GIMBAL SYSTEMS PROVIDING HIGH-PRECISION IMAGING CAPABILITIES IN A COMPACT FORM-FACTOR
First Claim
1. A two-axis gimbal system, comprising:
- a gimbal assembly including a base subassembly, an azimuth subassembly having a rotatably mounted on the base subassembly in a manner enabling the azimuth subassembly to rotate about a first rotational axis, and an elevation subassembly rotatably mounted on the azimuth subassembly in a manner enabling the elevation subassembly to rotate about a second rotational axis, wherein the second rotational axis extends substantially perpendicular to the first rotational axis;
a laser amounted on the azimuth subassembly;
a first laser light beam steering device amounted on the azimuth subassembly, wherein the first laser light beam steering device redirects a laser light output of the laser from a first laser light beam travelling direction to a second laser light beam travelling direction and wherein the second laser light beam travelling direction is substantially along the second rotational axis;
a second laser light beam steering device mounted on the elevation subassembly for redirecting the laser light output from along the second laser light beam travelling direction to along a third laser light beam travelling direction; and
a micro-electro-mechanical system (MEMS) gyro mounted on the elevation subassembly.
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Accused Products
Abstract
A small form-factor gimbal system that provides for stabilization of payload assets in a manner that provides improved stabilization capability. Such a small form-factor gimbal system provides for precision payload asset steering functionality through integration of an inertially stabilized two-axis gimbal in combination with a beam stabilization mechanism (BSM). In a preferred embodiment, such a small form-factor gimbal system has a gimbal diameter of about 5″ or less and employs a laser assembly having a Coudé path arrangement in which the laser beam passes from the azimuth subassembly to the elevation subassembly along the elevation subassembly rotational axis.
57 Citations
17 Claims
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1. A two-axis gimbal system, comprising:
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a gimbal assembly including a base subassembly, an azimuth subassembly having a rotatably mounted on the base subassembly in a manner enabling the azimuth subassembly to rotate about a first rotational axis, and an elevation subassembly rotatably mounted on the azimuth subassembly in a manner enabling the elevation subassembly to rotate about a second rotational axis, wherein the second rotational axis extends substantially perpendicular to the first rotational axis; a laser amounted on the azimuth subassembly; a first laser light beam steering device amounted on the azimuth subassembly, wherein the first laser light beam steering device redirects a laser light output of the laser from a first laser light beam travelling direction to a second laser light beam travelling direction and wherein the second laser light beam travelling direction is substantially along the second rotational axis; a second laser light beam steering device mounted on the elevation subassembly for redirecting the laser light output from along the second laser light beam travelling direction to along a third laser light beam travelling direction; and a micro-electro-mechanical system (MEMS) gyro mounted on the elevation subassembly. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14)
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15. A two-axis gimbal system, comprising:
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a gimbal assembly including a base subassembly, an azimuth subassembly having a rotatably mounted on the base subassembly in a manner enabling the azimuth subassembly to rotate about a first rotational axis, and an elevation subassembly rotatably mounted on the azimuth subassembly in a manner enabling the elevation subassembly to rotate about a second rotational axis, wherein the second rotational axis extends substantially perpendicular to the first rotational axis; a laser assembly mounted on the azimuth subassembly, wherein the laser assembly includes a laser light beam steering device that redirects a laser light output of a laser of the laser assembly from a first laser light beam travelling direction to a second laser light beam travelling direction and wherein the second laser light beam travelling direction is substantially along the second rotational axis; a short wavelength infrared (SWIR) camera mounted on the elevation subassembly; a SWIR illuminator mounted on the elevation subassembly; a visible light camera mounted on the elevation subassembly; a micro-electro-mechanical system (MEMS) gyro mounted on the elevation subassembly; and a beam stabilization mechanism mounted on the gimbal assembly, wherein the beam stabilization mechanism includes a fast steering mirror mounted on the elevation subassembly for redirecting the laser light output from along the second laser light beam travelling direction to along a third laser light beam travelling direction and wherein the beam stabilization mechanism is coupled to an output signal of the MEMS gyro, to an output signal of the SWIR camera, to an input signal of a gimbal subassembly movement apparatus of the azimuth subassembly and to an input signal of a gimbal subassembly movement apparatus of the elevation subassembly. - View Dependent Claims (16, 17)
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Specification