Abstract: A torque tube coupler may include an outer body that includes a first abutting surface and a second abutting surface adjacent to the first abutting surface. Set screws may be inserted into one or more channels of the first abutting surface. Tightening the set screws may force the abutting surfaces away from each other and the outer body to press against an inner surface of a torque tube. Another embodiment of the torque tube coupler may include a central ring sized based on a size of a torque tube. The torque tube coupler may also include a set of fingers that extend away from a first side of the central ring and are shaped to flex radially outward. The torque tube coupler may include a core disposed within the set of fingers that, when drawn towards the central ring, causes the fingers to flex radially outwards.

Abstract: A first embodiment of a torque tube coupler may include an outer body that includes a first abutting surface and a second abutting surface adjacent to the first abutting surface. Set screws may be inserted into one or more channels of the first abutting surface. Tightening the set screws may force the abutting surfaces away from each other and the outer body to press against an inner surface of a torque tube. Another embodiment of the torque tube coupler may include a central ring sized based on a size of a torque tube. The torque tube coupler may also include a set of fingers that extend away from a first side of the central ring and are shaped to flex radially outward. The torque tube coupler may include a core disposed within the set of fingers that, when drawn towards the central ring, causes the fingers to flex radially outwards.

Abstract: A first embodiment of a torque tube coupler may include an outer body that includes a first abutting surface and a second abutting surface adjacent to the first abutting surface. Set screws may be inserted into one or more channels of the first abutting surface. Tightening the set screws may force the abutting surfaces away from each other and the outer body to press against an inner surface of a torque tube. Another embodiment of the torque tube coupler may include a central ring sized based on a size of a torque tube. The torque tube coupler may also include a set of fingers that extend away from a first side of the central ring and are shaped to flex radially outward. The torque tube coupler may include a core disposed within the set of fingers that, when drawn towards the central ring, causes the fingers to flex radially outwards.

Abstract: A method may include obtaining a normal set point of a solar panel and a wind velocity measurement corresponding to wind that affects the solar panel. The method may include determining an allowable range of tilt angles according to a first lookup table that describes a relationship between the wind velocity measurement and the allowable range of tilt angles. The method may include identifying whether the normal set point of the solar panel is outside of the allowable range of tilt angles, and responsive to identifying that the normal set point of the solar panel is outside of the allowable range of tilt angles, determining a temporary stow set point. The method may include rotating the solar panel to the temporary stow set point.

Abstract: A method may include obtaining a normal set point of a solar panel and a wind velocity measurement corresponding to wind that affects the solar panel. The method may include determining an allowable range of tilt angles according to a first lookup table that describes a relationship between the wind velocity measurement and the allowable range of tilt angles. The method may include identifying whether the normal set point of the solar panel is outside of the allowable range of tilt angles, and responsive to identifying that the normal set point of the solar panel is outside of the allowable range of tilt angles, determining a temporary stow set point. The method may include rotating the solar panel to the temporary stow set point.

Abstract: A method may include obtaining a normal set point of a solar panel and a wind velocity measurement corresponding to wind that affects the solar panel. The method may include determining an allowable range of tilt angles according to a first lookup table that describes a relationship between the wind velocity measurement and the allowable range of tilt angles. The method may include identifying whether the normal set point of the solar panel is outside of the allowable range of tilt angles, and responsive to identifying that the normal set point of the solar panel is outside of the allowable range of tilt angles, determining a temporary stow set point. The method may include rotating the solar panel to the temporary stow set point.

Abstract: A first embodiment of a torque tube coupler may include an outer body that includes a first abutting surface and a second abutting surface adjacent to the first abutting surface. Set screws may be inserted into one or more channels of the first abutting surface. Tightening the set screws may force the abutting surfaces away from each other and the outer body to press against an inner surface of a torque tube. Another embodiment of the torque tube coupler may include a central ring sized based on a size of a torque tube. The torque tube coupler may also include a set of fingers that extend away from a first side of the central ring and are shaped to flex radially outward. The torque tube coupler may include a core disposed within the set of fingers that, when drawn towards the central ring, causes the fingers to flex radially outwards.

Abstract: Apparatuses, systems and methods are provided for automatically pushing aircraft back from an airport gate and/or for automatically taxiing an aircraft. At least one engines-off drive is attached to at least one landing gear wheel to apply a rotational force and/or a rotation impeding force to the at least one landing gear wheel. At least one friction brake is attached to at least one landing gear wheel to apply a rotation impeding force to the at least one landing gear wheel.

Abstract: Apparatuses, systems and methods are provided for automatically pushing aircraft back from an airport gate and/or for automatically taxiing an aircraft. At least one engines-off drive is attached to at least one landing gear wheel to apply a rotational force and/or a rotation impeding force to the at least one landing gear wheel. At least one friction brake is attached to at least one landing gear wheel to apply a rotation impeding force to the at least one landing gear wheel.

Abstract: A ground remote control system for an aircraft includes a security pairing device configured to establish a first secure communication link and protocol between a remote control device and a ground remote control system controller; and establish a second secure communication link and protocol, using the first communication link and protocol between the remote control device and the ground remote control system controller. The ground remote control system controller is configured to receive drive command signals, brake command signals, steering command signals, and power command signals, from the remote control device and generate the electronic drive commands, the electronic brake commands, the electronic steering commands, and the electronic power commands.

Abstract: A ground remote control system for an aircraft includes a security pairing device configured to establish a first secure communication link and protocol between a remote control device and a ground remote control system controller; and establish a second secure communication link and protocol, using the first communication link and protocol between the remote control device and the ground remote control system controller. The ground remote control system controller is configured to receive drive command signals, brake command signals, steering command signals, and power command signals, from the remote control device and generate the electronic drive commands, the electronic brake commands, the electronic steering commands, and the electronic power commands.