Abstract: A mounting bracket configured to receive a device to mount the device can include a first portion extending in an axial direction and configured to mount to a first side of the device, a second portion extending in the axial direction and configured to mount to a second side of the device, and a crossbar structure connecting the first portion to the second portion. The crossbar structure can extend between the first portion and the second portion in a transverse direction to the axial direction. The crossbar structure can be configured to flex to allow the first portion and the second portion to move laterally apart to allow insertion of the device between the first portion and the second portion and snap fit of the device between the first portion and the second portion.

Abstract: A mounting bracket configured to receive a device to mount the device can include a first portion extending in an axial direction and configured to mount to a first side of the device, a second portion extending in the axial direction and configured to mount to a second side of the device, and a crossbar structure connecting the first portion to the second portion. The crossbar structure can extend between the first portion and the second portion in a transverse direction to the axial direction. The crossbar structure can be configured to flex to allow the first portion and the second portion to move laterally apart to allow insertion of the device between the first portion and the second portion and snap fit of the device between the first portion and the second portion.

Abstract: A method for controlling each rotor on a multirotor aircraft includes receiving one or more sensed states of the multirotor aircraft, and determining a control scheme dynamically using the sensed one or more states of the multirotor aircraft. Receiving one or more sensed states can include receiving one or more of a rotational rate or acceleration of the aircraft, or any other suitable aircraft state.

Abstract: A rotary coupling includes a first waveguide, a second waveguide that is coaxial with the first waveguide and supported for rotation relative to the first waveguide, and a collar. The collar is connected to one of the first and second waveguides and extends circumferentially about an end of the other of the first and second waveguides to reduce attenuation of electromagnetic radiation conveyed between the first waveguide and the second waveguide.

Abstract: A method for controlling each rotor on a multirotor aircraft includes receiving one or more sensed states of the multirotor aircraft, and determining a control scheme dynamically using the sensed one or more states of the multirotor aircraft. Receiving one or more sensed states can include receiving one or more of a rotational rate or acceleration of the aircraft, or any other suitable aircraft state.