comprising:
a plurality of sensors carried by the platform, wherein the at least one sensor is part of the plurality of sensors;
a third image captured by a second sensor from the plurality of sensors;
an overlap region present in each of the first image and the third image, wherein a unique marker is in the overlap region; and
the instructions further including:
determine proximity of the platform respectively to the unique markers in the overlap region based, at least in part, on known mounting locations of the first and second sensors on the platform and on known distortion parameters of a lens on each of the first and second sensors.

12. The altimeter system of claim 11 , wherein the at least one sensor and the second sensors carried by the platform are passive infrared (IR) sensors, wherein at least the first image is an IR image.

13. The altimeter system of claim 12 , wherein the instructions further including compare the IR first image with the second image which is one of (i) an IR image, and (ii) a non-IR image.

14. The altimeter system of claim 1 , wherein the instructions further including activate the at least one sensor, which is part of an infrared countermeasure (IRCM) system, to determine the distance between the platform and the ground surface responsive to a global positioning system (GPS) in the platform being denied.

15. A method comprising:
providing an aircraft with a legacy infrared counter measure (IRCM) system including at least one countermeasure sensor adapted to locate threats approaching the aircraft;
capturing at least one infrared (IR) first image with the at least one countermeasure sensor;
receiving a second image from a remote source;
determining a fixed dimensional distance between two points in the second image;
determining, in the first image, an angle between the at least one countermeasure sensor and each of the same two points based, at least in part, on and accounting for distortion parameters of a lens in the at least one countermeasure sensor relative to a central boresight thereof; and
triangulating an altitude of the aircraft relative to the ground with the legacy IRCM system based on the fixed dimensional distance between the same two points and the angle between the at least one countermeasure sensor and each of the two points.

16. The method of claim 15 , further comprising:
retrofitting the legacy IRCM system to calculate the altitude of the aircraft;
triangulating the altitude of the aircraft in a GPS denied environment and without a laser range finder.

17. The method of claim 16 , further comprising:
descending the aircraft towards a ground surface;
generating a surface contour map in a display for a pilot, wherein the surface contour map is generated from the a plurality of IR images captured by the at least one countermeasure sensor.

18. The method of claim 17 , further comprising:
detecting a sloped surface beneath the aircraft prior to landing;
effecting the aircraft to move to a flat ground portion.

19. The method of claim 16 , further comprising:
determining a second dimensional distance in the first image to increase the accuracy of the altitude of the aircraft.

20. A passive altimeter system comprising an angle between a point and a central boresight that is determined from distortion parameters of a lens in an infrared sensor in a countermeasure system on a mobile platform wherein the infrared sensor captures a first image for determining a distance between the mobile platform and one of (i) a ground surface and (ii) a target, and the passive altimeter system further comprising a dimensional distance between two points in the first image that is determined from a secondary source external to the countermeasure system, and a processor to triangulate the distance between the mobile platform and one of (i) the ground surface and (ii) the target based on the dimensional distance and the angle.

Assignees

• Bae Sys Inf & Elect Sys Integ
• Bae Systems Information And Electronic Systems Integrations Inc

Inventors

• Mercier Michael N

Classifications

• G06T2207/30181

  Earth observation · CPC title

• G06T2207/10048

  Infrared image · CPC title

• G06T7/55

  from multiple images · CPC title

• G01C23/00 Primary

  Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration · CPC title

• G06T2207/10032

  Satellite or aerial image; Remote sensing · CPC title