Abstract: A method comprises generating a respective code-carrier difference for each of a plurality of satellite vehicle and signal frequency combinations, wherein the code-carrier difference is based on a code range and a carrier range. The method also comprises filtering the respective code-carrier difference for an unknown bias and random noise; determining whether multipath is present for each of the plurality of satellite vehicle and signal frequency combinations based on the respective filtered code-carrier difference; and computing a position solution based on trust placed in respective measurements from each of the plurality of satellite vehicle and signal frequency combinations, the trust based on whether multipath is present for the respective satellite vehicle and signal frequency combination.

Abstract: In one embodiment, a method for optimizing a set of matched features is provided. The method includes matching features between an optical image and a geo-referenced orthoimage to produce an initial set of matched features. An initial position solution is then determined for the optical image using the initial set of N matched features. The initial set of N matched features are then optimized based on a set of N sub-solutions and the initial position solution, wherein each of the N sub-solutions is a position solution using a different set of (N?1) matched features. A refined position solution is then calculated for the optical image using the optimized set of matched features.

Abstract: In one embodiment, a method for optimizing a set of matched features is provided. The method includes matching features between an optical image and a geo-referenced orthoimage to produce an initial set of matched features. An initial position solution is then determined for the optical image using the initial set of N matched features. The initial set of N matched features are then optimized based on a set of N sub-solutions and the initial position solution, wherein each of the N sub-solutions is a position solution using a different set of (N?1) matched features. A refined position solution is then calculated for the optical image using the optimized set of matched features.

Abstract: Systems and methods for using image warping to improve geo-registration feature matching in vision-aided positioning is provided. In at least one embodiment, the method comprises capturing an oblique optical image of an area of interest using an image capturing device. Furthermore, digital elevation data and at least one geo-referenced orthoimage of an area that includes the area of interest are provided. The area of interest in the oblique optical image is then correlated with the digital elevation data to create an image warping matrix. The at least one geo-referenced orthoimage is then warped to the perspective of the oblique optical image using the image warping matrix. And, features in the oblique optical image are matched with features in the at least one warped geo-referenced orthoimage.

Abstract: A method comprises generating a respective code-carrier difference for each of a plurality of satellite vehicle and signal frequency combinations, wherein the code-carrier difference is based on a code range and a carrier range. The method also comprises filtering the respective code-carrier difference for an unknown bias and random noise; determining whether multipath is present for each of the plurality of satellite vehicle and signal frequency combinations based on the respective filtered code-carrier difference; and computing a position solution based on trust placed in respective measurements from each of the plurality of satellite vehicle and signal frequency combinations, the trust based on whether multipath is present for the respective satellite vehicle and signal frequency combination.

Abstract: Systems and methods for a target locator device are provided. In one embodiment, a target locator device comprises: a high performance gyroscope; an inertial measurement unit including an accelerometer triad and a gyroscope triad; a rangefinder; a global navigation satellite system (GNSS) receiver; and a processor coupled to the high performance gyroscope, the inertial measurement unit, the rangefinder and the GNSS receiver. The processor derives an alignment heading from a heading measurement provided by the high performance gyroscope. The processor calculates a heading to a target based on a deviation from the alignment heading as measured from a heading and elevation measurement determined from the inertial measurement unit.

Abstract: A target locator system comprises at least two target-locator cameras and a wireless communication system to communicatively couple the at least two target-locator cameras. Each target-locator camera includes a target sight to sight a target, a range finder, which is aligned with the target sight, configured to determine a distance to the target, a location sensor to determine a location associated with the range finder, at least one elevation angle sensor to determine an elevation angle of the axis of the target sight when sighting the target.

Abstract: A method for determining a position of a target is described that includes establishing a reference target position and a measuring location position and measuring a range to the target, an azimuth angle to the target, and an elevation angle to the target. The reference target position, the measuring location position, the measured range to the target, the azimuth angle to the target, and the elevation angle to the target are utilized to calculate a position of the target.

Abstract: An agent for performing a mission function is provided. The agent includes at least one sensor for collecting data related to the mission function; and a sensor middleware system. The sensor middleware system includes a physical interface module including at least one socket for receiving the at least one sensor, a fault tolerance and sensor fusion module coupled to the physical interface, the fault tolerance and sensor fusion module configured to detect faults in the at least one sensor, and a mission services module coupled to the physical interface module and including algorithms for performing the mission function based on the data from the at least one sensor.

Abstract: A system for providing connectivity to co-located instruments includes a processor for receiving and processing GPS data and IMU data, a GPS receiver antenna operable to supply the GPS data to the processor, and an IMU, co-located with the GPS receiver antenna, operable to provide the IMU data to the processor. A single cable is provided between the processor and co-located equipment and, by using filtering mechanisms, the single cable is operable to simultaneously supply DC power to the IMU and to transmit the GPS data and the IMU data to the processor.

Abstract: A system for providing connectivity to co-located instruments includes a processor for receiving and processing GPS data and IMU data, a GPS receiver antenna operable to supply the GPS data to the processor, and an IMU, co-located with the GPS receiver antenna, operable to provide the IMU data to the processor. A single cable is provided between the processor and co-located equipment and, by using filtering mechanisms, the single cable is operable to simultaneously supply DC power to the IMU and to transmit the GPS data and the IMU data to the processor.