Abstract: Thrust values for motors in an aircraft are generated where each flight controller in a plurality of flight controllers generates a thrust value for each motor in a plurality of motors using an optimization problem with a single solution. Each flight controller in the plurality of flight controllers passes one of the generated thrust values to a corresponding motor in the plurality of motors, where other generated thrust values for that flight controller terminate at that flight controller. The plurality of motors perform the passed thrust values.

Abstract: Thrust values for motors in an aircraft are generated where each flight controller in a plurality of flight controllers generates a thrust value for each motor in a plurality of motors using an optimization problem with a single solution. Each flight controller in the plurality of flight controllers passes one of the generated thrust values to a corresponding motor in the plurality of motors, where other generated thrust values for that flight controller terminate at that flight controller. The plurality of motors perform the passed thrust values.

Abstract: A parking system including a plurality of trays, a plurality of automated guided vehicles (AGVs) configured to transport the plurality of trays, a plurality of bays, and a controller. The controller is configured to determine a bay configuration ratio based on collected parking data, each bay being configured into one of an insert-ready state and a retrieve-ready state in accordance with the bay configuration ratio. When a bay is in the insert-ready state, a tray is placed within the bay and an outward-facing door of the bay is in an open position. When a bay is in the retrieve-ready state, the outward-facing door of the bay is in a closed position, an inward-facing door of the bay is in an open position, and no tray is positioned within the bay.

Abstract: A parking system including a plurality of automated guided vehicles (AGVs), a bay, and a controller. The controller is configured to send instruction to an AGV to move into the bay to receive a target vehicle in response to receiving a parking reservation from a user device, send instruction to the AGV to navigate the target vehicle to a target parking space, and send instruction to at least a subset of the AGVs to rearrange the target vehicle based on a pick up time indicated in the parking reservation.

Abstract: Thrust values for motors in an aircraft are generated where each flight controller in a plurality of flight controllers generates a thrust value for each motor in a plurality of motors using an optimization problem with a single solution. Each flight controller in the plurality of flight controllers passes one of the generated thrust values to a corresponding motor in the plurality of motors, where other generated thrust values for that flight controller terminate at that flight controller. The plurality of motors perform the passed thrust values.

Abstract: Thrust values for motors in an aircraft are generated where each flight controller in a plurality of flight controllers generates a thrust value for each motor in a plurality of motors using an optimization problem with a single solution. Each flight controller in the plurality of flight controllers passes one of the generated thrust values to a corresponding motor in the plurality of motors, where other generated thrust values for that flight controller terminate at that flight controller. The plurality of motors perform the passed thrust values.

Abstract: Thrust values for motors in an aircraft are generated where each flight controller in a plurality of flight controllers generates a thrust value for each motor in a plurality of motors using an optimization problem with a single solution. Each flight controller in the plurality of flight controllers passes one of the generated thrust values to a corresponding motor in the plurality of motors, where other generated thrust values for that flight controller terminate at that flight controller. The plurality of motors perform the passed thrust values.