An instrument (20) determines the attitude of a spacecraft (3) on which it is mounted, by interacting incident light (11) from the Sun with one or more light conditioning elements (12) and thereby forming a diffraction pattern at a photo-sensitive detector (13). The intensity distribution of light on the detector (13) is dependent on the angle of incidence of the light (11). An on-board computer (16) determines a direction vector to the Sun based on the light diffraction pattern detected by the detector (13).

Embodiments disclosed herein relate to solar tracking apparatuses, systems that include the same, and methods of operating the same. An example solar tracking apparatus includes a structure attachment portion configured to be attached to a structure (e.g., a moveable or stationary structure) and to remain relatively stationary relative to the structure. The structure attachment portion may include one or more mounts configured to attach the structure attachment portion to the structure. The solar tracking apparatus also includes at least one solar panel portion coupled to the structure attachment portion. The solar panel portion may be configured to move relative to the structure attachment portion and the structure. For example, the solar tracking apparatus may include one or more actuators coupled to solar panel portion configured to move at least a portion of the solar panel portion relative to the structure attachment portion.

System and method of controlling operation of an optical sensor in a device. The optical sensor is configured to employ a scan pattern to scan respective portions of a full field of view. A navigation sensor is configured to obtain location coordinates of the device. An inertial sensor is configured to obtain an acceleration data of the device in a plurality of directions. A controller is configured to determine a position of the device at the present time based in part on the location coordinates and the acceleration data. The controller is configured to determine a sun striking zone based in part on a relative position of the sun and the device. When a sun overlap region between the respective portions of the full field of view and sun striking zone exceeds a first overlap threshold, operation of the optical sensor is modified.

A system and method for array level terrain based backtracking includes a tracker configured to collect solar irradiance and attached to a rotational mechanism for changing a plane of the tracker and a controller in communication with a rotational mechanism. The controller is programmed to determine a position of the sun at a first specific point in time, retrieve height information, execute a shadow model based on the retrieved height information and the position of the sun, determine a first angle for the tracker; collect an angle for each tracker in a plurality of trackers in an array; adjust the first angle based on executing the shadow model with the first angle and the plurality of angles associated with the plurality of trackers; transmit instructions to the rotational mechanism to change the plane of the tracker to the adjusted first angle.

Apparatus, systems, and methods are disclosed for tracking movement over the ground or other surfaces of tools or instruments or equipment, such as buried object locators or other devices, and generating motion, position, location, mapping and/or related information for tracked locations, as well as measuring and storing associated signals and other information detected or generated during tracking.

Methods and apparatus for tracking movement over the ground or other surfaces of a buried utility locator during a utility locate operation are disclosed.

A computer-implemented method includes receiving, with a vehicle computing system, global position system (GPS) data associated with a vehicle, determining a solar position relative to the vehicle, receiving trip information associated with the vehicle, and executing one or more vehicle actuators based at least in part on the GPS data, the trip information and the solar position relative to the vehicle. Determining the solar position can include determining a sun glare period during a future time period based at least in part on the trip information associated with the vehicle. The vehicle computing system may display a warning indicative of the sun glare period, generate a window tint command that causes the window to tint and/or generate a vent control command that causes the vent to change one or more of an airflow temperature, and an airflow velocity.

Described are systems and methods for direct sun imaging by a star tracker. Disclosed in a certain example is a direct sun imaging star tracker that includes an imaging sensor and a baffle. The baffle includes a star port, a sun port, and a beam splitter. The star port is configured to image first viewing environment while the sun port is configured to image a second viewing environment that includes the sun. The beam splitter is configured to combine electromagnetic radiation from the star port and the sun port into a combined image. In various examples, the systems and techniques described herein allow a star tracker to simultaneously view both the sun and the stars.

An adaptive filter system and a method for controlling the adaptive filter system are described herein. The system can includes one or more filters to attenuate incoming light. The one or more filters can be moved by one or more actuators. The method can capture image data from an imaging device through the one or more filters. Information can be determined from the captured image data. The one or more filters can be moved to a position for capturing image data based on the information.

A system and method for array level terrain based backtracking includes a tracker configured to collect solar irradiance and attached to a rotational mechanism for changing a plane of the tracker and a controller in communication with a rotational mechanism. The controller is programmed to determine a position of the sun at a first specific point in time, retrieve height information, execute a shadow model based on the retrieved height information and the position of the sun, determine a first angle for the tracker; collect an angle for each tracker in a plurality of trackers in an array; adjust the first angle based on executing the shadow model with the first angle and the plurality of angles associated with the plurality of trackers; transmit instructions to the rotational mechanism to change the plane of the tracker to the adjusted first angle.