Abstract: A system for inspecting features of an airframe, the system including a feature inspection device configured to measure an aspect of a first feature and a tracking subsystem configured to determine a position of the feature inspection device when the feature inspection device measures the aspect of the first feature. The system is configured to determine a position of the first feature on the airframe via the feature inspection device and the tracking subsystem, the determination of the position of the first feature being independent from the measurement of the aspect of the first feature.

Abstract: A system for inspecting features of an airframe, the system including a feature inspection device configured to measure an aspect of a first feature and a tracking subsystem configured to determine a position of the feature inspection device when the feature inspection device measures the aspect of the first feature. The system is configured to determine a position of the first feature on the airframe via the feature inspection device and the tracking subsystem, the determination of the position of the first feature being independent from the measurement of the aspect of the first feature.

Abstract: A system for inspecting features of an airframe, the system including a feature inspection device configured to measure an aspect of a first feature and a tracking subsystem configured to determine a position of the feature inspection device when the feature inspection device measures the aspect of the first feature. The system is configured to determine a position of the first feature on the airframe via the feature inspection device and the tracking subsystem, the determination of the position of the first feature being independent from the measurement of the aspect of the first feature.

Abstract: A system for inspecting features of an airframe, the system including a feature inspection device configured to measure an aspect of a first feature and a tracking subsystem configured to determine a position of the feature inspection device when the feature inspection device measures the aspect of the first feature. The system is configured to determine a position of the first feature on the airframe via the feature inspection device and the tracking subsystem, the determination of the position of the first feature being independent from the measurement of the aspect of the first feature.

Abstract: A system for inspecting features of an airframe, the system including a feature inspection device configured to measure an aspect of a first feature and a tracking subsystem configured to determine a position of the feature inspection device when the feature inspection device measures the aspect of the first feature. The system is configured to determine a position of the first feature on the airframe via the feature inspection device and the tracking subsystem, the determination of the position of the first feature being independent from the measurement of the aspect of the first feature.

Abstract: A system and method for locating and displaying aircraft information, such as three-dimensional models and various information about an aircraft component. The system may include a portable display, a remote processor, and one or more location and/or orientation-determining components. The models and other various information displayed on the portable display may correspond with a location and orientation of the portable display relative to the aircraft component. The location and/or orientation-determining components may include one or more infrared cameras for communicating with the remote processor and a plurality of infrared targets or infrared markers. The remote processor may be configured to filter the information provided to the portable display based on the portable display's location and orientation relative to the aircraft component, geographic location, user input, or other various parameters.

Abstract: A system and method for locating and displaying aircraft information, such as three-dimensional models and various information about an aircraft component. The system may include a portable display, a remote processor, and one or more location and/or orientation-determining components. The models and other various information displayed on the portable display may correspond with a location and orientation of the portable display relative to the aircraft component. The location and/or orientation-determining components may include one or more infrared cameras for communicating with the remote processor and a plurality of infrared targets or infrared markers. The remote processor may be configured to filter the information provided to the portable display based on the portable display's location and orientation relative to the aircraft component, geographic location, user input, or other various parameters.