Abstract:
Systems and methods for improved state estimates using filter algorithms are provided. In one embodiment, a method for navigating a vehicle comprises executing a filter algorithm having a state transition matrix that calculates an update to a state vector based on a state vector for a previous instance in time; receiving inertial measurement data from at least one inertial sensor; receiving data from at least one navigation aid; monitoring for the existence of one or more conditions based on a known error characteristic of the at least one inertial sensor; when the one or more conditions exist, calculating at least one element of the one or more elements of the state transition matrix based on the data from the at least one navigation aid; and when the one or more conditions do not exist, calculating the one or more elements of the state transition matrix based on inertial measurement data.
Abstract:
A system and method for enhancing the performance of satellite navigation receivers are disclosed, which incorporate a precise frequency reference in a satellite navigation receiver that reduces the system's dependence on maintaining continuous satellite reception for RAIM availability. As one example, a system for enhancing the performance of a satellite navigation receiver is disclosed, which includes a GPS receiver and a high precision (e.g., atomic) clock incorporated into the GPS receiver. The use of the high precision clock reduces clock error and the number of satellite measurements needed to meet existing RAIM availability requirements. For example, incorporating a precision clock into a GPS receiver provides an enhanced system that meets existing RAIM availability requirements with at least one less satellite measurement than the number needed for prior systems using RAIM.
Abstract:
An apparatus for providing information pertaining to the orientation of a vehicle to which the apparatus is coupled includes a chassis having a first interior surface and an inertial-sensor assembly disposed within the chassis and having a first exterior surface. A first sensor element is mounted on the first interior surface, and a second sensor element is mounted on the first exterior surface. At least one of the first and second sensor elements is configured to generate a first signal corresponding to an angle of displacement of the second sensor element with respect to the first sensor element.
Abstract:
An apparatus for providing information pertaining to the orientation of a vehicle to which the apparatus is coupled includes a chassis having a first interior surface and an inertial-sensor assembly disposed within the chassis and having a first exterior surface. A first sensor element is mounted on the first interior surface, and a second sensor element is mounted on the first exterior surface. At least one of the first and second sensor elements is configured to generate a first signal corresponding to a distance of displacement of the second sensor element with respect to the first sensor element.
Abstract:
An apparatus for providing information pertaining to the orientation of a vehicle to which the apparatus is coupled includes a chassis having a first interior surface and an inertial-sensor assembly disposed within the chassis and having a first exterior surface. A first sensor element is mounted on the first interior surface, and a second sensor element is mounted on the first exterior surface. At least one of the first and second sensor elements is configured to generate a first signal corresponding to a distance of displacement of the second sensor element with respect to the first sensor element.
Abstract:
A method and systems for processing Global Positioning System (GPS) signals is provided. The method includes determining if two signals or more signals with the same pseudorandom number bit sequence (PRN) are detected by a GPS receiver.
Abstract:
A navigation system includes a Kalman filter to compensate for bias errors in inertial sensing elements. An observed pitch, roll or heading change is input to the Kalman filter either from an aiding source or when the navigation system is in a known condition. The Kalman filter generates a correction signal that is provided to the navigation computation system.
Abstract:
Apparatus and method for the surveying of bore holes, for example, oil wells and the like, to permit accurate three-dimensional mapping thereof, using a single rate gyroscope and an accelerometer package in an instrumentation pod which is lowered into the bore hole. Signals from the accelerometers and the rate gyroscope plus the increments by which the pod is lowered into the well permit continual calculation of pod attitude and updated of pod position at all depths in the hole.
Abstract:
A method of determining an operational state of a navigation system of a platform is provided. The method comprises testing at least a portion of hardware in the navigation system. Additionally, a measurement of at least one navigation variable from an inertial sensor is combined with a measurement of another navigation variable. A plurality of residuals for the measurement of at least one navigation variable and the measurement of another navigation variable are determined with a blending filter. An error for the measurement of at least one navigation variable is estimated based on the plurality of residuals. The method also predicts an error for the measurement of at least one navigation variable while the navigation system is in route. A determination is made as to whether the navigation system meets operational standards based on testing at least a portion of hardware, estimating an error for the measurement of at least one navigation variable, and predicting an error for the measurement of at least one navigation variable. Finally, one of a first state and a second state of the navigation system is output, the first state indicating that the navigation system does meet operational standards and the second state indicating that the navigation system does not meet operational standards.
Abstract:
A method of determining an operational state of a navigation system of a platform is provided. The method comprises testing at least a portion of hardware in the navigation system. Additionally, a measurement of at least one navigation variable from an inertial sensor is combined with a measurement of another navigation variable. A plurality of residuals for the measurement of at least one navigation variable and the measurement of another navigation variable are determined with a blending filter. An error for the measurement of at least one navigation variable is estimated based on the plurality of residuals. The method also predicts an error for the measurement of at least one navigation variable while the navigation system is in route. A determination is made as to whether the navigation system meets operational standards based on testing at least a portion of hardware, estimating an error for the measurement of at least one navigation variable, and predicting an error for the measurement of at least one navigation variable. Finally, one of a first state and a second state of the navigation system is output, the first state indicating that the navigation system does meet operational standards and the second state indicating that the navigation system does not meet operational standards.